CN204802068U - Novel unmanned aerial vehicle cabin body - Google Patents
Novel unmanned aerial vehicle cabin body Download PDFInfo
- Publication number
- CN204802068U CN204802068U CN201520513813.0U CN201520513813U CN204802068U CN 204802068 U CN204802068 U CN 204802068U CN 201520513813 U CN201520513813 U CN 201520513813U CN 204802068 U CN204802068 U CN 204802068U
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- CN
- China
- Prior art keywords
- flight control
- engine compartment
- hatch
- quick detach
- engine
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Abstract
The utility model provides a novel unmanned aerial vehicle cabin body is by flight control cabin cover, cabin casing, engine compartment lid, a plurality of quick detach hasp handle with constitute rather than the quick detach latch hook that matches, its characterized in that, the tip top of flight control cabin cover is equipped with the engine compartment mouth, and the middle part top is equipped with the flight control hatch, engine compartment mouth and flight control hatch seal with engine compartment lid and flight control cabin cover respectively and match, the outer of engine compartment lid and flight control cabin cover both sides do not is fixed with a plurality of quick detach latch hook along the part, engine compartment mouth and flight control hatch both sides outer along the part do not be fixed with with quick detach latch hook corresponding match's quick detach hasp one by one. Engine compartment mouth and flight control hatch respectively with the sealed back of matcing of engine compartment lid and flight control cabin cover, corresponding match's quick detach hasp is connected or is opened with the quick detach latch hook one by one, can the engine compartment mouth cover with engine compartment respectively with the flight control hatch and the flight control cabin cover seals and perhaps shirks.
Description
Technical field
The utility model relates to a kind of technical field of aerospace, is specifically related to a kind of novel engine room zero people body, can fast sealing or shirk engine compartment cover and flight control hatchcover.
Background technology
What China Patent No. 201120519898.5 disclosed that the intersegmental sealing in type engine room zero people, a kind of sea and mechanism for monitoring relate to is a kind of be arranged on marinely to reclaim, the floating intersegmental rapid sealing mechanism in unmanned aerial vehicle body cabin, the water-proff packing and the sealing state that are mainly used in section junction, type engine room zero people, sea are monitored.Comprise docking structure, Inflatted rubber tyre, appendix, air-pressure gauge and self-styled charging connector; Docking structure is separately positioned on nose capsule and rear sealed module joint, and a sealed module joint is provided with the annular groove, air-pressure gauge installation tapped bore and the self-styled charging connector that hold Inflatted rubber tyre and installs tapped bore wherein; The air-pressure gauge that air-pressure gauge sealing is arranged on sealing bulkhead is installed on tapped bore, Inflatted rubber tyre is inserted in the annular groove of docking structure, drawing appendix is connected on air-pressure gauge, and the self-styled charging connector that self-styled charging connector is arranged on sealing bulkhead is installed on tapped bore, and is communicated with air-pressure gauge.The intersegmental sealing in type engine room zero people, the utility model sea and mechanism for monitoring reasonable in design, structure is simple, good sealing effect, and can Real-Time Monitoring.
China Patent No. 201420374131.1 discloses a kind of for locking device fixing between unmanned plane housing, the cabin cover that it comprises cabin and matches with cabin, the opening part in cabin is provided with thin liner plate, the outward flange of cabin cover medial surface is provided with the thin cover plate matched with thin liner plate, the middle part of cabin cover medial surface is provided with thick cover plate, the two ends of thick cover plate lower end are respectively arranged with base, base upper side is provided with two cylinders, be respectively cylinder A and cylinder B, the lateral surface place of the corresponding cabin cover of cylinder A and cylinder B offers groove, cylinder A inside is interspersed with L-type latch, the horizontal segment of L-type latch interts in the inside of cylinder A, the vertical section of L-type latch stretches out the lateral surface of cabin cover by groove, cylinder B inside is provided with spring.The utility model simplicity of design, good looking appearance, easy to operate, only need stir latch in the outside of cabin cover, thus realize the open and close of cabin cover.
Utility model content
The purpose of this utility model is to provide a kind of novel engine room zero people body, has simple and practical, safe and reliable, can fast sealing or shirk engine compartment cover and flight controls the good effect of hatchcover.
For achieving the above object, the utility model have employed such technical scheme: described novel engine room zero people body, controls hatchcover, cabin housing, engine compartment cover, several quick disassemble lock Button Handles and the quick detach latch hook that mates with it form by flight; It is characterized in that, be provided with engine hatch above the end of flight control hatchcover, be provided with flight above middle part and control hatch; Engine hatch and flight control hatch and control hatchcover respectively with engine compartment cover and flying and seal and mate; The peripheral rim portion that engine compartment cover and flight control hatchcover both sides is not fixed with several quick detach latch hooks; The peripheral rim portion that engine hatch and flight control hatch both sides is not fixed with the quick detach snap close mated with quick detach latch hook one_to_one corresponding.
In the utility model, described quick detach latch hook and quick detach snap close are two assemblies of quick release buckle in Hardware fitting, have feature convenient to disassembly, usually for needing the making of furniture or the case and bag often opened; Its model and kind more, call also more, such as: cabinet is buckled, butterfly is buckled, duckbilled is buckled, spring buckle, pulling buckle etc.But no matter the quick release buckle of which kind of model all drops in range of choice of the present utility model.
After adopting such structure, engine hatch and flight control hatch and control with engine compartment cover and flying after hatchcover seals and mate respectively, the quick detach snap close that one_to_one corresponding mates be connected with quick detach latch hook or open, engine hatch and flight can controlling hatch and control hatchcover with engine compartment cover and seal with flying or shirk respectively.Like this, the use of very convenient machinery space and any purposes of flight control cabinet.
The beneficial effects of the utility model: simple and practical, safe and reliable, can fast sealing or shirk engine compartment cover and flight control hatchcover.
Accompanying drawing explanation
Accompanying drawing is depicted as the schematic diagram of the utility model concrete structure.
Detailed description of the invention
Below in conjunction with accompanying drawing, novel engine room zero people described in the utility model body is described in detail; As shown in the figure, described novel engine room zero people body, controls hatchcover 1, cabin housing 2, engine compartment cover 3, several quick disassemble lock Button Handles 4 and the quick detach latch hook 40 that mates with it by flight and forms; It is characterized in that, be provided with engine hatch 5 above the end of flight control hatchcover 1, be provided with flight above middle part and control hatch 6; Engine hatch 5 and flight control hatch 6 and control hatchcover 1 respectively with engine compartment cover 3 and flying and seal and mate; The peripheral rim portion that engine compartment cover 3 and flight control hatchcover 1 both sides is not fixed with several quick detach latch hooks 40; The peripheral rim portion that engine hatch 5 and flight control hatch 6 both sides is not fixed with the quick detach snap close 4 mated with quick detach latch hook 40 one_to_one corresponding.
Claims (1)
1. a novel engine room zero people body, controls hatchcover (1), cabin housing (2), engine compartment cover (3), several quick disassemble lock Button Handles (4) and the quick detach latch hook (40) that mates with it by flight and forms; It is characterized in that, above the end of flight control hatchcover (1), be provided with engine hatch (5), being provided with flight above middle part and controlling hatch (6); Engine hatch (5) and flight control hatch (6) and control hatchcover (1) respectively with engine compartment cover (3) and flying and seal and mate; The peripheral rim portion that engine compartment cover (3) and flight control hatchcover (1) both sides is not fixed with several quick detach latch hooks (40); The peripheral rim portion that engine hatch (5) and flight control hatch (6) both sides is not fixed with the quick detach snap close (4) mated with quick detach latch hook (40) one_to_one corresponding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520513813.0U CN204802068U (en) | 2015-07-09 | 2015-07-09 | Novel unmanned aerial vehicle cabin body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520513813.0U CN204802068U (en) | 2015-07-09 | 2015-07-09 | Novel unmanned aerial vehicle cabin body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204802068U true CN204802068U (en) | 2015-11-25 |
Family
ID=54586928
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520513813.0U Active CN204802068U (en) | 2015-07-09 | 2015-07-09 | Novel unmanned aerial vehicle cabin body |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204802068U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105173055A (en) * | 2015-07-09 | 2015-12-23 | 河南翱翔航空科技有限公司 | Novel unmanned plane cabin |
| CN106275374A (en) * | 2016-08-31 | 2017-01-04 | 河南翱翔航空科技有限公司 | Novel unmanned plane nacelle of taking photo by plane |
-
2015
- 2015-07-09 CN CN201520513813.0U patent/CN204802068U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105173055A (en) * | 2015-07-09 | 2015-12-23 | 河南翱翔航空科技有限公司 | Novel unmanned plane cabin |
| CN106275374A (en) * | 2016-08-31 | 2017-01-04 | 河南翱翔航空科技有限公司 | Novel unmanned plane nacelle of taking photo by plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |