CN202201165U - Steering erection support of dynamical system of cantilever of small air vehicle - Google Patents
Steering erection support of dynamical system of cantilever of small air vehicle Download PDFInfo
- Publication number
- CN202201165U CN202201165U CN2011202203731U CN201120220373U CN202201165U CN 202201165 U CN202201165 U CN 202201165U CN 2011202203731 U CN2011202203731 U CN 2011202203731U CN 201120220373 U CN201120220373 U CN 201120220373U CN 202201165 U CN202201165 U CN 202201165U
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- CN
- China
- Prior art keywords
- mounting hole
- dirigible
- cantilever
- airship
- erection support
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
A steering erection support of a cantilever dynamical system of a small air vehicle comprises a T-shaped base 1, a prestressed damping connecting ring 2, a dynamical mounting hole 3 and a mounting hole 4 of the T-shaped base. The dynamical mounting hole 3 and the mounting hole 4 of the T-shaped base are arranged on the T-shaped base 1; and the prestressed damping connecting ring 2 is connected with an empennage of the T-shaped base. With the adoption of the dynamical steering erection support of the utility model, the dynamical system of the small air vehicle is arranged on the two sides of an airship, therefore, the air equipment carried in the airship is provided with visual angle without obstructions. At the same time, a cantilever supporting structure is provide by the prestressed damping connecting ring, the shock of the dynamical system is absorbed by the airbag of the airship by a stay rope, the shock of the airship is reduced, and the damping performance of the airship is improved.
Description
Technical field
The utility model relates to the small-sized aerial craft technology, relates in particular to the bearing that small-sized dirigible and blimp cantilever power system turn to installation.
Background technology
An important use of small aircraft; Just provide a unpiloted airflight platform; Be applicable to purposes such as aviation detection, aerial photography, aerial signal relaying, above various uses need be installed various professional equipment under dirigible or aircraft belly.
At present, small-sized dirigible, particularly blimp; Its power system device generally is installed in the gondola part under the dirigible; Cause the power system of dirigible that the same position that is installed in professional equipment is installed, produce the disadvantageous power of equipment is shaken, and influence the visual field of equipment; Therefore, one of way of solution is with the unsettled both sides that are installed in dirigible of the power system of dirigible.
At present; SUAV; Its engine installation generally is installed in the nose (preceding pull-type) or the afterbody (back-pushed) of aircraft, and body shakes greatly and influence the visual field of equipment, and one of way of solution is back or the both sides wing that aircraft power system cantilever is installed in aircraft.
The blimp both sides do not have can supply to install the solid base of power, can't power system be installed by conventional approach, are the unsettled great difficult problems that is installed on both sides of present blimp power.SUAV also is an interior problem of industry because the thinner thickness of wing is difficult to the space and the intensity direct mount airscrew engine that provide enough.
Summary of the invention
The purpose of the utility model is to provide a kind of small-sized dirigible and blimp cantilever power system to turn to erection support; The direction and the installation direction of the pulling force of airscrew engine generation are changed, realized that a kind of later-model screw propeller power is installed in the technology of dirigible side; The prestressed damping coupling link that turns to bearing to provide makes the air bag of dirigible can absorb the vibrations of engine producing, the vibration influence that makes all kinds of professional equipment that is installed under the dirigible not produced by airscrew engine.The airscrew engine that the utility model can also be used to solve SUAV is on wing or the installation question of other specific positions.
The purpose of the utility model is to realize like this; It is made up of T shape pier 1, prestressed damping coupling link 2, power mounting hole 3, T shape base mounting hole 4; Dynamic mounting hole 3 and T shape base mounting hole 4 on the T shape pier 1, what link to each other with T shape base afterbody is prestressed damping coupling link 2.
The utility model has the advantages that: through this power steering erection support, the power system of dirigible is installed in the both sides of dirigible, thereby the aerial equipment that carries for dirigible provides unscreened visual angle; And cantilevered support structure is provided through the prestressed damping coupling link, and drag-line is passed through in the vibrations of power system absorb by the dirigible air bag, reduced the vibrations of dirigible, improved the damping performance of dirigible.
Description of drawings
Accompanying drawing 1 is the axonometric drawing of the utility model structural representation.
Accompanying drawing 2 is the front view of the utility model structural representation.
Accompanying drawing 3 is the top view of the utility model structural representation.
Accompanying drawing 4 is the upward view of the utility model structural representation.
Accompanying drawing 5 is the installation process scheme drawing.
Accompanying drawing 6 is the top view of the dirigible scheme drawing of installation the utility model.
Accompanying drawing 7 is the front view of the dirigible scheme drawing of installation the utility model.
Among the figure, 1 is T shape pier, and 2 is the prestressed damping coupling link, and 3 is the power mounting hole, and 4 is T shape base mounting hole, and 5 is prestressed cable, and 6 is the dirigible power system, and 7 is dirigible air bag permanent seat.
The specific embodiment
Following according to accompanying drawing 1, Fig. 5, Fig. 6, the given embodiment of Fig. 7, the utility model technical scheme is done further explain.This small aircraft cantilever power system turns to erection support to be made up of T font structure base 1, prestressed damping coupling link 2, power mounting hole 3, T shape base mounting hole 4.Four T shape base mounting holes 4 of this bearing are fixed on T shape pier 1 on the cantilever design of dirigible both sides through bolt; The power system 6 of dirigible is through on four power mounting holes 3 that are bolted to T shape pier 1 upper periphery; Drag-line 5 colligations are on the prestressed damping coupling link 2 and be tightened on the dirigible air bag permanent seat 7, thereby reach the unsettled purpose that is installed in the dirigible both wings of the power system of dirigible; The shock transfer that drag-line 5 produces the dirigible power system is to the dirigible air bag, and air bag has absorbed the vibrations that power system produces, thereby has reached the purpose of dynamic damping.
Claims (1)
1. a small aircraft cantilever power system turns to erection support; Comprise T shape pier (1), prestressed damping coupling link (2), power mounting hole (3), T shape base mounting hole (4); It is characterized in that T shape pier (1) upward dynamic mounting hole (3) and T shape base mounting hole (4), what link to each other with T shape base afterbody is prestressed damping coupling link (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011202203731U CN202201165U (en) | 2011-06-27 | 2011-06-27 | Steering erection support of dynamical system of cantilever of small air vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011202203731U CN202201165U (en) | 2011-06-27 | 2011-06-27 | Steering erection support of dynamical system of cantilever of small air vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202201165U true CN202201165U (en) | 2012-04-25 |
Family
ID=45965300
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011202203731U Expired - Fee Related CN202201165U (en) | 2011-06-27 | 2011-06-27 | Steering erection support of dynamical system of cantilever of small air vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202201165U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102320374A (en) * | 2011-06-27 | 2012-01-18 | 湖北金像无人航空科技服务有限公司 | Steering erection support for cantilever power system of small-sized aircraft |
-
2011
- 2011-06-27 CN CN2011202203731U patent/CN202201165U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102320374A (en) * | 2011-06-27 | 2012-01-18 | 湖北金像无人航空科技服务有限公司 | Steering erection support for cantilever power system of small-sized aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170829 Address after: 430056 No. 8503, No. 5, block A, Huayuan Business Plaza, 16 business road, Wuhan economic and Technological Development Zone, Hubei, China Patentee after: Wuhan parallel world network technology Co., Ltd. Address before: 8506, room 430056, block A, Huayuan Business Plaza, 16 entrepreneurial road, Wuhan economic and Technological Development Zone, Hubei Patentee before: Hubei Jinxiang Unmanned Aviation Technology Service Co., Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120425 Termination date: 20200627 |