CN105173055A - Novel unmanned plane cabin - Google Patents
Novel unmanned plane cabin Download PDFInfo
- Publication number
- CN105173055A CN105173055A CN201510416487.6A CN201510416487A CN105173055A CN 105173055 A CN105173055 A CN 105173055A CN 201510416487 A CN201510416487 A CN 201510416487A CN 105173055 A CN105173055 A CN 105173055A
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- CN
- China
- Prior art keywords
- engine
- cabin
- flying control
- hatch
- cover
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- 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.)
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Abstract
A novel unmanned plane cabin is composed of a flying control cabin cover, a plane cabin shell, an engine cabin cover, a plurality of quick release buckle handles and a plurality of quick release lock hooks matched with the quick release buckle handles. The novel unmanned plane cabin is characterized in that an engine cabin opening is formed in the upper portion of the end of the flying control cabin cover, and a flying control cabin opening is formed in the upper portion of the middle of the flying control cabin cover; the engine cabin opening and the flying control cabin opening are matched with the engine cabin cover and the flying control cabin cover in a sealed mode respectively; the quick release buckle handles are fixed to the outer edges of the two sides of the engine cabin cover and the outer edges of the two sides of the flying control cabin cover respectively; quick release buckles matched with the quick release lock hooks in a one-to-one correspondence mode are fixed to the outer edges of the two sides of the engine cabin opening and the outer edges of the two sides of the flying control cabin opening respectively. After the engine cabin opening and the flying control cabin opening are matched with the engine cabin cover and the flying control cabin cover in a sealed mode, the quick release buckles and the quick release lock hooks which are matched in the one-to-one correspondence mode are connected or opened, and accordingly the engine cabin opening and the flying control cabin opening can be sealed or disconnected with the engine cabin cover and the flying control cabin cover respectively.
Description
Technical field
The present invention relates to a kind of technical field of aerospace, be 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 present invention 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.Simplicity of design of the present invention, 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.
Summary of the invention
The object of this invention is to provide a kind of novel engine room zero people body, have 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, present invention employs such technical scheme: described novel engine room zero people body, controlling hatchcover, cabin housing, engine compartment cover, several quick disassemble lock Button Handles and the quick detach lock hook that mates with it by flight and forming; 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 lock 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 lock hook one_to_one corresponding.
In the present invention, described quick detach lock 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 invention.
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 mate one_to_one corresponding and quick disassemble lock link and connect or open, and engine hatch and flight can control hatch respectively with engine compartment cover with fly and control hatchcover and seal or shirk.Like this, the use of very convenient machinery space and any purposes of flight control cabinet.
Beneficial effect of the present invention: 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 concrete structure of the present invention.
Detailed description of the invention
Below in conjunction with accompanying drawing, novel engine room zero people of the present invention 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 lock 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 lock 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 lock 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 lock 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 lock 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 lock hook (40) one_to_one corresponding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510416487.6A CN105173055A (en) | 2015-07-09 | 2015-07-09 | Novel unmanned plane cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510416487.6A CN105173055A (en) | 2015-07-09 | 2015-07-09 | Novel unmanned plane cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105173055A true CN105173055A (en) | 2015-12-23 |
Family
ID=54895641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510416487.6A Pending CN105173055A (en) | 2015-07-09 | 2015-07-09 | Novel unmanned plane cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105173055A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005359A (en) * | 2016-06-16 | 2016-10-12 | 沈阳飞机工业（集团）有限公司 | Airplane hatch cover connecting lock mounting method based on digital measurement |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1998025817A1 (en) * | 1996-12-09 | 1998-06-18 | Cartercopters, L.L.C. | Fuselage door for pressurized aircraft |
| CN201597751U (en) * | 2010-01-28 | 2010-10-06 | 江西洪都航空工业集团有限责任公司 | Flexible connection structure for glass edge of airplane cabin cover |
| CN203666962U (en) * | 2013-11-20 | 2014-06-25 | 天津三爻航空航天科技发展有限公司 | Hatch cover fastening structure for unmanned fixed wing operation aircraft |
| US20150040484A1 (en) * | 2011-08-19 | 2015-02-12 | Aerovironment, Inc. | Water-tight compartment with removable hatch and two-sided gel seal for multiple conduit access |
| CN204802068U (en) * | 2015-07-09 | 2015-11-25 | 河南翱翔航空科技有限公司 | Novel unmanned aerial vehicle cabin body |
-
2015
- 2015-07-09 CN CN201510416487.6A patent/CN105173055A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1998025817A1 (en) * | 1996-12-09 | 1998-06-18 | Cartercopters, L.L.C. | Fuselage door for pressurized aircraft |
| CN201597751U (en) * | 2010-01-28 | 2010-10-06 | 江西洪都航空工业集团有限责任公司 | Flexible connection structure for glass edge of airplane cabin cover |
| US20150040484A1 (en) * | 2011-08-19 | 2015-02-12 | Aerovironment, Inc. | Water-tight compartment with removable hatch and two-sided gel seal for multiple conduit access |
| CN203666962U (en) * | 2013-11-20 | 2014-06-25 | 天津三爻航空航天科技发展有限公司 | Hatch cover fastening structure for unmanned fixed wing operation aircraft |
| CN204802068U (en) * | 2015-07-09 | 2015-11-25 | 河南翱翔航空科技有限公司 | Novel unmanned aerial vehicle cabin body |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005359A (en) * | 2016-06-16 | 2016-10-12 | 沈阳飞机工业（集团）有限公司 | Airplane hatch cover connecting lock mounting method based on digital measurement |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20151223 |