CN213022200U

CN213022200U - Missile area moment test equipment

Info

Publication number: CN213022200U
Application number: CN202021078501.9U
Authority: CN
Inventors: 曹隽
Original assignee: Shanghai Wangqing Automation Technology Co ltd
Current assignee: Shanghai Wangqing Automation Technology Co ltd
Priority date: 2020-06-12
Filing date: 2020-06-12
Publication date: 2021-04-20
Anticipated expiration: 2030-06-12

Abstract

The utility model discloses a guided missile bullet area moment test equipment, include: operation platform, rotating electrical machines, support, chuck, clamp dress structure and gyro wheel frame, support fixed mounting in on the operation platform wall, just the support is located operation platform one end, rotating electrical machines with support one side fixed connection, the utility model relates to a bullet area moment test technical field, this missile bullet area moment test equipment reasonable in design, the simple operation of being convenient for of application method, through the record to the state behind the missile bullet area atress to judge the testing result, thereby improve current operating condition, improve the quality and the efficiency that the product detected, through increasing process control and information-based means, realize closing up process data's collection, bind, the record is uploaded, improve the quality and the efficiency that the missile detected simultaneously, reduce manual work intensity of labour, reduce the influence of human factor to testing process.

Description

Missile area moment test equipment

Technical Field

The utility model relates to a bullet area moment test technical field specifically is a guided missile bullet area moment test equipment.

Background

The test of the moment of the missile belt is taken as an important test in the missile assembling process, the existing production mode is relatively laggard, the detection work on site is mostly finished manually, the detection process and the precision are both determined by site operators according to the past experience, according to the original detection requirements of products, the manual efficiency is not high and the detection precision is difficult to ensure, so that a novel detection device for automatically and accurately detecting the moment of a missile belt is provided, after the missile is loaded and clamped, can automatically complete the detection of the missile cartridge according to the preset program and the end condition, and take pictures or record videos of key steps in the process, the collected information is automatically uploaded, processed and analyzed, a data statistics report and batch quality consistency result analysis are formed, manual participation is not needed in the whole process, the accuracy and reliability of detection results are guaranteed, and the method has great significance for improving the efficiency and quality of product assembly.

SUMMERY OF THE UTILITY MODEL

To prior art's not enough, the utility model provides a guided missile bullet area moment test equipment through the record to guided missile bullet area atress back state to judge the testing result, thereby improve current operating condition, improve the quality and the efficiency that the product detected, solved the problem of mentioning in the above background art.

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a missile belt moment test device mainly comprises: the device comprises an operating platform, a rotating motor, a bracket, a chuck, a clamping structure and a roller frame;

support fixed mounting in on the operation platform wall, just the support is located operation platform one end, the rotating electrical machines with support one side fixed connection, just the rotating electrical machines drive end extends to inside the support, so the chuck set up in the support opposite side, just the chuck with rotating electrical machines drive end fixed connection, be provided with the work piece on the chuck, press from both sides dress structure fixed mounting in on the operation platform wall, just press from both sides dress structure with the laminating of work piece outside wall mutually, gyro wheel frame fixed mounting in on the operation platform wall, just the gyro wheel frame is located the operation platform other end, the gyro wheel frame with work piece one end is laminated mutually, the operation platform bottom is provided with the support frame.

Preferably, the clip fitting structure includes: the fixture comprises a fixing frame, a cylinder, a clamp, a sensor and a threaded component;

the fixture is fixedly connected with the upper wall surface of the operating platform, the fixture is fixedly installed on the fixture, the fixture is sleeved on the workpiece, the cylinder is fixedly installed on the upper wall surface of the operating platform and is located on one side of the fixture, the top end of the cylinder is connected with the fixture, the thread assembly is arranged on the fixture, the sensor is arranged inside the fixture, and the sensor is attached to the workpiece.

Preferably, a display panel is arranged on the operating platform and is positioned on the upper wall surface of the operating platform.

Preferably, the operation platform is provided with a first warning light and a second warning light on the upper wall surface, and the first warning light and the second warning light are both located on one side of the display panel.

Preferably, a base is arranged at the joint of the rotating motor and the operating platform, and a screw is arranged at the joint of the base and the operating platform.

Advantageous effects

The utility model provides a guided missile bullet area moment test equipment possesses following beneficial effect: the missile belt torque testing equipment is reasonable in design, the using method is simple and convenient to operate, the existing operation conditions are improved by recording the state of the missile belt after stress, and the detection result is judged, so that the quality and the efficiency of product detection are improved, the collection, binding and record uploading of closing-up process data are realized by adding process control and informatization means, the quality and the efficiency of missile detection are improved, the labor intensity of manual operation is reduced, and the influence of human factors on the detection process is reduced.

Drawings

Fig. 1 is a front view of a missile belt torque testing device according to the present invention;

fig. 2 is a top view of the missile belt torque testing device of the present invention;

fig. 3 is a schematic view of an embodiment of the present invention.

In the figure: 1. an operating platform; 2. a rotating electric machine; 3. a support; 4. a chuck; 5. a clamping structure; 501. a fixed mount; 502. a cylinder; 503. a clamp; 504. a sensor; 505. a threaded assembly; 6. a roller frame; 7. a workpiece; 8. a display panel; 9. a first warning light; 10. a second warning light; 11. a base.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative work belong to the protection scope of the present invention based on the embodiments of the present invention.

All the electrical components in the present application are connected with the power supply adapted to the electrical components through a wire, and an appropriate controller and an appropriate encoder should be selected according to actual conditions to meet control requirements, and specific connection and control sequences should be obtained.

Example (b): the utility model provides a technical scheme: as can be known from the attached figures 1-3 of the specification, the missile belt moment testing equipment mainly comprises: the operation platform 1, the rotating motor 2, the bracket 3, the chuck 4, the clamping structure 5 and the roller frame 6 are connected as follows:

the support 3 is fixedly arranged on the upper wall surface of the operation platform 1, the support 3 is positioned at one end of the operation platform 1, the rotating motor 2 is fixedly connected with one side of the support 3, and the driving end of the rotating motor 2 extends into the support 3, so that the chuck 4 is arranged at the other side of the support 3, the chuck 4 is fixedly connected with the driving end of the rotating motor 2, a workpiece 7 is arranged on the chuck 4, the clamping structure 5 is fixedly arranged on the upper wall surface of the operation platform 1, the clamping structure 5 is attached to the outer side wall surface of the workpiece 7, the roller frame 6 is fixedly arranged on the upper wall surface of the operation platform 1, the roller frame 6 is positioned at the other end of the operation platform 1, the roller frame 6 is attached to one end of the.

According to the situation, when the clamping device is used, the support 3 and the clamping structure 5 are fixedly supported through the operating platform 1, the chuck 4 is started, the bottom end of the workpiece 7 is fixed through the chuck 4, the rotating motor 2 is started, the chuck 4 and the workpiece 7 are driven to rotate through the rotation of the rotating motor 2, the workpiece 7 is supported through the clamping structure 5, and meanwhile, the elastic belt moment of the workpiece is detected.

Preferably, the clip structure 5 further includes: a fixed frame 501, a cylinder 502, a clamp 503, a sensor 504 and a thread component 505;

the fixing frame 501 is fixedly connected with the upper wall surface of the operating platform 1, the clamp 503 is fixedly installed on the fixing frame 501, the clamp 503 is sleeved on the workpiece 7, the cylinder 502 is fixedly installed on the upper wall surface of the operating platform 1, the cylinder 502 is located on one side of the fixing frame 501, the top end of the cylinder 502 is connected with the clamp 503, the threaded component 505 is arranged on the clamp 503, the sensor 504 is arranged inside the clamp 503, and the sensor 504 is attached to the workpiece 7.

As can be seen from the above, when the elastic belt is used, the clamp 503 is supported by the fixing frame 501, the tightness of the clamp 503 is controlled by the air cylinder 502, and the elastic belt moment is detected by the sensor 504.

Preferably, a display panel 8 is further disposed on the operation platform 1, and the display panel 8 is located on an upper wall surface of the operation platform 1.

As a preferred scheme, furthermore, a first warning light 9 and a second warning light 10 are arranged on the upper wall surface of the operation platform 1, and the first warning light 9 and the second warning light 10 are both located on one side of the display panel 8, wherein the first warning light 9 is a red light, and the second warning light 10 is a green light.

Preferably, a base 11 is disposed at a connection position of the rotating electrical machine 2 and the operation platform 1, and a screw is disposed at a connection position of the base 11 and the operation platform 1.

According to the general situation, when the belt feeder is used, according to the requirements of a production process, whether the belt feeder moment is qualified or not is detected: the automatic application of 0.02 Kgf.M moment, the alarm of the elastic belt turning to the red light, the passing of the green light and the automatic application of 0.4 Kgf.M moment on the elastic belt test ring can ensure that the elastic belt can slightly rotate and can not stop in the midway.

Equipment and instrument requirements: automatically clamping the closed missile on an assembly fixture in a horizontal position, automatically clamping a missile belt testing ring on a single belt seat, and arranging a missile belt torque tester at a station, wherein the torque is 0-1 Kgf.M, and the precision is 0.1 Kgf.M.

Assembly correctness: the working position should collect pictures locked by the locking clamp, pictures of correct installation of the belt test ring, pictures of static and rotating of the belt under load and dynamic videos, and pictures of the belt gasket and the belt picture, wherein the holes on the spiral ring are aligned with the holes on the speed-increasing engine body.

Informatization requirements: the collected information is automatically uploaded, processed and analyzed to form a graphic data statistical report, a test result report and a batch consistency result analysis report.

Problems that easily occur in the detection process: crushing, breaking the elastic band washer and bruising the elastic band.

It is to be noted that, in this document, relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action, without necessarily requiring or implying any such actual relationship or order between such entities or operations, furthermore, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements, but also includes other elements not expressly listed or inherent to such process, method, article, or apparatus, without further limitation, an element defined by the phrase "comprising one.. may, it does not exclude the presence of additional identical elements in a process, method, article or apparatus that comprises a said element.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a guided missile bullet area moment test equipment which characterized in that mainly includes: the device comprises an operating platform (1), a rotating motor (2), a bracket (3), a chuck (4), a clamping structure (5) and a roller frame (6);

the support (3) is fixedly installed on the upper wall surface of the operation platform (1), the support (3) is located at one end of the operation platform (1), the rotating motor (2) is fixedly connected with one side of the support (3), the driving end of the rotating motor (2) extends into the support (3), so that the chuck (4) is arranged at the other side of the support (3), the chuck (4) is fixedly connected with the driving end of the rotating motor (2), a workpiece (7) is arranged on the chuck (4), the clamping structure (5) is fixedly installed on the upper wall surface of the operation platform (1), the clamping structure (5) is attached to the outer side wall surface of the workpiece (7), the roller frame (6) is fixedly installed on the upper wall surface of the operation platform (1), and the roller frame (6) is located at the other end of the operation platform (1), the roller carrier (6) is attached to one end of the workpiece (7), and a support frame is arranged at the bottom end of the operating platform (1).

2. Missile belt torque test equipment according to claim 1, characterized in that the clamping structure (5) comprises: the device comprises a fixed frame (501), a cylinder (502), a clamp (503), a sensor (504) and a threaded component (505);

mount (501) with operation platform (1) wall fixed connection, anchor clamps (503) fixed mounting in on mount (501), just anchor clamps (503) cover is located on work piece (7), cylinder (502) fixed mounting in on operation platform (1) the wall, just cylinder (502) are located mount (501) one side, cylinder (502) top with anchor clamps (503) are connected, threaded component (505) set up in on anchor clamps (503), sensor (504) set up in inside anchor clamps (503), just sensor (504) with work piece (7) are laminated mutually.

3. The missile belt moment testing device of claim 1, wherein a display panel (8) is arranged on the operating platform (1), and the display panel (8) is positioned on the upper wall surface of the operating platform (1).

4. The missile belt moment testing equipment of claim 3, wherein a first warning lamp (9) and a second warning lamp (10) are arranged on the upper wall surface of the operating platform (1), and the first warning lamp (9) and the second warning lamp (10) are both positioned on one side of the display panel (8).

5. Missile belt moment test equipment according to claim 1, wherein a base (11) is arranged at the joint of the rotating motor (2) and the operating platform (1), and a screw is arranged at the joint of the base (11) and the operating platform (1).