CN205632001U - Triphibian aircraft - Google Patents
Triphibian aircraft Download PDFInfo
- Publication number
- CN205632001U CN205632001U CN201620462563.7U CN201620462563U CN205632001U CN 205632001 U CN205632001 U CN 205632001U CN 201620462563 U CN201620462563 U CN 201620462563U CN 205632001 U CN205632001 U CN 205632001U
- Authority
- CN
- China
- Prior art keywords
- car body
- wheel
- axletree
- flexible
- aircraft
- 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
Links
Landscapes
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
The utility model belongs to the technical field of flight equipment, concretely relates to triphibian aircraft. It includes automobile body and wheel, and the automobile body is equipped with the driver's cabin, and the automobile body is equipped with the gas dome all around, gas dome and compressor intercommunication, and the automobile body front portion is equipped with discharge chamber, and discharge chamber is equipped with the discharge, is equipped with ball bearing on the wheel, and ball bearing installs twisting of joints pivot through flexible axletree and car connection, flexible axletree both sides. This triphibian aircraft has a large amount of helium deposits to the gasbag is filled to application compression helium, and realized jet aircraft original place and gone up and down, adaptable multiple topography, and helium density is little, and the security is high, increases flight safety nature. Wheel, wing all adopt collapsible mode, have reduced the windage, have reduced unnecessary energy loss. Simultaneously, application twisting of joints pivot and ball bearing cooperation work have realized the rotatory twisting of joints pivot irrotational of axletree, and the wheel shrink has been realized to the flexible axletree of light cooperation, have also compensatied the not enough problem of wheel stability that hollow axle guide sent.
Description
Technical field
This utility model belongs to flight equipment technical field, is specifically related to a kind of three and dwells aircraft.
Background technology
Middle-size and small-size manned vehicle particularly light aerocraft is the least because of it, park and landing without big airport, obtaining at civil area in recent years and extensively apply and develop rapidly, and hovercar also has the trend of big research great development, these represent an important development direction of future transportation instrument.In the various small-sized manned vehicle schemes such as light aerocraft, ultra light aircraft, hovercar, seaplane class because having good comprehensive advantage without airport.But existing ground effect vehicle or seaplane there is also many in place of being not so good as people's will in terms of land use and high-altitude flight.
Utility model content
The purpose of this utility model is to provide a kind of production cost low, and safety coefficient is high, good stability, is suitable to three the three of flights of dwelling and dwells aircraft.
This utility model is achieved through the following technical solutions:
A kind of three dwell aircraft, are characterized in that and include car body 1 and wheel 2, and described car body 1 front portion is provided with driver's cabin 3, and driver's cabin 3 is arranged above high-strength armoured-glass 4；Car body 1 surrounding is provided with gas dome 5, and gas dome 5 connects with compressor 6, and compressor 6 exports connection has air bag 7, car body 1 front portion to be provided with drain chamber 8, and air bag 7 can be covered with whole drain chamber 8 after being full of, and drain chamber 8 is provided with import and export 9；Car body 1 rear portion is provided with main fuel tank 10 and auxiliary fuel tank 11, is separately installed with telescopic wing 12 and empennage 13 with afterbody in the middle part of car body 1；Described wheel 2 is provided with ball bearing 14, and ball bearing 14 is connected with car body 1 by flexible axletree 15, and flexible axletree 15 both sides are provided with twisting of joints rotating shaft 16, and twisting of joints rotating shaft 16 one end is fixed on flexible axletree 15 end, and the other end is fixed on ball bearing 14；Described car body 1 head and afterbody are equipped with car light 17.
Preferably, for saving fuel oil cost, adapting to the flight of different geographical, described car body 1 is provided with fanjet 18 and diesel engine 19, fanjet 18 is connected with the auxiliary fuel tank 11 equipped with aerial kerosene, and diesel engine 19 is connected with the main fuel tank 10 equipped with diesel oil.
This three aircraft of dwelling has a substantial amounts of helium deposit, and uses compressed helium to fill air bag, it is achieved that jet aircraft original place lifts, and is suitable for multiple landform, and helium density is little, and safety is high, increases flight safety.Wheel, wing all use collapsible pattern, reduce windage, decrease unnecessary energy loss.Meanwhile, use twisting of joints rotating shaft and ball-bearing fit work to achieve axletree rotation twisting of joints rotating shaft and do not rotate, easily coordinate flexible axletree to achieve wheel and shrink, the problem that also compensate for the wheel stability deficiency that hollow axle causes.
Accompanying drawing explanation
Fig. 1: three structural representations dwelling aircraft；
Fig. 2: compressor and the connection diagram of drain chamber；
Fig. 3: car wheel structure schematic diagram；
In figure: 1: car body；2: wheel；3: driver's cabin；4: high-strength armoured-glass；5: gas dome；6: compressor；7: air bag；8: drain chamber；9: import and export；10: main fuel tank；11: auxiliary fuel tank；12: wing；13: empennage；14: ball bearing；15: flexible axletree；16: twisting of joints rotating shaft；17: car light；18: fanjet；19: diesel engine.
Detailed description of the invention
Referring to the drawings, provide detailed description of the invention of the present utility model, be used for structure of the present utility model is further described.
Embodiment 1
The three of the present embodiment are dwelt aircraft, 1-3 referring to the drawings, including car body 1 and wheel 2, described car body 1 front portion is provided with driver's cabin 3, driver's cabin 3 is arranged above high-strength armoured-glass 4, both can expand driving vision, again can when there is emergency also can the whole ejection in top, facilitate human pilot to launch hedging.
Car body 1 surrounding is provided with gas dome 5, gas dome 5 connects with compressor 6, compressor 6 exports connection air bag 7, car body 1 front portion is provided with drain chamber 8, air bag 7 can be covered with whole drain chamber 8 after being full of, drain chamber 8 is provided with import and export 9, and in can discharging car by import and export 9, air reduces car body density or is filled with air increase car body density.
Car body 1 rear portion is provided with main fuel tank 10 and auxiliary fuel tank 11, and main fuel tank 10 is built with diesel oil, and auxiliary fuel tank 11, built with aerial kerosene, is separately installed with telescopic wing 12 and empennage 13 with afterbody in the middle part of car body 1, in order to aloft fly.
Additionally, car body 1 head and afterbody are equipped with car light 17, it is used for travelling illumination.
Wheel 2 is provided with ball bearing 14, and ball bearing 14 is connected with car body 1 by flexible axletree 15, and flexible axletree 15 both sides are provided with twisting of joints rotating shaft 16, and twisting of joints rotating shaft 16 one end is fixed on flexible axletree 15 end, and the other end is fixed on ball bearing 14.
During aircraft preparation hole flight, compressor operating also discharges high intensity compressed helium, helium is filled with air bag, air bag is full of drain chamber, simultaneously by importing and exporting the air discharge in car body, overall vehicle density is made to be slightly less than air, car body can rise and hover over overhead to be had on the height of certain distance, now wing and empennage launch, fanjet works, fuel is made with the aerial kerosene in auxiliary fuel tank, fuel combustion produces onward impulse, wing and the upper and lower pressure difference of empennage produce climbing power, the now helium recovery in air bag compressing, import and export are filled with air, prevent high-altitude pressure official post air bag damaged.
When landing prepares land locomotion, shunk by twisting of joints rotating shaft and flexible axletree, compressor release high intensity compressed helium, helium is filled with air bag, and wheel reclaims, and wing and empennage are regained, fanjet cuts out, and aircraft hovers in the air, regains air bag afterwards, it is filled with air by import and export, aircraft slowly lands, and wheel ejects, now diesel engine work, using the diesel oil in main fuel tank as fuel, vehicle wheel rotation starts land and exercises.Wherein, use twisting of joints rotating shaft and ball-bearing fit work to achieve axletree rotation twisting of joints rotating shaft and do not rotate, maintain wheel stability substantially.
When entering water, aircraft first hangs and is parked in the air, and wheel bounces back, compressor release high intensity compressed helium, helium is filled with air bag, and aircraft is suspended on the water surface, and import and export are opened and are filled with water, increase car body density, the optional position that car body sinks and hovers in certain depth, now diesel engine work, using the diesel oil in main fuel tank as fuel, produce onward impulse, reach the purpose advanced under water.
Vehicle body uses low-density and high-strength steel to make, and wing and empennage end all use titanium alloy, and fanjet is small-sized low horsepower engine, effectively reduces the manufacturing cost of aircraft car body.
Embodiment 2
The three of the present embodiment are dwelt aircraft, its structure is basically identical with embodiment 1, difference is for saving fuel oil cost, adapt to the flight of different geographical, fanjet 18 and diesel engine 19 it is provided with on described car body 1, fanjet 18 is connected with the auxiliary fuel tank 11 equipped with aerial kerosene, and diesel engine 19 is connected with the main fuel tank 10 equipped with diesel oil.
This utility model three aircraft of dwelling has a substantial amounts of helium deposit, and uses compressed helium to fill air bag, it is achieved that jet aircraft original place lifts, and is suitable for multiple landform, and helium density is little, and safety is high, increases flight safety.Wheel, wing all use collapsible pattern, reduce windage, decrease unnecessary energy loss.Meanwhile, use twisting of joints rotating shaft and ball-bearing fit work to achieve axletree rotation twisting of joints rotating shaft and do not rotate, easily coordinate flexible axletree to achieve wheel and shrink, the problem that also compensate for the wheel stability deficiency that hollow axle causes.Additionally, be provided with the auxiliary fuel tank holding aerial kerosene and the main fuel tank holding diesel oil, ground and under water with diesel oil, flying overhead aerial kerosene, and car body design have many spaces and empty room, materials are less, greatly the manufacturing cost of reduction aircraft.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model, all within spirit of the present utility model and principle, any modification, equivalent substitution and improvement etc. made, within the scope of should be included in environmental protection of the present utility model.
Claims (2)
1. an aircraft of dwelling, it is characterised in that: including car body (1) and wheel (2), described car body (1) front portion is provided with driver's cabin (3), and driver's cabin (3) is arranged above high-strength armoured-glass (4)；Car body (1) surrounding is provided with gas dome (5), gas dome (5) connects with compressor (6), compressor (6) outlet connection has air bag (7), car body (1) front portion is provided with drain chamber (8), air bag (7) can be covered with whole drain chamber (8) after being full of, and drain chamber (8) is provided with import and export (9)；Car body (1) rear portion is provided with main fuel tank (10) and auxiliary fuel tank (11), and car body (1) middle part and afterbody are separately installed with telescopic wing (12) and empennage (13)；Described wheel (2) is provided with ball bearing (14), ball bearing (14) is connected with car body (1) by flexible axletree (15), flexible axletree (15) both sides are provided with twisting of joints rotating shaft (16), twisting of joints rotating shaft (16) one end is fixed on flexible axletree (15) end, and the other end is fixed on ball bearing (14)；Described car body (1) head and afterbody are equipped with car light (17).
The most as claimed in claim 1 three dwell aircraft, it is characterized in that: on described car body (1), be provided with fanjet (18) and diesel engine (19), fanjet (18) is connected with the auxiliary fuel tank (11) equipped with aerial kerosene, and diesel engine (19) is connected with the main fuel tank (10) equipped with diesel oil.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620462563.7U CN205632001U (en) | 2016-05-20 | 2016-05-20 | Triphibian aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620462563.7U CN205632001U (en) | 2016-05-20 | 2016-05-20 | Triphibian aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205632001U true CN205632001U (en) | 2016-10-12 |
Family
ID=57054040
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620462563.7U Expired - Fee Related CN205632001U (en) | 2016-05-20 | 2016-05-20 | Triphibian aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205632001U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110744978A (en) * | 2018-07-22 | 2020-02-04 | 上海天轩科技发展有限公司 | Boosting triphibian coaxial double-rotor wing vertical lift aerobat |
| CN114775972A (en) * | 2022-05-18 | 2022-07-22 | 孙强 | Beautiful seam device of ceramic tile for building |
-
2016
- 2016-05-20 CN CN201620462563.7U patent/CN205632001U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110744978A (en) * | 2018-07-22 | 2020-02-04 | 上海天轩科技发展有限公司 | Boosting triphibian coaxial double-rotor wing vertical lift aerobat |
| CN114775972A (en) * | 2022-05-18 | 2022-07-22 | 孙强 | Beautiful seam device of ceramic tile for building |
| CN114775972B (en) * | 2022-05-18 | 2023-09-05 | 四川华西宜宾建设有限公司 | Ceramic tile seam beautifying device for building |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107984992A (en) | It is a kind of can VTOL land and air double-used vehicle | |
| CN101885295A (en) | Land and air double-used aircraft | |
| CN103496305A (en) | Hovercar | |
| CN108146169A (en) | The land and air double-used vehicle of folding after a kind of wing | |
| CN101367435A (en) | Novel air injection aerial vehicle | |
| CN105730170B (en) | Four culvert vertical take-off and landing hovercars | |
| CN203528804U (en) | Large-size rescue amphibious aircraft | |
| CN101365624A (en) | Ground air water craft | |
| CN103770589B (en) | Hovercar | |
| DE102019001130B3 (en) | Wheel propellers and vehicles with wheel propellers | |
| CN103552435A (en) | Multi-jet self-balancing aerocar | |
| CN209257804U (en) | A kind of folding hovercar of VTOL wing | |
| CN108437715A (en) | A kind of emergency management and rescue hovercar | |
| CN104723816B (en) | The aerodynamic arrangement and power configuration embodiment of land and air double-used car and officer's car | |
| CN106184741A (en) | A kind of flying wing type ducted fan VUAV | |
| CN109606605A (en) | A kind of more rotor combined type aircraft of dirigible | |
| CN202528786U (en) | Ground effect type extreme low-altitude dual-purpose flying car | |
| CN102649391A (en) | Ground-effect type extreme low-altitude dual-purpose aerocar or dual-purpose aircraft | |
| CN105730168B (en) | Three culvert vertical take-off and landing hovercars | |
| CN108177491A (en) | One kind can vertical take-off and landing flying car | |
| CN205632001U (en) | Triphibian aircraft | |
| CN108501639A (en) | A kind of hovercar | |
| CN108100207B (en) | Inflatable VTOL aircraft | |
| CN101857087A (en) | Dual-rotor dish-shaped aircraft | |
| CN101774429A (en) | Small UAV aerodynamic layout for vertical rope-type recovery |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161012 Termination date: 20170520 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |