CN2237597Y - Amphibious helicopter - Google Patents
Amphibious helicopter Download PDFInfo
- Publication number
- CN2237597Y CN2237597Y CN 95217770 CN95217770U CN2237597Y CN 2237597 Y CN2237597 Y CN 2237597Y CN 95217770 CN95217770 CN 95217770 CN 95217770 U CN95217770 U CN 95217770U CN 2237597 Y CN2237597 Y CN 2237597Y
- Authority
- CN
- China
- Prior art keywords
- wing
- screw propeller
- afterbody
- string edge
- sides
- 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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Abstract
The utility model relates to a 'symbiosis helicopter', which comprises propeller assemblies for vertically lifting, a turbojet engine and a barrel type screw propeller for aerial flight and water sailing. The utility model collects the advantages of an airplane, an automobile and a naval ship, and is a transportation tool for civil transportation and military transfer. The utility model has the advantages of fast running, flexible maneuver and safety, and achieves one machine with multiple functions. The symbiosis helicopter is an ideal vehicle.
Description
The utility model is the aircraft that belongs to advanced, particularly a kind of can be aloft, three helicopters of dwelling of waterborne, land use.
Current the most popular fast speed transatmospheric vehicle is an aircraft, needs sufficiently long runway and the service of other airports to establish when it takes off and revolves, and is generally far away apart from urban architecture in the world, because it needs the safety of certain spatial domain when guaranteeing to take off.Human desires is wanted to go out of the city by bus earlier by air, by plane in general, and at present, various vehicles are increasing on each big city street, and is especially very serious in traffic congestion in peak time on and off duty, meets traffic accident again, and desire to go out of the city and seize the opportunity, be extremely difficult really.In order to realize dream for many years, make the human vehicle that obtain a kind of more high-revolving, safety and reliability, the utility model proposes a kind of three of aerial, waterborne, land use helicopter of dwelling that is applicable to.
The utility model purpose is that aircraft, automobile, naval vessel three's advantage is concentrated on all over the body, proposes three of a kind of maneuverability that is applicable to aerial, waterborne, land use helicopter of dwelling.
The technical solution of the utility model is: this three helicopter of dwelling is made up of fuselage, the string edge wing, empennage, operator's compartment, Vertical Lift screw propeller, cartridge type screw propeller, turbojet engine, piston type electrical generator, parachute, wheel and control system parts.It is characterized in that: fuselage is the oblate main cabin of the length of center protrusion, and operator's compartment is than main cabin higher level, and the string edge wing (being equivalent to wing) is extended down to head in the both sides of fuselage from afterbody and joins, antenna is established in head the place ahead, to link up contact, empennage contains vertical tail and tailplane, its rudder face controlling party to.Three groups (by 8: 4: 4) are installed 16 Vertical Lift screw propellers altogether and are sunk in the string edge aerofoil from the front end to the portion on the string edge wing, and (can divide into groups to control), when taking off, this propellerpiston turns forward 45 °, and wing flap puts down to increase lift simultaneously; A turbojet engine is respectively installed in both sides on the afterbody string edge wing, flies forward so that powerful thrust to be provided; The electrical generator that piston engine drives also is installed directly over afterbody, and its power supply is supplied with the electric power of the cartridge type screw propeller on two on 16 Vertical Lift screw propeller chord edge wings.The in case of emergency available qi of chong channel ascending adversely of parachute is opened.
Cartridge type screw propeller one is to assist to fly forward in the air, the 2nd, need aloft slow down or during left alone without help staying, available prior left alone without help car or reversing realize.
The cartridge type screw propeller also can be used as the land power that travels, and 4 wheels have control to show as the walking support part during turning.Cartridge type screw propeller and turbojet driving engine start simultaneously, can be used as the power that advances waterborne, the belly navigation of keeping afloat.
This three advantage of dwelling helicopter is that the advantage of aerial, waterborne, land transportation means is concentrated on all over the body, realized rapidly, the purpose of safety, maneuverability, a tractor serves several purposes; It can left alone without helply be placed at any time, and building pushes up upward or in the hangar, this is the vehicle of civilian traffic and military the best of transferring, as, fire-fighting, watering, oiling, the disaster relief, handling etc.
The description of the drawings
Fig. 1 is three lateral plans of dwelling autogyro
Fig. 2 is three birds-eye vieies of dwelling autogyro
Fig. 3 is three front elevations of dwelling autogyro
Fig. 4 is three back views of dwelling autogyro
Below in conjunction with description of drawings most preferred embodiment of the present utility model:
The three helicopter main bodys of dwelling are fuselage (1), and fuselage is the oblate main cabin of the length of center protrusion, and operator's compartment (3), is hoped and handled for the Liao Dynasty than main cabin higher level in middle the place ahead; To be string edge wings (4) be extended down to head from afterbody in both sides joins, and antenna (14) is established for contact in head the place ahead, and empennage (13) contains vertical tail and tailplane, its rudder face controlling party to; Three groups (by 8: 4: 4) install 16 Vertical Lift screw propellers (2) and heavy being contained in the string edge aerofoil altogether from front end to portion in the string edge wing (4), can divide three groups of startings when taking off, and propellerpiston turns forward 45 °, and wing flap puts down to increase lift simultaneously.A turbo type jet engine (7) is respectively installed in both sides on the afterbody string edge wing, to produce powerful thrust; A piston engine also is installed to drive an electrical generator (10) directly over afterbody, its power supply is supplied with the electric power of the cartridge type screw propeller (6) on 16 Vertical Lift screw propellers (2) chord edge wing both sides.Parachute can be done manual work with urgent qi of chong channel ascending adversely.
The cartridge type screw propeller (6) of both sides also can be used as the land power that travels, and 4 wheels (12) have control display lamp (8) as the walking support part when turning to.Cartridge type screw propeller and turbojet driving engine start the power that travels as waterborne simultaneously, the belly navigation of keeping afloat.
Claims (1)
1, three helicopters of dwelling, comprise fuselage (1), the string edge wing (4), empennage (13), wing flap (14), operator's compartment (3), Vertical Lift screw propeller (2), cartridge type screw propeller (6), turbojet engine (7), piston type electrical generator (10), parachute (5), wheel (12) and control system parts thereof, it is characterized in that: fuselage is the oblate main cabin of the length of center protrusion, operator's compartment is than main cabin higher level, the string edge wing is extended down to head in the both sides of fuselage from afterbody and joins, head the place ahead is provided with antenna (14), empennage (13) contains vertical tail and tailplane, its rudder face controlling party to; In the string edge wing from the front end to the portion three groups---16 Vertical Lift screw propellers are installed altogether and are sunk in the string edge aerofoil, propellerpiston turns forward 45 ° when taking off, and wing flap (18) puts down simultaneously; A turbojet engine (7) is respectively installed in both sides on the afterbody string edge wing, the electrical generator that a piston engine drives also is installed directly over afterbody, and its power supply is supplied with the electric power of the cartridge type screw propeller (6) on 16 Vertical Lift screw propellers (2) chord edge wing both sides.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 95217770 CN2237597Y (en) | 1995-08-01 | 1995-08-01 | Amphibious helicopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 95217770 CN2237597Y (en) | 1995-08-01 | 1995-08-01 | Amphibious helicopter |
Publications (1)
Publication Number | Publication Date |
---|---|
CN2237597Y true CN2237597Y (en) | 1996-10-16 |
Family
ID=33866501
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 95217770 Expired - Fee Related CN2237597Y (en) | 1995-08-01 | 1995-08-01 | Amphibious helicopter |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN2237597Y (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102712347A (en) * | 2010-03-30 | 2012-10-03 | 水翼艇技术株式会社 | WIG craft having hybrid propulsion means |
CN102923256A (en) * | 2012-11-13 | 2013-02-13 | 浙江海洋学院 | Novel river-sea-through express ship |
CN103466066A (en) * | 2013-10-08 | 2013-12-25 | 洪满 | Water-attaching flying boat |
WO2015090071A1 (en) * | 2013-12-20 | 2015-06-25 | 胡新如 | Land and water flying automobile |
CN105564631A (en) * | 2016-03-06 | 2016-05-11 | 陈俞任 | Bullet shaped plane |
CN108698683A (en) * | 2015-08-31 | 2018-10-23 | 马里兰大学帕克分校 | In the air, the General Motors that the stability of safety operation gets a promotion in water and ground environment |
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 |
-
1995
- 1995-08-01 CN CN 95217770 patent/CN2237597Y/en not_active Expired - Fee Related
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102712347A (en) * | 2010-03-30 | 2012-10-03 | 水翼艇技术株式会社 | WIG craft having hybrid propulsion means |
CN102923256A (en) * | 2012-11-13 | 2013-02-13 | 浙江海洋学院 | Novel river-sea-through express ship |
CN103466066A (en) * | 2013-10-08 | 2013-12-25 | 洪满 | Water-attaching flying boat |
WO2015090071A1 (en) * | 2013-12-20 | 2015-06-25 | 胡新如 | Land and water flying automobile |
US9505282B2 (en) | 2013-12-20 | 2016-11-29 | Xinru HU | Amphibious flying car |
CN108698683A (en) * | 2015-08-31 | 2018-10-23 | 马里兰大学帕克分校 | In the air, the General Motors that the stability of safety operation gets a promotion in water and ground environment |
CN105564631A (en) * | 2016-03-06 | 2016-05-11 | 陈俞任 | Bullet shaped plane |
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 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |