CN109552653A - A kind of emission type unmanned plane - Google Patents
A kind of emission type unmanned plane Download PDFInfo
- Publication number
- CN109552653A CN109552653A CN201811447059.XA CN201811447059A CN109552653A CN 109552653 A CN109552653 A CN 109552653A CN 201811447059 A CN201811447059 A CN 201811447059A CN 109552653 A CN109552653 A CN 109552653A
- Authority
- CN
- China
- Prior art keywords
- shell
- unmanned plane
- emission type
- dispersion
- pedestal
- 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.)
- Pending
Links
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 25
- 239000006185 dispersion Substances 0.000 claims abstract description 21
- 230000013011 mating Effects 0.000 claims abstract description 4
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 12
- 239000007789 gas Substances 0.000 claims description 7
- 239000007788 liquid Substances 0.000 claims description 6
- 229910052757 nitrogen Inorganic materials 0.000 claims description 6
- 238000005265 energy consumption Methods 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The present invention discloses a kind of emission type unmanned plane, including emitting shell, the transmitting shell includes two pieces etc. big of cambered surface shell, it is in mating connection between the cambered surface shell, the transmitting shell is closed at one end, the other end snaps connection dispersion pedestal, and emission cavity is equipped in the transmitting shell, the device of ejection launch shell is equipped in the dispersion pedestal.It realizes and carries out hovering or flight operation after quickly approaching target area, improve working efficiency, reduce energy consumption, be suitable for being widely used to promote.
Description
Technical field
The present invention relates to unmanned plane, specifically a kind of emission type unmanned plane.
Background technique
Currently, unmanned air vehicle technique is quickly grown, many traditional industries start the application for slowly introducing unmanned plane, promote row
The intelligentized updating of industry.Unmanned plane in the market is usually based on rotor wing unmanned aerial vehicle and fixed-wing unmanned plane.Unmanned plane is working
When, the process from departure place to job site generally requires the regular hour, if it is that cannot facilitate close region, emits
To the need of work long period, working efficiency is reduced, increases energy consumption.
Summary of the invention
In view of the above existing problems in the prior art, the present invention provides a kind of emission type unmanned planes, can quickly approach mesh
Mark carries out hovering or flight operation behind region.
To achieve the goals above, a kind of emission type unmanned plane that the present invention uses, including transmitting shell, the transmitting shell
Body includes two pieces etc. big of cambered surface shell, and in mating connection between the cambered surface shell, the transmitting shell is closed at one end, another
End snaps connection dispersion pedestal, and emission cavity is equipped in the transmitting shell, is equipped with ejection launch shell in the dispersion pedestal
Device.
As an improvement, be equipped with inflation packet in the dispersion pedestal, equipped with liquid nitrogen container in inflation packet, on the liquid nitrogen container
Equipped with electromagnetic gas valve, the electromagnetic gas valve is electrically connected controller.
As an improvement, being equipped with baffle, the transmitting shell and dispersion bottom close to transmitting shell side in the dispersion pedestal
Seat junction is circumferentially uniformly provided with Elastic buckle, the deck that the dispersion pedestal is equipped with and Elastic buckle matches.
The present invention realizes that folded unmanned plane can bear higher overload to obtain biggish initial velocity, can be with letter
Single fast means make unmanned plane quickly approach target area, quickly arrive at target area at the first time, save a large amount of flight roads
Time on way reduces energy consumption, improves working efficiency, is suitable for being widely used to promote.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
In figure: 1, emitting shell, 2, cambered surface shell, 3, dispersion pedestal, 4, inflation packet, 5, electromagnetic gas valve, 6, baffle, 7, elastic card
Button, 8, deck.
Specific embodiment
In order to make the objectives, technical solutions and advantages of the present invention clearer, right below by attached drawing and embodiment
The present invention is further elaborated.However, it should be understood that specific embodiment described herein is only used to explain this hair
Range that is bright, being not intended to restrict the invention.
A kind of emission type unmanned plane, including transmitting shell 1, the transmitting shell 1 include two pieces etc. big of cambered surface shell 2,
In mating connection between the cambered surface shell 2, the transmitting shell 1 is closed at one end, and the other end snaps connection dispersion pedestal 3, institute
It states and is equipped with emission cavity in transmitting shell 1, the device of ejection launch shell 1 is equipped in the dispersion pedestal 3.
It is equipped with inflation packet 4 in the dispersion pedestal 3, is equipped with liquid nitrogen container in the inflation packet 4, the liquid nitrogen container is equipped with electricity
Magnetism valve 5, the electromagnetic gas valve 5 are electrically connected controller.
It is equipped with baffle 6 close to transmitting 1 side of shell in the dispersion pedestal 3, the transmitting shell 1 and dispersion pedestal 3 connect
The place of connecing circumferentially is uniformly provided with Elastic buckle 7, the deck 8 that the dispersion pedestal 3 is equipped with and Elastic buckle 7 matches.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Made any modification, equivalent replacement or improvement etc., should all be included in the protection scope of the present invention within mind and principle.
Claims (3)
1. a kind of emission type unmanned plane, including transmitting shell (1), which is characterized in that the transmitting shell (1) is big including two pieces etc.
Cambered surface shell (2), in mating connection between the cambered surface shell (2), the transmitting shell (1) is closed at one end, other end card
Button connection dispersion pedestal (3), the transmitting shell (1) is interior to be equipped with emission cavity, is equipped with ejection launch in the dispersion pedestal (3)
The device of shell (1).
2. a kind of emission type unmanned plane according to claim 1, it is characterised in that: be equipped with and fill in the dispersion pedestal (3)
Gas bag (4), the inflation packet (4) is interior to be equipped with liquid nitrogen container, and the liquid nitrogen container is equipped with electromagnetic gas valve (5), the electromagnetic gas valve (5)
It is electrically connected controller.
3. a kind of emission type unmanned plane according to claim 1, it is characterised in that: close to hair in the dispersion pedestal (3)
It penetrates shell (1) side and is circumferentially uniformly provided with elasticity equipped with baffle (6), the transmitting shell (1) and dispersion pedestal (3) junction
It buckles (7), the deck (8) that dispersion pedestal (3) is equipped with and Elastic buckle (7) match.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811447059.XA CN109552653A (en) | 2018-11-29 | 2018-11-29 | A kind of emission type unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811447059.XA CN109552653A (en) | 2018-11-29 | 2018-11-29 | A kind of emission type unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109552653A true CN109552653A (en) | 2019-04-02 |
Family
ID=65868025
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811447059.XA Pending CN109552653A (en) | 2018-11-29 | 2018-11-29 | A kind of emission type unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109552653A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101233045A (en) * | 2005-05-31 | 2008-07-30 | 西科尔斯基飞机公司 | Rotor hub fairing system for a counter-rotating, coaxial rotor system |
| CN202574628U (en) * | 2012-04-10 | 2012-12-05 | 航宇救生装备有限公司 | Sled-type power parachute launcher |
| CN103979110A (en) * | 2014-05-29 | 2014-08-13 | 襄阳宏伟航空器有限责任公司 | Ballistic parachute life-saving system |
| US9889941B1 (en) * | 2017-02-03 | 2018-02-13 | Indemnis, Inc. | Inflatable deployment apparatus for descent-restraint system for aerial vehicles |
| CN108791859A (en) * | 2018-07-12 | 2018-11-13 | 西安君晖航空科技有限公司 | A kind of rotor wing unmanned aerial vehicle quickly approached |
-
2018
- 2018-11-29 CN CN201811447059.XA patent/CN109552653A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101233045A (en) * | 2005-05-31 | 2008-07-30 | 西科尔斯基飞机公司 | Rotor hub fairing system for a counter-rotating, coaxial rotor system |
| CN202574628U (en) * | 2012-04-10 | 2012-12-05 | 航宇救生装备有限公司 | Sled-type power parachute launcher |
| CN103979110A (en) * | 2014-05-29 | 2014-08-13 | 襄阳宏伟航空器有限责任公司 | Ballistic parachute life-saving system |
| US9889941B1 (en) * | 2017-02-03 | 2018-02-13 | Indemnis, Inc. | Inflatable deployment apparatus for descent-restraint system for aerial vehicles |
| CN108791859A (en) * | 2018-07-12 | 2018-11-13 | 西安君晖航空科技有限公司 | A kind of rotor wing unmanned aerial vehicle quickly approached |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190402 |
|
| WD01 | Invention patent application deemed withdrawn after publication |