CN205819576U - A kind of flight control system shell - Google Patents
A kind of flight control system shell Download PDFInfo
- Publication number
- CN205819576U CN205819576U CN201620488485.8U CN201620488485U CN205819576U CN 205819576 U CN205819576 U CN 205819576U CN 201620488485 U CN201620488485 U CN 201620488485U CN 205819576 U CN205819576 U CN 205819576U
- Authority
- CN
- China
- Prior art keywords
- control system
- flight control
- hole
- shell
- cable
- 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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- Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
Abstract
This utility model relates to a kind of flight control system shell, overall making by metal material is formed, and has uncovered housing including one, and described housing has the cavity of accommodating flight control system, the lateral wall of described housing is provided with cable-through hole, is provided with O-ring seal in described cable-through hole.This utility model utilizes the heat conductivity of metal self, add the heat-sinking capability of parts, utilize the electrical conductivity of metal itself, serve the shielding action of noise signal, so that the flight control system of pilot is avoided being disturbed by outer signals and weather, ensure the steady-working state of pilot.
Description
Technical field
This utility model belongs to unmanned air vehicle technique field, is specifically related to a kind of flight control system shell.
Background technology
Unmanned plane has on military and civil area and is widely applied very much, and flight control system is the core of aircraft, is arranged on
On unmanned plane, control the flight of unmanned plane and the communications exchange of exogenous data.Therefore, it is necessary to protected by safety, and prevent
The only interference of external signal, current unmanned plane does not still have a kind of guard system very well to protect flight control system.
Utility model content
The purpose of this utility model is to solve above-mentioned technical problem and provides a kind of flight for unmanned plane to control
The flight control system shell that system is installed.
For achieving the above object, this utility model adopts the following technical scheme that
A kind of flight control system shell, overall making by metal material is formed, and has uncovered housing, described shell including one
Body has the cavity of accommodating flight control system, and the lateral wall of described housing is provided with cable-through hole, is provided with in described cable-through hole
O-ring seal.
Described cable-through hole is two, is opened in respectively on relative two sidewall of described shell.
The outside of described shell is provided with the fixed installation hole for being connected with the bottom fixed board of flight control system.
This utility model flight control system shell, is formed by metal material making by entirety, has uncovered including one
Housing, described housing has the cavity of accommodating flight control system, and the lateral wall of described housing is provided with cable-through hole, described line excessively
Hole is provided with O-ring seal, the heat conductivity of available metal self, add the heat-sinking capability of parts, utilize metal itself
Electrical conductivity, serve the shielding action of noise signal, so that the flight control system of pilot is avoided by outer signals and gas
The interference waited, has ensured the steady-working state of pilot.
Accompanying drawing explanation
Fig. 1 is the structural representation of flight control system shell；
Fig. 2 is the front view of flight control system shell；
Fig. 3 is the side view of flight control system shell；
Fig. 4 is the top view of flight control system shell.
Detailed description of the invention
Below, in conjunction with example, substantive distinguishing features of the present utility model and advantage are further described, this utility model
Including, but not limited to listed embodiment.
Seeing shown in Fig. 1-4, a kind of flight control system shell, overall making by metal material is formed, and has spacious including one
Mouthful housing 100, described housing has the cavity of accommodating flight control system, the lateral wall of described housing be provided with offer wired
Hole 11, is provided with O-ring seal 10 in described string holes.
Described cable-through hole is two, is opened in respectively on relative two sidewall of described shell.
The outside of described shell is provided with the fixed installation hole for being connected with the bottom fixed board 200 of flight control system
12。
It should be noted that in this utility model, described cable-through hole 11 can be U-shaped hole, from the opening end of described shell
Offering downwards formation, described O-ring seal 10 is arranged in this U-shaped hole.
Described shell can use steel matter or aluminum alloy materials to make, and the shield effectiveness of such noise signal is more preferable, from
And more can ensure the stability of flight.
This utility model sealed heat-dissipating filtering flight control system shell, owing to using all-metal sealing design, shell utilizes two
End rubber ring plays dust-proof, waterproof action, utilizes the heat conductivity of metal self, adds the heat-sinking capability of parts, utilizes gold
The electrical conductivity of genus itself, serves the shielding action of noise signal, so that the flight control system of pilot is avoided being believed by the external world
Number and the interference of weather, ensured the steady-working state of pilot.
The above is only preferred implementation of the present utility model, it is noted that for the common skill of the art
For art personnel, on the premise of without departing from this utility model principle, it is also possible to make some improvements and modifications, these improve and
Retouching should be regarded as protection domain of the present utility model.
Claims (1)
1. a flight control system shell, it is characterised in that overall making by metal material is formed, and has uncovered shell including
Body, described housing has the cavity of accommodating flight control system, and the lateral wall of described housing is provided with the cable-through hole of U-shape, institute
State and cable-through hole is provided with O-ring seal；Described cable-through hole is two, is opened in relative two sidewall of described shell respectively
On；The outside of described shell is provided with the fixed installation hole for being connected with the bottom fixed board of flight control system；Described mistake
String holes offers downwards formation from the opening end of described shell, and described shell uses steel matter or aluminum alloy materials to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620488485.8U CN205819576U (en) | 2016-05-25 | 2016-05-25 | A kind of flight control system shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620488485.8U CN205819576U (en) | 2016-05-25 | 2016-05-25 | A kind of flight control system shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205819576U true CN205819576U (en) | 2016-12-21 |
Family
ID=57558035
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620488485.8U Expired - Fee Related CN205819576U (en) | 2016-05-25 | 2016-05-25 | A kind of flight control system shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205819576U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020114525A1 (en) * | 2018-12-05 | 2020-06-11 | 顺丰科技有限公司 | Avionic structure of unmanned aerial vehicle and unmanned aerial vehicle |
-
2016
- 2016-05-25 CN CN201620488485.8U patent/CN205819576U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020114525A1 (en) * | 2018-12-05 | 2020-06-11 | 顺丰科技有限公司 | Avionic structure of unmanned aerial vehicle and unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 300270 Tianjin Binhai New Area, Dagang seaside street, red flag Road south side of bungalow 7. Patentee after: Tianjin City tianxiang Hongyu Technology Co. Ltd. Address before: 300270 Tianjin Binhai New Area, Dagang seaside street, red flag Road south side of bungalow 7. Patentee before: TIANJIN HONGYU TIANXIANG TECHNOLOGY 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: 20161221 Termination date: 20210525 |