CN206086243U - High performance amphibian manned flight vehicle - Google Patents
High performance amphibian manned flight vehicle Download PDFInfo
- Publication number
- CN206086243U CN206086243U CN201621120534.9U CN201621120534U CN206086243U CN 206086243 U CN206086243 U CN 206086243U CN 201621120534 U CN201621120534 U CN 201621120534U CN 206086243 U CN206086243 U CN 206086243U
- Authority
- CN
- China
- Prior art keywords
- air bag
- wall
- housing
- manned vehicle
- igniter
- 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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- Air Bags (AREA)
Abstract
The utility model belongs to the technical field of the aircraft technique and specifically relates to a high performance amphibian manned flight vehicle, which comprises a housin, the inner chamber of casing is provided with the controlling means who is used for controlling whole aircraft, the outer wall symmetry of casing is provided with top wing and lower wing, install the engine that is used for driving the flight of whole aircraft through the installing support between top wing and the lower wing, the bottom symmetry of casing is provided with the support frame, the outer wall fixedly connected with backup pad of support frame, the backup pad is kept away from the one end of support frame outer wall and is installed the pivot seat, it is connected with the fly leaf to rotate through the pivot on the pivot seat, the outer wall of backup pad bonds through binding board and has the gasbag, be provided with the ignition who is used for opening the gasbag on the gasbag, the support frame is kept away from the one end of casing and is installed the gyro wheel, this high performance amphibian manned flight vehicle has realized amphibious's function, the performance when traveling has in aqueous been promoted, the condition that can not take place to turn on one's side, safe and reliable more.
Description
Technical field
This utility model is related to vehicle technology field, more particularly to a kind of amphibious manned vehicle of high-performance.
Background technology
In recent years, with science and technology continuous development, occur in that diversified aircraft, be applied to it is military, civilian,
The multiple fields such as amusement.With people's further seeking for for aircraft, it is desirable to which the aircraft of a new generation can adapt to various
Complicated landform, such as it is amphibious etc., but existing amphibious aircraft in water when travelling, and performance is not sufficiently stable,
Easily turn on one's side.
Utility model content
The purpose of this utility model is and a kind of high-performance land and water for proposing in order to solve shortcoming present in prior art
Dual-purpose manned vehicle, stable performance when the amphibious manned vehicle of the high-performance is travelled in water is not susceptible to rollover.
To achieve these goals, this utility model employs following technical scheme：
A kind of amphibious manned vehicle of high-performance, including housing are designed, the inner chamber of the housing is provided with for controlling
The control device of whole aircraft is made, the outer wall of the housing is symmetrically arranged with top wing and lower wing, and the top wing is with
The electromotor for driving whole aircraft flight is provided with by mounting bracket between wing, the bottom symmetrical of the housing sets
Bracing frame is equipped with, the outer wall of support frame as described above is fixedly connected with gripper shoe, and the gripper shoe is pacified away from one end of bracing frame outer wall
Equipped with shaft seat, portable plate is connected with by axis of rotation on shaft seat, the outer wall of the gripper shoe is bonded with by adhesive sheet
Air bag, is provided with the igniter for opening air bag on the air bag, support frame as described above is provided with rolling away from one end of housing
Wheel.
Preferably, the air bag includes interior air bag and the outer air bag being arranged on outside interior air bag, and igniter is arranged on
On interior air bag.
Preferably, the outer wall of the outer air bag is adopted in latticed being provided between multiple fixed columns, and multiple fixed columns
Connected with line is tightened.
Preferably, the outer wall of the gripper shoe is provided with baffle plate, and the outer wall of portable plate offers recessed with what baffle plate matched
Groove.
Preferably, the air bag is cuboid-type air bag, and the outer wall of air bag fits with the outer wall of portable plate.
Preferably, the igniter is electronic type igniter, and igniter is by wire and is arranged in housing
The control device connection in chamber.
The utility model proposes a kind of amphibious manned vehicle of high-performance, beneficial effect is：On bracing frame
Gripper shoe is provided with, the outer wall of gripper shoe is bonded with air bag by tack coat, and air bag includes outer air bag and interior air bag, on interior air bag
Igniter is provided with, when the manned vehicle needs from aerial steering water to travel, the control igniting of flying vehicles control device
By interior airbag-releasing, inside and outside air bag plays a part of to support aircraft on the water surface device, and now aircraft just can be in the water surface
Upper traveling, realizes the amphibious function of the aircraft, while gripper shoe and portable plate are provided with, when interior air bag is strutted,
Portable plate rotate and with gripper shoe clamping, increase the contact area between bracing frame and outer air bag, improve in water travel
When performance, will not occur turn on one's side situation, it is more safe and reliable.
Description of the drawings
Fig. 1 be the utility model proposes a kind of amphibious manned vehicle of high-performance structural representation；
Fig. 2 be the utility model proposes a kind of amphibious manned vehicle of high-performance A portions structural representation；
Fig. 3 be the utility model proposes a kind of amphibious manned vehicle of high-performance air bag sectional view.
In figure：1 housing, 2 top wings, 3 lower wings, 4 mounting brackets, 5 electromotors, 6 bracing frames, 7 rollers, 8 gripper shoes, 9
Shaft seat, 10 rotating shafts, 11 portable plates, 12 adhesive sheets, 13 air bags, 14 igniters, 15 outer air bags, air bag in 16,17 tighten line,
18 fixed columns.
Specific embodiment
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of this utility model, rather than whole
Embodiment.
Reference picture 1-3, a kind of amphibious manned vehicle of high-performance, including housing 1, the inner chamber of housing 1 is provided with use
In the control device for controlling whole aircraft, the outer wall of housing 1 is symmetrically arranged with top wing 2 and lower wing 3, and top wing 2 is with
The electromotor 5 for driving whole aircraft flight is provided with by mounting bracket 4 between wing 3, the bottom symmetrical of housing 1 sets
Bracing frame 6 is equipped with, the outer wall of bracing frame 6 is fixedly connected with gripper shoe 8, and gripper shoe 8 is provided with away from one end of the outer wall of bracing frame 6
Shaft seat 9, portable plate 11 is rotatably connected on shaft seat 9 by rotating shaft 10, and the outer wall of gripper shoe 8 is provided with baffle plate, portable plate
11 outer wall offers the groove matched with baffle plate.
The outer wall of gripper shoe 8 is bonded with air bag 13 by adhesive sheet 12, is provided with air bag 13 for opening air bag 13
Igniter 14, air bag 13 is cuboid-type air bag, and the outer wall of air bag 13 fits with the outer wall of portable plate 11, and bracing frame 6 is remote
One end of shrinking away from theshell body 1 is provided with roller 7, and air bag 13 includes interior air bag 16 and the outer air bag 15 being arranged on outside interior air bag 16, and
Igniter 14 is arranged on interior air bag 16, igniter 14 be electronic type igniter, and igniter 14 by wire with
The control device connection of the inner chamber of housing 1 is arranged on, when the manned vehicle needs from aerial steering water to travel, aircraft control
Device control igniter 14 processed opens in interior air bag 16, and inside and outside air bag plays a part of to support aircraft on the water surface, now
Aircraft just can sail on the water, and realize the amphibious function of the aircraft, and the outer wall of outer air bag 15 is in grid
Shape is provided between multiple fixed columns 18, and multiple fixed columns 18 and is connected using tightening line 17, and setting is tightened line 17 and prevents outer
The deformation quantity of air bag 15 causes greatly very much aircraft unstable, when interior air bag 16 is strutted, portable plate 11 rotate and with the clamping of gripper shoe 8,
The contact area between bracing frame 6 and outer air bag 15 is increased, the performance during traveling in water is improved, will not occur what is turned on one's side
Situation, it is more safe and reliable.
Operation principle：When the manned vehicle needs from aerial steering water to travel, flying vehicles control device control point
Fiery device 14 opens in interior air bag 16, and inside and outside air bag plays a part of to support aircraft on the water surface, and now aircraft just can be with
Sail on the water, realize the amphibious function of the aircraft, and stable performance.
The above, only this utility model preferably specific embodiment, but protection domain of the present utility model is not
Be confined to this, any those familiar with the art in the technical scope that this utility model is disclosed, according to this practicality
New technical scheme and its utility model design in addition equivalent or change, all should cover in protection model of the present utility model
Within enclosing.
Claims (6)
1. the amphibious manned vehicle of a kind of high-performance, including housing (1), it is characterised in that the inner chamber of the housing (1) sets
The control device for controlling whole aircraft is equipped with, the outer wall of the housing (1) is symmetrically arranged with top wing (2) and lower wing
(3), it is provided with for driving whole aircraft flight by mounting bracket (4) between the top wing (2) and lower wing (3)
Electromotor (5), the bottom symmetrical of the housing (1) is provided with bracing frame (6), and the outer wall of support frame as described above (6) is fixedly connected with
Gripper shoe (8), the gripper shoe (8) is provided with shaft seat (9) away from one end of bracing frame (6) outer wall, and shaft seat passes through on (9)
Rotating shaft (10) is rotatably connected to portable plate (11), and the outer wall of the gripper shoe (8) is bonded with air bag (13) by adhesive sheet (12),
The igniter (14) for opening air bag (13) is provided with the air bag (13), support frame as described above (6) is away from housing (1)
One end is provided with roller (7).
2. a kind of amphibious manned vehicle of high-performance according to claim 1, it is characterised in that the air bag (13)
Including interior air bag (16) and the outer air bag (15) being arranged on outside interior air bag (16), the igniter (14) is arranged on interior air bag
(16) on.
3. a kind of amphibious manned vehicle of high-performance according to claim 2, it is characterised in that the outer air bag
(15) outer wall is provided between multiple fixed columns (18), and multiple fixed columns (18) using tightening line (17) even in latticed
Connect.
4. a kind of amphibious manned vehicle of high-performance according to claim 1, it is characterised in that the gripper shoe
(8) outer wall is provided with baffle plate, and the outer wall of portable plate (11) offers the groove matched with baffle plate.
5. a kind of amphibious manned vehicle of high-performance according to claim 1, it is characterised in that the air bag (13)
Fit with the outer wall of portable plate (11) for cuboid-type air bag, and the outer wall of air bag (13).
6. a kind of amphibious manned vehicle of high-performance according to claim 1, it is characterised in that the igniter
(14) it is electronic type igniter, and igniter (14) is connected by wire with the control device for being arranged on housing (1) inner chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621120534.9U CN206086243U (en) | 2016-10-13 | 2016-10-13 | High performance amphibian manned flight vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621120534.9U CN206086243U (en) | 2016-10-13 | 2016-10-13 | High performance amphibian manned flight vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206086243U true CN206086243U (en) | 2017-04-12 |
Family
ID=58483772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621120534.9U Expired - Fee Related CN206086243U (en) | 2016-10-13 | 2016-10-13 | High performance amphibian manned flight vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206086243U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110893907A (en) * | 2018-09-12 | 2020-03-20 | 台山市金桥铝型材厂有限公司 | Unmanned aerial vehicle air bag and aluminium system unmanned aerial vehicle undercarriage |
| CN110893911A (en) * | 2018-09-12 | 2020-03-20 | 台山市金桥铝型材厂有限公司 | Parachute device and aluminium system multiaxis unmanned aerial vehicle |
-
2016
- 2016-10-13 CN CN201621120534.9U patent/CN206086243U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110893907A (en) * | 2018-09-12 | 2020-03-20 | 台山市金桥铝型材厂有限公司 | Unmanned aerial vehicle air bag and aluminium system unmanned aerial vehicle undercarriage |
| CN110893911A (en) * | 2018-09-12 | 2020-03-20 | 台山市金桥铝型材厂有限公司 | Parachute device and aluminium system multiaxis unmanned aerial vehicle |
| CN110893911B (en) * | 2018-09-12 | 2021-06-04 | 台山市金桥铝型材厂有限公司 | Aluminium system multiaxis unmanned aerial vehicle |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170412 Termination date: 20191013 |