CN207683774U - A kind of unmanned plane having air bag of saving oneself - Google Patents
A kind of unmanned plane having air bag of saving oneself Download PDFInfo
- Publication number
- CN207683774U CN207683774U CN201721443573.7U CN201721443573U CN207683774U CN 207683774 U CN207683774 U CN 207683774U CN 201721443573 U CN201721443573 U CN 201721443573U CN 207683774 U CN207683774 U CN 207683774U
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- CN
- China
- Prior art keywords
- air bag
- unmanned plane
- self
- fuselage
- saving oneself
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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
The utility model discloses a kind of unmanned planes having air bag of saving oneself,Its structure includes fuselage,Undercarriage,Self-rescuing air bag device,Wing,Bottom case,Motor,Paddle shaft,Tripod,Blade,Locator,Cable,Self-rescuing air bag device is embedded in the inside for being installed on fuselage,Undercarriage is mutually welded with fuselage,Motor welds the upper surface for being installed on bottom case,Tripod is mutually welded with wing,Blade is integrated with paddle shaft,Locator is connected with cable,Self-rescuing air bag device includes venthole,Body,Storehouse occurs for gas,Cylindrantherae,Heating wire,Venthole is integrated with body,A kind of unmanned plane having air bag of saving oneself of the utility model,Structure is equipped with self-rescuing air bag device,Self-rescuing air bag device is embedded in the inside for being installed on fuselage,When unmanned plane is in flight,When colliding,The air bag of saving oneself that gas occurs in storehouse will automatically turn on,It is damaged when unmanned plane being avoided freely to land,Wealth is caused to lose,Safe ready.
Description
Technical field
The utility model is a kind of unmanned plane having air bag of saving oneself, and belongs to unmanned plane field.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, Huo Zheyou
Car-mounted computer fully or intermittently automatically operates UAV, is to utilize radio robot and the journey provided for oneself
The not manned vehicle that sequence control device manipulates, unmanned plane is actually the general designation of unmanned vehicle, fixed from technical standpoint
Justice can be divided into：Unmanned fixed wing aircraft, unmanned VTOL aircraft unmanned airship, unmanned helicopter, nobody more rotor flyings
Device, unmanned parasol etc., compared with manned aircraft, it have small, low cost, it is easy to use, to operational environment require it is low,
The advantages that battlefield survival is stronger.
Prior art discloses application No. is：201620034718.7 a kind of unmanned plane having air bag of saving oneself, it is described
Unmanned plane is included in the monitoring device of dishing out for throwing the data for flying to monitor the unmanned plane under pattern, monitoring device and the institute of dishing out
Flight control assemblies electrical connection is stated, the data monitored are sent to the flight control assemblies by the monitoring device of dishing out,
The flight control assemblies control the unmanned plane after judging that the unmanned plane is spilled over and enter from steady pattern, but this is existing
Technology is saved oneself when can not collide to unmanned plane so that unmanned plane damages in landing, and safety coefficient is low.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of unmanned plane having air bag of saving oneself,
It saves oneself when can not be collided to unmanned plane with the prior art of solution so that unmanned plane damages in landing, peace
The low problem of overall coefficient.
To achieve the goals above, the utility model is to realize by the following technical solutions：One kind having gas of saving oneself
The unmanned plane of capsule, structure include fuselage, undercarriage, self-rescuing air bag device, wing, bottom case, motor, paddle shaft, tripod, leaf
Piece, locator, cable, the self-rescuing air bag device insertion are installed on the inside of fuselage, and the undercarriage is mutually welded with fuselage, institute
The upper surface that motor welding is installed on bottom case is stated, the tripod is mutually welded with wing, and the blade is integrated knot with paddle shaft
Structure, the locator are connected with cable, and the self-rescuing air bag device includes venthole, body, gas generation storehouse, cylindrantherae, electricity
Heated filament, the venthole are integrated with body, and the inside that storehouse insertion is installed on body, the electric heating occur for the gas
Silk is nested with cylindrantherae, and the bottom surface of the body is connected with cable.
Further, the wing is integrated with bottom case.
Further, the wing vertical is installed on the side of fuselage.
Further, the self-rescuing air bag device and cable be in the same plane.
Further, the paddle shaft is cylindrical structure.
Further, the blade uses alloy material, light and durable.
Further, the fuselage uses carbon fibre materials, beautiful and be hardly damaged.
Advantageous effect
A kind of unmanned plane having air bag of saving oneself of the utility model, structure are equipped with self-rescuing air bag device, air bag of saving oneself dress
The embedded inside for being installed on fuselage is set, when unmanned plane is in flight, when colliding, the air bag of saving oneself that gas occurs in storehouse will
It automatically turns on, is damaged when unmanned plane being avoided freely to land, wealth is caused to lose, safe ready.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram for the unmanned plane having air bag of saving oneself of the utility model；
Fig. 2 is a kind of internal structure schematic diagram of self-rescuing air bag device of the utility model.
In figure：Fuselage -1, undercarriage -2, self-rescuing air bag device -3, wing -4, bottom case -5, motor -6, paddle shaft -7, foot
Storehouse -303, cylindrantherae -304, electricity occur for frame -8, blade -9, locator -10, cable -11, venthole -301, body -302, gas
Heated filament -305.
Specific implementation mode
To make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, below
In conjunction with specific implementation mode, the utility model is expanded on further.
It please refers to Fig.1, Fig. 2, the utility model provides a kind of unmanned air vehicle technique scheme having air bag of saving oneself：Its structure packet
Include fuselage 1, undercarriage 2, self-rescuing air bag device 3, wing 4, bottom case 5, motor 6, paddle shaft 7, tripod 8, blade 9, locator 10,
Cable 11, the self-rescuing air bag device 3 are embedded in the inside for being installed on fuselage 1, and the undercarriage 2 is welded with 1 phase of fuselage, the electricity
Machine 6 welds the upper surface for being installed on bottom case 5, and the tripod 8 is welded with 4 phase of wing, and the blade 9 is integrated with paddle shaft 7
Structure, the locator 10 are connected with cable 11, and the self-rescuing air bag device 3 includes venthole 301, body 302, gas hair
Raw storehouse 303, cylindrantherae 304, heating wire 305, the venthole 301 are integrated with body 302, and storehouse occurs for the gas
303 insertions are installed on the inside of body 302, and the heating wire 305 is nested with cylindrantherae 304, bottom surface and the electricity of the body 302
Cable 11 is connected, and the wing 4 is integrated with bottom case 5, and the wing 4 is installed vertically on the side of fuselage 1, described
In the same plane with cable 11, the paddle shaft 7 is cylindrical structure to self-rescuing air bag device 3, and the blade 9 uses alloy material
Matter, light and durable, the fuselage 1 uses carbon fibre materials, beautiful and be hardly damaged.
Undercarriage 2 described in this patent be aircraft lower part for take off landing or ground taxi when support aircraft and for ground
The accessories apparatus of face movement is a kind of component of unique support whole airplane, and the wing 4 is one of important component of aircraft,
On fuselage, main effect is to generate lift, while ammunition cabins and fuel tank can also be set inside wing, is being flown
In can collect undercarriage.
When being used when unmanned plane awing breaks down, collides, when freely landing, self-rescuing air bag device 3 is just
It can start, the venthole 301 in self-rescuing air bag device 3 will enter air so that heating wire 305 is run, thus and cylindrantherae 304
Thermal effect reaction occurs, then generates bulk gas, storehouse 303, which occurs, in gas is inflated so that air bag gassy, to make
It obtains unmanned plane under the protection of air bag slowly to land, reduces the damage in descent.
The utility model solves to save oneself when the prior art can not collide to unmanned plane so that unmanned plane is landing
In damage, the low problem of safety coefficient, the utility model is combined with each other by above-mentioned component, and structure is equipped with and saves oneself gas
Bag apparatus, self-rescuing air bag device is embedded in the inside for being installed on fuselage, and when unmanned plane is in flight, when colliding, gas occurs
Air bag of saving oneself in storehouse will automatically turn on, and be damaged when unmanned plane being avoided freely to land, wealth is caused to lose, secure side
Just, described in detail below:
The self-rescuing air bag device 3 includes venthole 301, body 302, gas generation storehouse 303, cylindrantherae 304, heating wire
305, the venthole 301 is integrated with body 302, and the gas occurs the insertion of storehouse 303 and is installed on the interior of body 302
Side, the heating wire 305 are nested with cylindrantherae 304, and the bottom surface of the body 302 is connected with cable 11.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (5)
1. a kind of unmanned plane having air bag of saving oneself, it is characterised in that：Its structure includes fuselage (1), undercarriage (2), gas of saving oneself
Bag apparatus (3), wing (4), bottom case (5), motor (6), paddle shaft (7), tripod (8), blade (9), locator (10), cable
(11), the embedded inside for being installed on fuselage (1) of the self-rescuing air bag device (3), the undercarriage (2) are mutually welded with fuselage (1),
Motor (6) welding is installed on the upper surface of bottom case (5), and the tripod (8) is mutually welded with wing (4), the blade (9)
It is integrated with paddle shaft (7), the locator (10) is connected with cable (11), and the self-rescuing air bag device (3) includes
Venthole (301), body (302), gas occur storehouse (303), cylindrantherae (304), heating wire (305), the venthole (301) with
Body (302) is integrated, and storehouse (303) embedded inside for being installed on body (302), the heating wire occur for the gas
(305) it is nested with cylindrantherae (304), the bottom surface of the body (302) is connected with cable (11).
2. a kind of unmanned plane having air bag of saving oneself according to claim 1, it is characterised in that：The wing (4) and bottom
Case (5) is integrated.
3. a kind of unmanned plane having air bag of saving oneself according to claim 1, it is characterised in that：The wing (4) is vertical
It is installed on the side of fuselage (1).
4. a kind of unmanned plane having air bag of saving oneself according to claim 1, it is characterised in that：The self-rescuing air bag device
(3) in the same plane with cable (11).
5. a kind of unmanned plane having air bag of saving oneself according to claim 1, it is characterised in that：The paddle shaft (7) is round
Column structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721443573.7U CN207683774U (en) | 2017-11-01 | 2017-11-01 | A kind of unmanned plane having air bag of saving oneself |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721443573.7U CN207683774U (en) | 2017-11-01 | 2017-11-01 | A kind of unmanned plane having air bag of saving oneself |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207683774U true CN207683774U (en) | 2018-08-03 |
Family
ID=62988519
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721443573.7U Expired - Fee Related CN207683774U (en) | 2017-11-01 | 2017-11-01 | A kind of unmanned plane having air bag of saving oneself |
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| CN (1) | CN207683774U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353493A (en) * | 2018-09-28 | 2019-02-19 | 许剑聪 | A kind of self-rescue device of drowning unmanned plane equipped with gas generation buoyancy |
| WO2021072464A1 (en) | 2019-10-18 | 2021-04-22 | Glovetac Gmbh | Parachute system for a projectile |
| CN112896535A (en) * | 2021-03-09 | 2021-06-04 | 上海澄派信息科技有限公司 | Prevent that branch shelves unmanned aerial vehicle of saving oneself |
-
2017
- 2017-11-01 CN CN201721443573.7U patent/CN207683774U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353493A (en) * | 2018-09-28 | 2019-02-19 | 许剑聪 | A kind of self-rescue device of drowning unmanned plane equipped with gas generation buoyancy |
| WO2021072464A1 (en) | 2019-10-18 | 2021-04-22 | Glovetac Gmbh | Parachute system for a projectile |
| CN112896535A (en) * | 2021-03-09 | 2021-06-04 | 上海澄派信息科技有限公司 | Prevent that branch shelves unmanned aerial vehicle of saving oneself |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180803 Termination date: 20181101 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |