CN206813318U - A kind of aircraft air propeller - Google Patents
A kind of aircraft air propeller Download PDFInfo
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- CN206813318U CN206813318U CN201720704048.XU CN201720704048U CN206813318U CN 206813318 U CN206813318 U CN 206813318U CN 201720704048 U CN201720704048 U CN 201720704048U CN 206813318 U CN206813318 U CN 206813318U
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- fuselage
- screw mechanism
- propeller
- aircraft air
- aircraft
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Abstract
The utility model discloses a kind of aircraft air propeller, including fuselage, above push away screw mechanism, preceding push away screw mechanism, wing and propeller control system.The rear and front end that fuselage is installed in and above pushes away screw mechanism, push away the left and right sides that screw mechanism is installed in fuselage, the waist is provided with cabin, and the wing is on fuselage before described.The propeller control system includes the middle control main frame in cabin and the dynamical system, control module, laser ranging controller and the center dynamic balance system that are electrically connected with middle control main frame, the control module is electrically connected with dynamical system, self balancing device and remote control, the dynamical system is electrically connected with lifting force system and advance propulsion system, the screw mechanism that above pushes away is controlled by the lifting force system, and screw mechanism is pushed away before described and is controlled by the advance propulsion system.A kind of aircraft air propeller of the utility model has the advantages of simple to operate, easy to use and security performance is high.
Description
Technical field
The present invention relates to vehicle technology field, and in particular to a kind of aircraft air propeller.
Background technology
The mankind have the ideal flown in the air as birds very early.For a long time, the mankind are most for the fantasy that can fly up into the sky
Various methods.With the continuous development of scientific technology, the dream that the mankind fly in the air becomes reality.It is existing most of
Aircraft is mainly used in scientific research, and cost is sufficiently expensive, is not particularly suited for masses, and needs to stop in the large-scale place such as airport
Put, it is suppressed that the consumption of most people, while existing aircraft operation when due to more complicated, it is therefore desirable to Special Training
It could drive, therefore, urgent need offer is a kind of simple to operate, and the aircraft that security performance is high.
The content of the invention
For above-mentioned deficiency, it is an object of the present invention to provide a kind of aircraft air propeller, and it has operation letter
Singly, the advantages of easy to use and security performance is high.
To achieve the above object, technical scheme provided by the present invention is：
A kind of aircraft air propeller, including fuselage, above push away screw mechanism, preceding push away screw mechanism, wing and propulsion
Device control system.The rear and front end for above pushing away screw mechanism and being installed in fuselage, pushes away screw mechanism before described and is installed in fuselage
The left and right sides, the waist are provided with cabin, and the wing is on fuselage.The propeller control system includes being located at machine
Middle control main frame in cabin and the dynamical system being electrically connected with middle control main frame, control module, laser ranging controller and in it is aroused in interest
Balance system, the control module are electrically connected with dynamical system, self balancing device and remote control, and the dynamical system is electrical
Lifting force system and advance propulsion system are connected with, the screw mechanism that above pushes away is controlled by the lifting force system, before described
Screw mechanism is pushed away to control by the advance propulsion system.
As a further improvement, it is described above push away screw mechanism be arranged at fuselage rear and front end above push away propeller blade.
As a further improvement, it is to push away propeller blade before being arranged at fuselage left and right ends that screw mechanism is pushed away before described, institute
Stating advance propulsion system includes course changing control module, and the left and right directions for pushing away propeller blade before control, which is adjusted, realizes steering work(
Energy.
As a further improvement, the self balancing device is gyroscope and controlled by control module, aircraft is improved
Balanced capacity.
As a further improvement, the fuselage uses carbon fiber and aluminium alloy, it can effectively mitigate fuselage weight.
As a further improvement, the dynamical system is driven using battery electric power.
As a further improvement, the dynamical system is driven using gasoline engine.
Beneficial effects of the present invention are：
A kind of aircraft of the utility model with air propeller using when by lifting force system control above push away screw mechanism
Rotate, aircraft, which is risen to after certain altitude, controls advance propulsion system to be pushed away before opening before screw mechanism rotates and realize aircraft
Enter, while turning function is realized in the left and right directions regulation that propeller blade is pushed away before being controlled by course changing control module, operator can
Lifting, advance and steering operation are completed in distribution, make the aircraft operation simpler, while the laser ranging controller, center
The setting of dynamic balance system and self balancing device, improve security performance of the present utility model.
Below in conjunction with the accompanying drawings with embodiment, the present invention is further described.
Brief description of the drawings
Accompanying drawing is for providing a further understanding of the present invention, and a part for constitution instruction, with following tool
Body embodiment is used to explain the present invention together, but is not construed as limiting the invention.In the accompanying drawings：
Fig. 1 is a kind of structural representation of aircraft air propeller of the present invention.
Fig. 2 is the theory diagram of propeller control system of the present utility model.
Each description of reference numerals is as follows in figure.
Fuselage -1, above push away screw mechanism -2, preceding push away screw mechanism -3, wing -4, cabin -5.
Embodiment
To describe the technology contents of the present invention, construction feature, the objects and the effects in detail, below in conjunction with embodiment
And accompanying drawing is coordinated to be explained in detail.
Technical scheme is clearly and completely described below in conjunction with accompanying drawing, it is clear that described implementation
Example is part of the embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, ordinary skill
The every other embodiment that personnel are obtained under the premise of creative work is not made, belongs to the scope of protection of the invention.
In the description of the invention, it is necessary to explanation, term " " center ", " on ", " under ", "left", "right", " vertical ", " level ",
The orientation or position relationship of the instructions such as " interior ", " outer " are based on orientation shown in the drawings or position relationship, are for only for ease of and retouch
State the present invention and simplify description, rather than indicate or imply that signified device or element there must be specific orientation, with specific
Azimuth configuration and operation, therefore be not considered as limiting the invention.
Refer to Fig. 1 and Fig. 2, a kind of aircraft air propeller, including fuselage 1, above push away screw mechanism 2, preceding push away spiral shell
Revolve mechanism 3, wing 4 and propeller control system.The rear and front end for above pushing away screw mechanism 2 and being installed in fuselage 1, it is aircraft
Raising and lowering power is provided, the left and right sides that screw mechanism 3 is installed in fuselage 1 is pushed away before described, is carried for the advance of aircraft
For power.The middle part of fuselage 1 is provided with cabin 5, and operator takes manipulation, and the wing 4 is on fuselage 1.The propeller
Control system includes the middle control main frame in cabin 5 and the dynamical system being electrically connected with middle control main frame, control module, laser
Ranging controller and center dynamic balance system, the control module are electrically connected with dynamical system, self balancing device and remote control dress
Put, the setting of the remote control can make aircraft of the present utility model serve as unmanned plane use by remote control control.Institute
State dynamical system and be electrically connected with lifting force system and advance propulsion system, the screw mechanism 2 that above pushes away passes through the lifting force
System is controlled, and screw mechanism 3 is pushed away before described and is controlled by the advance propulsion system.
In the present embodiment, it is described above push away screw mechanism 2 be arranged at the rear and front end of fuselage 1 above push away propeller blade, and
Above push away propeller blade to drive by motor, and rotated by lifting force system controlled motor and control the rotation for above pushing away propeller blade
Speed.
In the present embodiment, screw mechanism 3 is pushed away before described to push away propeller blade before being arranged at the left and right ends of fuselage 1, and
Propeller blade is pushed away before this to drive by motor, and pushes away propeller blade before rotating i.e. control by advance propulsion system controlled motor
Rotating speed.The advance propulsion system includes course changing control module, and the left and right directions for pushing away propeller blade before control, which is adjusted, to be realized
Turning function.
In the present embodiment, the self balancing device is gyroscope and controlled by control module, improves aircraft
Balanced capacity, ensure that the security performance of aircraft.
In the present embodiment, the fuselage 1 uses carbon fiber and aluminium alloy, can effectively mitigate fuselage weight.
In the present embodiment, the dynamical system is driven using battery electric power.
In the present embodiment, the dynamical system is driven using gasoline engine.
During utility model works：First, hollow main frame is opened, and dynamical system is opened by control module, by upper
Push system control above pushes away screw mechanism 2 and rotated, and aircraft controls advance propulsion system to be pushed away before opening after rising to certain altitude
Screw mechanism 3, which rotates, realizes that aircraft advances, while the left and right directions of propeller blade is pushed away before being controlled by course changing control module
Turning function is realized in regulation.After arriving at, advance propulsion system is closed, and gradually reduced by lifting force system and above push away spiral shell
The thrust of mechanism 2 is revolved, ground is slowly dropped to, is then shut off dynamical system.Wherein, the laser ranging controller is used to control
Aircraft is awing not above safe altitude, and then improves the safety coefficient of aircraft, the center dynamic balance system
Adjustable lower load-bearing is always maintained at center, improves dynamic balancing ability of the aircraft in running, further improves safety coefficient.
In summary, a kind of aircraft of the utility model with air propeller using when by lifting force system control above push away
Screw mechanism 2 rotates, and aircraft controls advance propulsion system to push away the rotation realization of screw mechanism 3 before opening after rising to certain altitude
Aircraft advances, while turning function is realized in the left and right directions regulation that propeller blade is pushed away before being controlled by course changing control module,
Operator can be distributed completion lifting, advance and steering operation, make the aircraft operation simpler, while the laser ranging controls
The setting of instrument, center dynamic balance system and self balancing device, improve security performance of the present utility model.
The announcement and teaching of book according to the above description, those skilled in the art in the invention can also be to above-mentioned embodiment party
Formula is changed and changed.Therefore, the invention is not limited in embodiment disclosed and described above, to the present invention's
Some modifications and changes should also be as falling into the scope of the claims of the present invention.In addition, although used in this specification
Some specific terms, but these terms are merely for convenience of description, do not form any restrictions to the present invention, using with its
Same or analogous other devices, all fall in the scope of protection of the present invention.
Claims (7)
- A kind of 1. aircraft air propeller, it is characterised in that：Including fuselage (1), above push away screw mechanism (2), preceding push away spiral Mechanism (3), wing (4) and propeller control system, the rear and front end for above pushing away screw mechanism (2) and being installed in fuselage (1), institute The left and right sides that screw mechanism (3) is installed in fuselage (1) is pushed away before stating, cabin (5), the wing are provided with the middle part of the fuselage (1) (4) on fuselage (1), the propeller control system includes the middle control main frame in cabin (5) and controls main frame electricity with middle Property connection dynamical system, control module, laser ranging controller and center dynamic balance system, the control module is electrically connected with Dynamic system, self balancing device and remote control, the dynamical system, which is electrically connected with lifting force system and advanced, promotes system System, the screw mechanism (2) that above pushes away are controlled by the lifting force system, screw mechanism (3) are pushed away before described and passes through the advance Propulsion system controls.
- A kind of 2. aircraft air propeller as claimed in claim 1, it is characterised in that：It is described above to push away screw mechanism (2) Propeller blade is above pushed away for be arranged at fuselage (1) rear and front end.
- A kind of 3. aircraft air propeller as claimed in claim 1, it is characterised in that：Screw mechanism (3) is pushed away before described Propeller blade is pushed away to be arranged at before fuselage (1) left and right ends, the advance propulsion system includes course changing control module, for controlling Turning function is realized in the left and right directions regulation that propeller blade is pushed away before system.
- A kind of 4. aircraft air propeller as claimed in claim 1, it is characterised in that：The self balancing device is gyro Instrument is simultaneously controlled by control module, improves the balanced capacity of aircraft.
- A kind of 5. aircraft air propeller as claimed in claim 1, it is characterised in that：The fuselage (1) is fine using carbon Peacekeeping aluminium alloy, it can effectively mitigate fuselage weight.
- A kind of 6. aircraft air propeller as claimed in claim 1, it is characterised in that：The dynamical system uses battery Driven by power.
- A kind of 7. aircraft air propeller as claimed in claim 1, it is characterised in that：The dynamical system uses gasoline Machine drives.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720704048.XU CN206813318U (en) | 2017-06-16 | 2017-06-16 | A kind of aircraft air propeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720704048.XU CN206813318U (en) | 2017-06-16 | 2017-06-16 | A kind of aircraft air propeller |
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| Publication Number | Publication Date |
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| CN206813318U true CN206813318U (en) | 2017-12-29 |
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| CN201720704048.XU Active CN206813318U (en) | 2017-06-16 | 2017-06-16 | A kind of aircraft air propeller |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107176292A (en) * | 2017-06-16 | 2017-09-19 | 重庆谭工科技有限公司 | A kind of aircraft air propeller |
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2017
- 2017-06-16 CN CN201720704048.XU patent/CN206813318U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107176292A (en) * | 2017-06-16 | 2017-09-19 | 重庆谭工科技有限公司 | A kind of aircraft air propeller |
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