CN115416871B - Method, device, equipment and medium for quickly disassembling thrust pin of engine - Google Patents
Method, device, equipment and medium for quickly disassembling thrust pin of engine Download PDFInfo
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- CN115416871B CN115416871B CN202210984299.3A CN202210984299A CN115416871B CN 115416871 B CN115416871 B CN 115416871B CN 202210984299 A CN202210984299 A CN 202210984299A CN 115416871 B CN115416871 B CN 115416871B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/02—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for connecting objects by press fit or for detaching same
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
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Abstract
The application discloses a method, a device, equipment and a medium for quickly disassembling an engine thrust pin, and relates to the technical field of thrust pin disassembly. The method comprises the steps of obtaining a theoretical tension value of a trolley bracket; the trolley bracket is used for supporting the target engine; controlling the trolley bracket to move to a clearance position between the installation cabin and the target engine; obtaining an actually measured tension value of the trolley bracket; the actually measured tension value is a tension value received by the trolley bracket after the target engine is used and is placed on the trolley bracket; comparing the actually measured tension value with the theoretical tension value to obtain a comparison result; and controlling the trolley bracket to adjust based on the comparison result so as to detach the thrust pin on the target engine. Thus, the target engine can be accurately adjusted to the horizontal position, and the thrust pin is less prone to damage.
Description
Technical Field
The application relates to the technical field of thrust pin disassembly, in particular to a method, a device, equipment and a medium for quickly disassembling an engine thrust pin.
Background
The manufacturing precision requirement of the engine and the matched parts thereof in the aviation field is high, the engine belongs to a high-value product, and if the engine is improperly operated in the mounting and dismounting processes, the engine is easy to cause larger scrapping loss. When the engine is installed, the end face of the engine is inserted into the engine for connection through the engine thrust pin, after the engine thrust pin enters the installation cabin along with the engine, the thrust pin is pressed by clamping in the installation cabin, and the thrust pin is fixed by two clamping bolts, so that the assembly of the engine in the installation cabin is realized.
The thrust pin is used as a force transmission piece of engine thrust and is in interference fit with the clamping device, so that the surface precision requirement is high. In the subsequent working process, the engine is required to be disassembled due to the arrangement of the airplane, and the state of the engine is inconsistent with the state of the engine under the initial static condition after the engine flies for a plurality of times, so that the stress of the airplane is likely to be born. If the thrust pin is detached without eliminating the stress of the engine, the surface of the thrust pin is easily damaged, and the larger scrapped amount is caused. In the prior art, when the thrust pin on the engine is disassembled, the stress condition of the engine is judged only by the experience of a line of operators, so that the stress condition of the engine is judged inaccurately, and the damage of the thrust pin is easy to cause.
Disclosure of Invention
The application mainly aims to provide a method, a device, equipment and a medium for quickly disassembling an engine thrust pin, and aims to solve the technical problem that in the prior art, when the thrust pin on the engine is disassembled, the stress condition of the thrust pin subjected to the engine is judged to be inaccurate, so that the thrust pin is easy to damage.
To achieve the above object, a first aspect of the present application provides a method for quickly disassembling an engine thrust pin, the method comprising:
Obtaining a theoretical tension value of the trolley bracket; when the target engine is not used, the theoretical tension value is horizontally placed on the trolley bracket, so that the trolley bracket receives the tension value; the trolley bracket is used for supporting the target engine;
Controlling the trolley bracket to move to a clearance position between the installation cabin and the target engine so that the trolley bracket supports the target engine;
Obtaining an actually measured tension value of the trolley bracket; the actually measured tension value is a tension value received by the trolley bracket after the target engine is used and is placed on the trolley bracket;
comparing the actually measured tension value with the theoretical tension value to obtain a comparison result;
And controlling the trolley bracket to adjust based on the comparison result so as to detach the thrust pin on the target engine.
Optionally, the comparing the measured tension value with the theoretical tension value to obtain a comparison result includes:
obtaining a first result when the measured tension value is greater than the theoretical tension value; wherein the first result is used to characterize that a head position of the target engine is lower than a tail position;
Obtaining a second result when the measured tension value is equal to the theoretical tension value; wherein the first result is used to characterize that the target engine is located in a horizontal direction;
Obtaining a third result when the measured tension value is less than the theoretical tension value; wherein the third result is used to characterize the target engine with a head position higher than a tail position.
Optionally, the adjusting the trolley bracket based on the comparison result to detach a thrust pin on the target engine includes:
If the first result is obtained, controlling the head of the trolley bracket to be adjusted up or controlling the tail of the trolley bracket to be adjusted down so that the actually measured tension value is equal to the theoretical tension value;
if the third result is obtained, controlling the tail of the trolley bracket to be adjusted up or controlling the head of the trolley bracket to be adjusted down so that the actually measured tension value is equal to the theoretical tension value;
And if the second result is obtained, disassembling the thrust pin on the target engine.
Optionally, a tension sensor is installed at the tail part of the trolley bracket;
the obtaining the measured tension value received by the trolley bracket comprises the following steps:
and obtaining an actually measured tension value received by the trolley bracket through the tension sensor.
Optionally, the obtaining the measured tension value received by the trolley bracket includes:
Obtaining the supporting force born by the supporting hinged support on the trolley bracket;
based on the supporting force of the support hinged support on the trolley bracket, tangential force of the trolley bracket is obtained;
Based on the tangential force received by the trolley bracket, the actually measured tension value received when the head of the trolley bracket is lower than the tail of the trolley bracket is obtained.
Optionally, the obtaining the supporting force of the support hinge base on the trolley bracket includes:
the supporting force born by the supporting hinged support on the trolley bracket is obtained by the following relational expression:
Based on the supporting force that support the free bearing received on the overhead traveling crane bracket, obtain the tangential force that the overhead traveling crane bracket received includes:
the tangential force to which the carriage is subjected is obtained by the following relation:
Based on the tangential force that the overhead traveling crane bracket received, obtain the actual measurement pulling force value that receives when overhead traveling crane bracket head is less than the afterbody, include:
The actually measured tensile force value received when the head part of the trolley bracket is lower than the tail part is obtained through the following relation:
Wherein, F 1 represents the supporting force of the support hinge support on the trolley bracket, F 2y represents the tangential force of the support hinge support, F 2 represents the measured tensile force of the support hinge support, G 0 represents the weight of the engine, L 0 represents the linear distance from the center of gravity of the engine to the support hinge support on the support hinge support, L 4 represents the force arm of the supporting force of the support hinge support on the support hinge support, alpha represents the angle between the connecting line of the center of gravity of the engine and the support hinge support on the support hinge support and the horizontal plane, beta represents the angle between the axis of the engine and the horizontal plane, L 2 represents the distance from the hinge point of the rear pull rod on the support hinge support to the support hinge support, L 3 represents the force arm of the tangential force of the support hinge support, ψ represents the angle between the tension sensor and the horizontal plane, and H represents the initial height of the tension sensor.
Optionally, the acquiring the theoretical tension value of the trolley bracket includes:
the theoretical tension value of the trolley bracket is obtained by the following relation:
Wherein, F '1 represents the supporting force received by the support hinge support when the trolley bracket is positioned in the horizontal direction, and F' 2 represents the theoretical pulling force value received by the trolley bracket.
In a second aspect, an engine thrust pin quick disconnect apparatus, the apparatus comprising:
The acquisition module is used for acquiring a theoretical tension value received by the trolley bracket; when the target engine is not used, the theoretical tension value is horizontally placed on the trolley bracket, so that the trolley bracket receives the tension value; the trolley bracket is used for supporting the target engine;
the first control module is used for controlling the trolley bracket to move to a clearance position between the installation cabin and the target engine so that the trolley bracket supports the target engine;
the first obtaining module is used for obtaining an actually measured tension value received by the trolley bracket; the actually measured tension value is a tension value received by the trolley bracket after the target engine is used and is placed on the trolley bracket;
The second obtaining module is used for comparing the actually measured tension value with the theoretical tension value to obtain a comparison result;
And the second control module is used for controlling the trolley bracket to be adjusted based on the comparison result so as to detach the thrust pin on the target engine.
In a third aspect, the present application provides a computer device comprising a memory and a processor, the memory having stored therein a computer program, the processor executing the computer program to perform the method described in the embodiments.
In a fourth aspect, the present application provides a computer readable storage medium having a computer program stored thereon, the computer program being executed by a processor to implement the method described in the embodiments.
Through the technical scheme, the application has at least the following beneficial effects:
The embodiment of the application provides a method, a device, equipment and a medium for quickly disassembling an engine thrust pin, wherein the method comprises the steps of firstly obtaining a theoretical tension value of a trolley bracket; when the target engine is not used, the theoretical tension value is horizontally placed on the trolley bracket, so that the trolley bracket receives the tension value; the trolley bracket is used for supporting the target engine; then controlling the trolley bracket to move to a clearance position between the installation cabin and the target engine so that the trolley bracket supports the target engine; then obtaining an actually measured tension value of the trolley bracket; the actually measured tension value is a tension value received by the trolley bracket after the target engine is used and is placed on the trolley bracket; comparing the actual measured tension value with the theoretical tension value to obtain a comparison result; and finally, based on the comparison result, controlling the trolley bracket to adjust so as to detach the thrust pin on the target engine. When the thrust pin of the engine is disassembled by the method, the trolley bracket is controlled to be positioned at the lower part of the target engine, the target engine is supported, the actually measured tension value of the trolley bracket is obtained, the theoretical tension value of the target engine in the horizontal direction is obtained, and the thrust pin is not stressed when the target engine is positioned in the horizontal direction. And then comparing the measured tension value with the theoretical tension value, and adjusting the trolley bracket according to the comparison result. Specifically, if the actually measured tension value is smaller than the theoretical tension value, the head position of the target engine is higher than the tail position, and the tail position of the target engine needs to be adjusted to be higher until the head position height of the target engine is basically equal to the tail position height, and when the actually measured tension value is basically equal to the theoretical tension value, the head position height of the target engine and the tail position height can be just reflected to be basically equal; if the measured tension value is greater than the theoretical tension value, the head position of the target engine is lower than the tail position, and the head position of the target engine needs to be adjusted higher until the head position height of the target engine is basically equal to the tail position height. When the head position height of the target engine is substantially equal to the tail position Gao Duji, it means that the thrust pin is not substantially stressed by the engine, and the thrust pin can be removed. That is, since the actual tension value of the bracket supporting the target engine can reflect the tension of the target engine, the tension of the target engine can reflect the stress condition of the thrust pin. And the theoretical tension value and the actual tension value received by the trolley bracket are quantized, so that the obtained theoretical tension value and actual tension value are accurate. Therefore, the stress condition of the thrust pin on the engine can be accurately judged through the quantized actual tension value of the trolley bracket. Because the stress condition that the thrust pin receives the engine can be judged more accurately, the trolley bracket and the target engine can be regulated more accurately, and the target engine can be regulated to the horizontal position more accurately, so that the stress that the thrust pin receives the target engine is smaller, and the thrust pin is less prone to being damaged when being disassembled.
Drawings
FIG. 1 is a schematic diagram of a computer device in a hardware operating environment according to an embodiment of the present application;
FIG. 2 is a flow chart of a method for quickly disassembling an engine thrust pin according to an embodiment of the present application;
FIG. 3 is a diagram illustrating a force analysis of a target engine in a horizontal state according to an embodiment of the present application;
FIG. 4 is a diagram illustrating a force analysis of a target engine with a head position lower than a tail position according to an embodiment of the present application;
FIG. 5 is a flowchart of a specific implementation method of step S12 of the present application;
Fig. 6 is a schematic view of an engine thrust pin quick release device according to an embodiment of the present application.
The achievement of the objects, functional features and advantages of the present application will be further described with reference to the accompanying drawings, in conjunction with the embodiments.
Detailed Description
It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the application.
The manufacturing precision requirement of the engine and the matched parts thereof in the aviation field is high, the engine belongs to a high-value product, and if the engine is improperly operated in the mounting and dismounting processes, the engine is easy to cause larger scrapping loss. When the engine is installed, the end face of the engine is inserted into the engine for connection through the engine thrust pin, after the engine thrust pin enters the installation cabin along with the engine, the thrust pin is pressed by clamping in the installation cabin, and the thrust pin is fixed by two clamping bolts, so that the assembly of the engine in the installation cabin is realized.
The thrust pin is used as a force transmission piece of engine thrust and is in interference fit with the clamping device, so that the surface precision requirement is high. In the subsequent working process, the engine is required to be disassembled due to the arrangement of the airplane, and the state of the engine is inconsistent with the state of the engine under the initial static condition after the engine flies for a plurality of times, so that the stress of the airplane is likely to be born. If the thrust pin is detached without eliminating the stress of the engine, the surface of the thrust pin is easily damaged, and the larger scrapped amount is caused. In the prior art, when the thrust pin on the engine is disassembled, the stress condition of the engine is judged only by the experience of a line of operators, so that the stress condition of the engine is judged inaccurately, and the damage of the thrust pin is easy to cause.
In order to solve the technical problems, the application provides a method, a device, equipment and a medium for quickly disassembling an engine thrust pin, and before the specific technical scheme of the application is introduced, the hardware operation environment related to the scheme of the embodiment of the application is introduced.
Referring to fig. 1, fig. 1 is a schematic diagram of a computer device structure of a hardware running environment according to an embodiment of the present application.
As shown in fig. 1, the computer device may include: a processor 1001, such as a central processing unit (Central Processing Unit, CPU), a communication bus 1002, a user interface 1003, a network interface 1004, a memory 1005. Wherein the communication bus 1002 is used to enable connected communication between these components. The user interface 1003 may include a Display, an input unit such as a Keyboard (Keyboard), and the optional user interface 1003 may further include a standard wired interface, a wireless interface. The network interface 1004 may optionally include a standard wired interface, a wireless interface (e.g., a wireless FIdelity (WI-FI) interface). The Memory 1005 may be a high-speed random access Memory (Random Access Memory, RAM) Memory or a stable Non-Volatile Memory (NVM), such as a disk Memory. The memory 1005 may also optionally be a storage device separate from the processor 1001 described above.
Those skilled in the art will appreciate that the architecture shown in fig. 1 is not limiting of a computer device and may include more or fewer components than shown, or may combine certain components, or a different arrangement of components.
As shown in fig. 1, an operating system, a data storage module, a network communication module, a user interface module, and an electronic program may be included in the memory 1005 as one type of storage medium.
In the computer device shown in fig. 1, the network interface 1004 is mainly used for data communication with a network server; the user interface 1003 is mainly used for data interaction with a user; the processor 1001 and the memory 1005 in the computer device of the present application may be provided in the computer device, where the computer device invokes the engine thrust pin quick disassembly device stored in the memory 1005 through the processor 1001, and executes the engine thrust pin quick disassembly method provided by the embodiment of the present application.
Referring to fig. 2, based on the hardware environment of the foregoing embodiment, an embodiment of the present application provides a method for quickly disassembling an engine thrust pin, including:
S10: obtaining a theoretical tension value of the trolley bracket; when the target engine is not used, the theoretical tension value is horizontally placed on the trolley bracket, so that the trolley bracket receives the tension value; the overhead trolley bracket is used for supporting the target engine.
In particular implementations, the target engine refers to an engine that requires removal of the thrust pin from the engine. The bracket of the trolley is mainly used for supporting the target engine when the target engine is installed or detached; the head of the trolley bracket is provided with two support hinge seats, the two support hinge seats are symmetrically arranged, the tail of the trolley bracket is provided with two rear pull rods which are symmetrically arranged, the upper ends of the rear pull rods are provided with rear pull rod hinge points, and the support hinge seats and the rear pull rod hinge points support the target engine. The target engine is arranged on the trolley bracket horizontally before the installation cabin, and the thrust pin is not stressed by the target engine basically because the target engine is arranged on the trolley bracket horizontally. At this time, as shown in fig. 3, fig. 3 is a schematic diagram illustrating stress analysis when the target engine is in a horizontal state in the embodiment of the present application. In fig. 3, F 1 represents the supporting force applied to the support hinge support when the trolley bracket is positioned in the horizontal direction, F 2 represents the theoretical pulling force applied to the trolley bracket, G 0 represents the weight of the engine, L 0 represents the linear distance from the center of gravity of the engine to the support hinge support on the trolley bracket, L 4 represents the arm of force applied to the support hinge support on the trolley bracket, α represents the angle between the line between the center of gravity of the engine and the support hinge support on the trolley bracket and the horizontal plane, and L 2 represents the distance from the rear pull rod hinge point on the trolley bracket to the support hinge support. According to the geometric relation of the target engine mounted on the trolley bracket, the theoretical tension value of the trolley bracket is obtained through the following relation:
wherein, F' 1 represents the supporting force of the support hinge support when the trolley bracket is located in the horizontal direction (corresponding to F 1),F'2 in fig. 1 represents the theoretical pulling force value of the trolley bracket (corresponding to F 2),G0 in fig. 1, L 0 represents the linear distance from the center of gravity of the engine to the support hinge support on the trolley bracket, L 4 represents the arm of force of the supporting force of the support hinge support on the trolley bracket, α represents the angle between the connecting line of the center of gravity of the engine and the support hinge support on the trolley bracket and the horizontal plane, and L 2 represents the distance from the rear pull rod hinge point on the trolley bracket to the support hinge support).
Because the target engine is a high-quality product, the tension value of the target engine cannot be directly measured on the target engine, the tension value of the bracket of the trolley is converted into the calculated tension value, and the tension value of the target engine can be known according to the force interaction relation, so that the stress of the thrust pin is known.
S11: and controlling the trolley bracket to move to a clearance position between the installation cabin and the target engine so that the trolley bracket supports the target engine.
In the specific implementation process, when the thrust pin arranged on the target engine in the installation cabin is detached, the trolley bracket is controlled to move to a gap between the installation cabin and the target engine in a conventional mode, and then the trolley bracket is controlled to support the target engine, and the target engine is mainly supported through the support hinge seat and the rear pull rod hinge point during support. Thus, the target engine can be conveniently disassembled, and the tension value of the target engine can be obtained indirectly through the trolley bracket.
S12: obtaining an actually measured tension value of the trolley bracket; the actually measured tension value is a tension value received by the trolley bracket after the target engine is used and is placed on the trolley bracket.
In the specific implementation process, two main methods are available for obtaining the measured tension value of the trolley bracket. The first method is to install a tension sensor at the tail of the trolley bracket, and obtain the measured tension value of the trolley bracket through the tension sensor. The pull sensor is a conventional sensor, the model of which can be selected according to actual needs, and the working principle and circuit connection of the pull sensor are also known to those skilled in the art. The tension sensor is used for measuring the tension value received by the trolley bracket in real time, so that the actually measured tension value received by the trolley bracket can be obtained quickly, and the trolley bracket can be adjusted correspondingly more conveniently.
In the second method, as shown in fig. 4 (here, the head position of the engine is lower than the tail position is taken as an example), fig. 4 is a schematic diagram of stress analysis when the head position of the target engine is lower than the tail position in the embodiment of the present application. In fig. 4, F 2y represents the tangential force to which the trolley bracket is subjected, G 0 represents the weight of the engine, L 0 represents the linear distance from the center of gravity of the engine to the support hinge support on the trolley bracket, L 4 represents the arm of force of the support hinge support on the trolley bracket, α represents the angle between the line connecting the center of gravity of the engine and the support hinge support on the trolley bracket and the horizontal plane, β represents the angle between the axis of the engine and the horizontal plane, L 2 represents the distance between the rear tie rod hinge point on the trolley bracket and the support hinge support, L 3 represents the arm of tangential force to which the trolley bracket is subjected, ψ represents the angle between the tension sensor and the horizontal plane, and H represents the initial height of the tension sensor. And obtaining the measured tension value received by the trolley bracket according to the geometric relation of the trolley bracket when supporting the target engine. Specifically, as shown in fig. 5, step S12 includes the steps of:
s121: and obtaining the supporting force born by the supporting hinged support on the trolley bracket.
In the specific implementation process, the supporting force born by the supporting hinged support on the trolley bracket is obtained by the following relational expression:
Wherein, F 1 represents the supporting force on the bracket of the trolley, beta represents the included angle between the axis of the engine and the horizontal plane, and phi represents the included angle between the tension sensor and the horizontal plane.
S122: and obtaining tangential force received by the trolley bracket based on the supporting force received by the support hinged support on the trolley bracket.
In the specific implementation process, the tangential force suffered by the trolley bracket is obtained through the following relation:
Wherein, F 2y represents the tangential force that the overhead traveling crane bracket receives, L 3 represents the arm of force of the tangential force that the overhead traveling crane bracket receives.
S123: based on the tangential force received by the trolley bracket, the actually measured tension value received when the head of the trolley bracket is lower than the tail of the trolley bracket is obtained.
In the specific implementation process, the actually measured tensile force value received when the head part of the trolley bracket is lower than the tail part is obtained through the following relation:
wherein F 2 represents the measured tension value received by the trolley bracket, and H represents the initial height of the tension sensor.
The measured tension value of the trolley bracket, which is obtained through the geometric relationship, is more accurate, and the obtained measured tension can be compared with the measured tension obtained by the tension sensor so as to be used as a reference for the measured tension obtained by the tension sensor.
S13: and comparing the actually measured tension value with the theoretical tension value to obtain a comparison result.
In the specific implementation process, the comparison of the measured tension value and the theoretical tension value can generate the following three conditions: firstly, under the condition that the measured tension value is larger than the theoretical tension value, a first result is obtained; wherein the first result is used to characterize that a head position of the target engine is lower than a tail position. Secondly, under the condition that the measured tension value is equal to the theoretical tension value, a second result is obtained; wherein the first result is used to characterize the target engine as being in a horizontal direction. Thirdly, under the condition that the actual measurement tension value is smaller than the theoretical tension value, a third result is obtained; wherein the third result is used to characterize the target engine with a head position higher than a tail position.
Therefore, the stress condition of the thrust pin is converted into the tension condition of the target engine, the tension condition of the target engine is converted into the tension condition of the trolley bracket, and the stress condition of the thrust pin can be more intuitively reflected by quantifying and comparing the theoretical tension condition and the actually measured tension condition of the trolley bracket, and the thrust pin is detached according to the stress condition of the thrust pin.
S14: and controlling the trolley bracket to adjust based on the comparison result so as to detach the thrust pin on the target engine.
In the specific implementation process, the trolley bracket is adjusted according to the three comparison results in the step S13, and finally the purpose of detaching the thrust pin from the target engine without damage is achieved. Wherein, the mode of adjusting the trolley bracket comprises manual adjustment or program control. Specifically, if the first result is obtained, controlling the head of the trolley bracket to be adjusted up or controlling the tail of the trolley bracket to be adjusted down so that the actually measured tension value is equal to the theoretical tension value; if the third result is obtained, controlling the tail of the trolley bracket to be adjusted up or controlling the head of the trolley bracket to be adjusted down so that the actually measured tension value is equal to the theoretical tension value; and if the second result is obtained, disassembling the thrust pin on the target engine.
In this embodiment, the actually measured tension value and the theoretical tension value are compared, if the actually measured tension value is greater than the theoretical tension value, the head position of the target engine is indicated to be lower than the tail position, the times need to control the head of the trolley bracket to be heightened or control the tail of the trolley bracket to be lowered, and finally the trolley bracket is basically in the horizontal position. If the measured tension value is smaller than the theoretical tension value, the head position of the target engine is higher than the tail position, at the moment, the head of the trolley bracket needs to be controlled to be lowered or the tail of the trolley bracket needs to be controlled to be raised, and finally the trolley bracket is basically in the horizontal position. If the measured tension value is equal to the theoretical tension value, the head position and the tail position of the target engine are basically the same, namely the target engine is in a horizontal position. When the carriage is in the horizontal position, the target engine is also in the horizontal position, and when the target engine is in the horizontal position, the thrust pin is substantially not stressed by the target engine. At this time, the thrust pin is detached from the target engine, and damage to the thrust pin is not easily caused.
Therefore, the application firstly moves the bracket of the mounting vehicle on the gesture adjusting platform to the gap position between the target engine and the engine mounting cabin, so that the interface of the arc-shaped support hinged support on the bracket of the mounting vehicle is fully contacted with the supporting point of the engine, and the tension sensor arranged at the tail end of the bracket of the mounting vehicle can detect the actual weight borne by the bracket in real time through the gesture adjusting of the platform; then, according to the actual measurement value of the tension sensor and the theoretical value in the installation vehicle system, the posture (head-up/head-down) of the current target engine is found, the posture of the target engine is adjusted through the posture adjusting mechanism of the installation vehicle, and when the actual measurement value of the tension sensor is equal to the theoretical value in the installation vehicle system, the engine is in a horizontal position, namely in a stress-free state; and finally, the operator removes the rear end and the front end of the engine to clamp the fixed point, removes the thrust pin of the engine, and orderly withdraws the engine from the installation cabin. Therefore, the quick disassembly of the thrust pin of the engine can be realized, and the scrapping loss caused by the disassembly of the thrust pin of the engine with stress is avoided. The application breaks through the bottleneck that the disassembly of the thrust pin of the current engine depends on the experience of operators, quantifies the stress value of the thrust pin of the engine before the disassembly, eliminates the stress of the thrust pin of the engine and the installation cabin through the posture adjustment of degrees of freedom such as pitching, rolling and lifting of the installation platform, ensures the stress-free disassembly of the thrust pin, and reduces the risk of the surface crush injury of the thrust pin. The state of the target engine can be clearly judged by quantifying the stress value of the engine, the dependence on experience of skilled personnel is reduced, the posture adjustment time for disassembling the thrust pin of the target engine is greatly saved, meanwhile, the target engine can be effectively prevented from being disassembled with stress, the disassembly quality is improved, and the method has a strong practical application value.
In summary, since the actual tension value of the bracket supporting the target engine can reflect the tension of the target engine, the tension of the target engine can reflect the stress condition of the thrust pin. And the theoretical tension value and the actual tension value received by the trolley bracket are quantized, so that the obtained theoretical tension value and actual tension value are accurate. Therefore, the stress condition of the thrust pin on the engine can be accurately judged through the quantized actual tension value of the trolley bracket. Because the stress condition that the thrust pin receives the engine can be judged more accurately, the trolley bracket and the target engine can be regulated more accurately, and the target engine can be regulated to the horizontal position more accurately, so that the stress that the thrust pin receives the target engine is smaller, and the thrust pin is less prone to being damaged when being disassembled.
In another embodiment, as shown in fig. 6, based on the same inventive concept as the previous embodiment, an embodiment of the present application further provides a quick-release device for an engine thrust pin, including:
The acquisition module is used for acquiring a theoretical tension value received by the trolley bracket; when the target engine is not used, the theoretical tension value is horizontally placed on the trolley bracket, so that the trolley bracket receives the tension value; the trolley bracket is used for supporting the target engine;
the first control module is used for controlling the trolley bracket to move to a clearance position between the installation cabin and the target engine so that the trolley bracket supports the target engine;
the first obtaining module is used for obtaining an actually measured tension value received by the trolley bracket; the actually measured tension value is a tension value received by the trolley bracket after the target engine is used and is placed on the trolley bracket;
The second obtaining module is used for comparing the actually measured tension value with the theoretical tension value to obtain a comparison result;
And the second control module is used for controlling the trolley bracket to be adjusted based on the comparison result so as to detach the thrust pin on the target engine.
It should be noted that, each module in the quick disassembly device for an engine thrust pin in this embodiment corresponds to each step in the quick disassembly method for an engine thrust pin in the foregoing embodiment one by one, so the specific implementation manner and the achieved technical effect of this embodiment may refer to the implementation manner of the quick disassembly method for an engine thrust pin, and will not be described herein again.
Furthermore, in an embodiment, the present application also provides a computer device, which includes a processor, a memory, and a computer program stored in the memory, which when executed by the processor, implements the method in the foregoing embodiment.
Furthermore, in an embodiment, the present application also provides a computer storage medium, on which a computer program is stored, which computer program, when being executed by a processor, implements the method in the previous embodiment.
In some embodiments, the computer readable storage medium may be FRAM, ROM, PROM, EPROM, EEPROM, flash memory, magnetic surface memory, optical disk, or CD-ROM; but may be a variety of devices including one or any combination of the above memories. The computer may be a variety of computing devices including smart terminals and servers.
In some embodiments, the executable instructions may be in the form of programs, software modules, scripts, or code, written in any form of programming language (including compiled or interpreted languages, or declarative or procedural languages), and they may be deployed in any form, including as stand-alone programs or as modules, components, subroutines, or other units suitable for use in a computing environment.
As an example, executable instructions may, but need not, correspond to files in a file system, may be stored as part of a file that holds other programs or data, such as in one or more scripts in a hypertext markup language (HTML, hyper Text Markup Language) document, in a single file dedicated to the program in question, or in multiple coordinated files (e.g., files that store one or more modules, sub-programs, or portions of code).
As an example, executable instructions may be deployed to be executed on one computing device or on multiple computing devices located at one site or distributed across multiple sites and interconnected by a communication network.
It should be noted that, in this document, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or system that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or system. Without further limitation, an element defined by the phrase "comprising one … …" does not exclude the presence of other like elements in a process, method, article, or system that comprises the element.
The foregoing embodiment numbers of the present application are merely for the purpose of description, and do not represent the advantages or disadvantages of the embodiments.
From the above description of the embodiments, it will be clear to those skilled in the art that the above-described embodiment method may be implemented by means of software plus a necessary general hardware platform, but of course may also be implemented by means of hardware, but in many cases the former is a preferred embodiment. Based on such understanding, the technical solution of the present application may be embodied essentially or in a part contributing to the prior art in the form of a software product stored in a storage medium (e.g. read-only memory/random-access memory, magnetic disk, optical disk), comprising instructions for causing a multimedia terminal device (which may be a mobile phone, a computer, a television receiver, or a network device, etc.) to perform the method according to the embodiments of the present application.
The foregoing description is only of the preferred embodiments of the present application, and is not intended to limit the scope of the application, but rather is intended to cover any equivalents of the structures or equivalent processes disclosed herein or in the alternative, which may be employed directly or indirectly in other related arts.
Claims (8)
1. A method for quickly disassembling an engine thrust pin, the method comprising:
Obtaining a theoretical tension value of the trolley bracket; when the target engine is not used, the theoretical tension value is horizontally placed on the trolley bracket, so that the trolley bracket receives the tension value; the trolley bracket is used for supporting the target engine;
Controlling the trolley bracket to move to a clearance position between the installation cabin and the target engine so that the trolley bracket supports the target engine;
Obtaining an actually measured tension value of the trolley bracket; the actually measured tension value is a tension value received by the trolley bracket after the target engine is used and is placed on the trolley bracket;
comparing the actually measured tension value with the theoretical tension value to obtain a comparison result;
Based on the comparison result, controlling the trolley bracket to adjust so as to detach a thrust pin on the target engine;
The comparing of the actually measured tension value with the theoretical tension value to obtain a comparison result comprises the following steps:
obtaining a first result when the measured tension value is greater than the theoretical tension value; wherein the first result is used to characterize that a head position of the target engine is lower than a tail position;
Obtaining a second result when the measured tension value is equal to the theoretical tension value; wherein the second result is used to characterize the target engine in a horizontal direction;
obtaining a third result when the measured tension value is less than the theoretical tension value; wherein the third result is used to characterize the head position of the target engine as higher than the tail position;
based on the comparison, adjust the overhead traveling crane bracket to dismantle the thrust pin on the target engine, include:
If the first result is obtained, controlling the head of the trolley bracket to be adjusted up or controlling the tail of the trolley bracket to be adjusted down so that the actually measured tension value is equal to the theoretical tension value;
if the third result is obtained, controlling the tail of the trolley bracket to be adjusted up or controlling the head of the trolley bracket to be adjusted down so that the actually measured tension value is equal to the theoretical tension value;
And if the second result is obtained, disassembling the thrust pin on the target engine.
2. The quick engine thrust pin removal method of claim 1, wherein a tension sensor is mounted at the tail of the trolley bracket;
the obtaining the measured tension value received by the trolley bracket comprises the following steps:
and obtaining an actually measured tension value received by the trolley bracket through the tension sensor.
3. The method of claim 1, wherein said obtaining a measured tension value to which said carriage is subjected comprises:
Obtaining the supporting force born by the supporting hinged support on the trolley bracket;
based on the supporting force of the support hinged support on the trolley bracket, tangential force of the trolley bracket is obtained;
Based on the tangential force received by the trolley bracket, the actually measured tension value received when the head of the trolley bracket is lower than the tail of the trolley bracket is obtained.
4. The method of claim 1, wherein said obtaining the supporting force received by the support hinge base on the carriage comprises:
the supporting force born by the supporting hinged support on the trolley bracket is obtained by the following relational expression:
Based on the supporting force that support the free bearing received on the overhead traveling crane bracket, obtain the tangential force that the overhead traveling crane bracket received includes:
the tangential force to which the carriage is subjected is obtained by the following relation:
Based on the tangential force that the overhead traveling crane bracket received, obtain the actual measurement pulling force value that receives when overhead traveling crane bracket head is less than the afterbody, include:
The actually measured tensile force value received when the head part of the trolley bracket is lower than the tail part is obtained through the following relation:
Wherein F 1 represents the supporting force applied to the support hinged support on the trolley bracket, The tangential force of the bracket of the trolley is shown, F 2 shows the measured tension value of the bracket of the trolley, G 0 shows the weight of the engine, L 0 shows the linear distance from the center of gravity of the engine to the support hinged support on the bracket of the trolley, L 4 shows the arm of force of the support hinged support on the bracket of the trolley, and IRepresents the included angle between the connecting line of the gravity center of the engine and the supporting hinged support on the trolley bracket and the horizontal plane, beta represents the included angle between the axis of the engine and the horizontal plane, L 2 represents the distance between the hinge point of the rear pull rod on the trolley bracket and the supporting hinged support, L 3 represents the arm of force of tangential force applied to the trolley bracket,Indicating the angle between the tension sensor and the horizontal plane, and H indicating the initial height of the tension sensor.
5. The method for quickly disassembling an engine thrust pin according to claim 4, wherein the obtaining a theoretical tension value to which the carriage is subjected comprises:
the theoretical tension value of the trolley bracket is obtained by the following relation:
Wherein, Representing the supporting force born by the supporting hinged support when the trolley bracket is positioned in the horizontal direction,/>Indicating the theoretical tension value to which the carriage is subjected.
6. An engine thrust pin quick disconnect apparatus for carrying out the engine thrust pin quick disconnect method of any one of claims 1-5, said apparatus comprising:
The acquisition module is used for acquiring a theoretical tension value received by the trolley bracket; when the target engine is not used, the theoretical tension value is horizontally placed on the trolley bracket, so that the trolley bracket receives the tension value; the trolley bracket is used for supporting the target engine;
the first control module is used for controlling the trolley bracket to move to a clearance position between the installation cabin and the target engine so that the trolley bracket supports the target engine;
the first obtaining module is used for obtaining an actually measured tension value received by the trolley bracket; the actually measured tension value is a tension value received by the trolley bracket after the target engine is used and is placed on the trolley bracket;
The second obtaining module is used for comparing the actually measured tension value with the theoretical tension value to obtain a comparison result;
And the second control module is used for controlling the trolley bracket to be adjusted based on the comparison result so as to detach the thrust pin on the target engine.
7. A computer device, characterized in that it comprises a memory in which a computer program is stored and a processor which executes the computer program, implementing the method according to any of claims 1-5.
8. A computer readable storage medium, having stored thereon a computer program, the computer program being executable by a processor to implement the method of any of claims 1-5.
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| CN202210984299.3A CN115416871B (en) | 2022-08-17 | 2022-08-17 | Method, device, equipment and medium for quickly disassembling thrust pin of engine |
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