CN101607596A - The power delta wing aircraft of a kind of suitable water, the amphibious landing flight in land - Google Patents
The power delta wing aircraft of a kind of suitable water, the amphibious landing flight in land Download PDFInfo
- Publication number
- CN101607596A CN101607596A CNA2008100315063A CN200810031506A CN101607596A CN 101607596 A CN101607596 A CN 101607596A CN A2008100315063 A CNA2008100315063 A CN A2008100315063A CN 200810031506 A CN200810031506 A CN 200810031506A CN 101607596 A CN101607596 A CN 101607596A
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- CN
- China
- Prior art keywords
- landing
- bottom platform
- land
- wing aircraft
- wheel apparatus
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
- B64C31/032—Hang-glider-type aircraft; Microlight-type aircraft having delta shaped wing
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/54—Floats
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/008—Amphibious sea planes
Abstract
The invention discloses a kind of suitable water, the power delta wing aircraft of the amphibious landing flight in land, comprise bottom platform, this bottom platform links to each other with wing by steering unit, the carrying support is installed on the bottom platform, the front end of this carrying support is provided with occupant position, driving engine is installed in the rear end of this carrying support, driving engine connecting bolt oar, the bottom of described bottom platform is equipped with contractile landing landing wheel apparatus, described steering unit is connected with described landing landing wheel apparatus, when stretching out by steering unit control landing landing wheel apparatus, this power delta wing aircraft can be in the land landing, when being recovered to bottom platform inside by steering unit control landing landing wheel apparatus, this power delta wing aircraft can be implemented in water surface landing.
Description
Technical field
The present invention relates to a kind of power delta wing aircraft, the power delta wing aircraft of particularly a kind of suitable water, the amphibious landing flight in land can make a kind of power delta wing aircraft can realize that the land landing can be implemented in water surface landing, glide again simultaneously.
Background technology
As shown in Figure 1, be existing a kind of power delta wing aircraft, it mainly adopts stent-type bottom platform 15, adds streamlined reefer housing 14, fixed type landing wheel apparatus 16, and top is equipped with delta wing 11, steering unit 12, driving engine 13.Because what it adopted is the bottom section of stent-type bottom platform 15 and fixed type landing wheel apparatus 16, it can only carry out landing on land, can not can not glide at the water surface in water surface landing.
As shown in Figure 2, be another kind of available dynamic delta wing aircraft, it mainly adopts buoyant material bottom platform 25, and as the device in water surface landing, top is equipped with delta wing 21, steering unit 22, driving engine 23 and support frame 24 etc.Because it makes the device of water surface landing with buoyant material bottom platform 25, the wheel apparatus that do not land, so it can only can not carry out landing at the water surface on land and fly, it can glide at the water surface, but velocity ratio is lower.
Therefore, existing two kinds of power delta wing aircraft all do not possess the function of water, the amphibious landing flight in land.
Summary of the invention
Technical matters to be solved by this invention is at the deficiency of existing power delta wing aircraft, to provide the power delta wing aircraft of a kind of suitable water, the amphibious landing flight in land, the expanding function range of use.
For solving the problems of the technologies described above, the technical solution adopted in the present invention is: a kind of suitable water, the power delta wing aircraft of the amphibious landing flight in land, comprise bottom platform, this bottom platform links to each other with wing by steering unit, the carrying support is installed on the bottom platform, the front end of this carrying support is provided with occupant position, driving engine is installed in the rear end of this carrying support, driving engine connecting bolt oar, the bottom of described bottom platform is equipped with contractile landing landing wheel apparatus, described steering unit is connected with described landing landing wheel apparatus, when stretching out by steering unit control landing landing wheel apparatus, this power delta wing aircraft can be in the land landing, and when being recovered to bottom platform inside by steering unit control landing landing wheel apparatus, this power delta wing aircraft can be implemented in water surface landing.
Compared with prior art, beneficial effect of the present invention is: the present invention adopts bottom platform, and contractile landing landing wheel apparatus is installed in the bottom of bottom platform, when landing landing wheel apparatus stretches out, the present invention can be in the land landing, when landing landing wheel apparatus is recovered to bottom platform inside, utilize bottom platform can realize that the present invention is in water surface landing, glide, thereby make the present invention can realize that land landing flight can realize water surface landing flight again, has expanded the range of use of power delta wing aircraft.
Description of drawings:
Fig. 1 is existing frame bottom platform power delta wing Flight Vehicle Structure scheme drawing.
Fig. 2 is existing buoyant material bottom platform power delta wing Flight Vehicle Structure scheme drawing.
Fig. 3 is a structural representation of the present invention.
The specific embodiment:
As shown in Figure 3, the present invention includes bottom platform 1, this bottom platform 1 is a ship shape, and makes moulding, embedded reinforcement girth reinforcing plate structure by epoxy resin and enhancing complex fiber material.This bottom platform 1 links to each other with steering unit 3 by bearing pin, steering unit 3 links to each other with wing 4 by bearing pin, the bottom of bottom platform 1 is equipped with collapsible landing landing wheel apparatus 2, this landing landing wheel apparatus 2 is the wheel body of three distributions triangular in shape, and steering unit 3 connects this landing landing wheel apparatus 2.When landing landing wheel apparatus 2 stretched out, the present invention can when landing landing wheel apparatus 2 is recovered to bottom platform 1 inside, utilize bottom platform 1 the present invention can be implemented in water surface landing in the land landing.The inside of bottom platform 1 is equipped with carrying support 5, this carrying support 5 is main load-carrying elements, and the front end of carrying support 5 is an occupant position 8, and driving engine 6 is installed in the rear end of carrying support 5, driving engine 6 connecting bolt oars 7, driving engine 6 provides flight thrust by screw propeller 7.
When the present invention uses, just in flight course of the present invention, control stretching out and withdrawal of contractile landing landing wheel apparatus 2 by control steering unit 3.When needs carry out landing on land, contractile landing landing wheel apparatus 2 is stretched out, on the land that meets the landing requirement,, can realize the steady landing flight of the present invention on land according to correct landing operation requirements; When needs when the water surface carries out landing, contractile landing landing wheel apparatus 2 is recovered to the inside of bottom platform 1, one complete hull is formed on the bottom of bottom platform 1, at the water surface that meets the landing requirement, according to correct landing operation requirements, can realize steady landing flight and the fast glide of the present invention at the water surface.
In order to improve performance of the present invention, bottom platform 1 has been taken all factors into consideration naval hydrodynamics and flight dynamics, carried out optimal design, guarantee the airworthiness of power delta wing aircraft excellence and at the gliding ability and the takeoff and landing performance of the fast and stable of the water surface.
Claims (3)
1, a kind of suitable water, the power delta wing aircraft of the amphibious landing flight in land, comprise bottom platform (1), this bottom platform (1) links to each other with wing (4) by steering unit (3), carrying support (5) is installed on the bottom platform (1), the front end of this carrying support (5) is provided with occupant position (8), driving engine (6) is installed in the rear end of this carrying support (5), driving engine (6) connecting bolt oar (7), it is characterized in that, the bottom of described bottom platform (1) is equipped with contractile landing landing wheel apparatus (2), described steering unit (3) is connected with described landing landing wheel apparatus (2), when controlling landing landing wheel apparatus (2) when stretching out by steering unit (3), this power delta wing aircraft can be in the land landing, when being recovered to bottom platform (1) inside by steering unit (3) control landing landing wheel apparatus (2), this power delta wing aircraft can be implemented in water surface landing.
2. the power delta wing aircraft of a kind of suitable water as claimed in claim 1, the amphibious landing flight in land is characterized in that described bottom platform (1) is a ship shape, and by epoxy resin and the manufacturing of enhancing complex fiber material.
3. the power delta wing aircraft of a kind of suitable water as claimed in claim 1 or 2, the amphibious landing flight in land is characterized in that described landing landing wheel apparatus (2) is the wheel body of three distributions triangular in shape.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2008100315063A CN101607596A (en) | 2008-06-16 | 2008-06-16 | The power delta wing aircraft of a kind of suitable water, the amphibious landing flight in land |
| PCT/CN2009/072263 WO2009152750A1 (en) | 2008-06-16 | 2009-06-15 | Amphibious powered delta-wing aircraft capable of taking off and landing both on water and on land |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2008100315063A CN101607596A (en) | 2008-06-16 | 2008-06-16 | The power delta wing aircraft of a kind of suitable water, the amphibious landing flight in land |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101607596A true CN101607596A (en) | 2009-12-23 |
Family
ID=41433697
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2008100315063A Pending CN101607596A (en) | 2008-06-16 | 2008-06-16 | The power delta wing aircraft of a kind of suitable water, the amphibious landing flight in land |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN101607596A (en) |
| WO (1) | WO2009152750A1 (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106218333A (en) * | 2015-11-10 | 2016-12-14 | 刘思佳 | Pure electronic hovercar |
| CN106671713A (en) * | 2015-11-10 | 2017-05-17 | 刘思佳 | Pure electric flying car |
| CN106671712A (en) * | 2015-11-10 | 2017-05-17 | 刘思佳 | Flight electric vehicle |
| CN109795686A (en) * | 2019-03-13 | 2019-05-24 | 青岛翼飞冲天科技有限公司 | Dalta wing airship waterborne |
| CN110341405A (en) * | 2019-07-09 | 2019-10-18 | 西安理工大学 | A kind of imitative amphibious walking robot of basilisk lizard |
| JP2020157816A (en) * | 2019-03-25 | 2020-10-01 | 高木 英治 | Ground surface effect sliding machine |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2485537B8 (en) * | 2010-11-16 | 2013-05-15 | Alan Kirtley | Integral - surface and air - personal transport |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2562490A (en) * | 1945-06-30 | 1951-07-31 | Theodore P Hall | Convertible car-airplane |
| US6131848A (en) * | 1997-10-02 | 2000-10-17 | Crow; Steven Collins | Roadable airplane drive through an automotive transaxle |
| US20020125367A1 (en) * | 2001-03-12 | 2002-09-12 | Killingsworth Norman Don | Combination fixed and rotating wing aircraft, land vehicle and water craft |
| CN2642674Y (en) * | 2003-10-17 | 2004-09-22 | 吴征 | Hull type amphibious super-light airplane with two seats arranged longitudinally |
| CN2695270Y (en) * | 2004-05-11 | 2005-04-27 | 陈星� | Triphibian aircraft with vehicle, ship and plane function |
| CN1915696A (en) * | 2006-07-03 | 2007-02-21 | 深圳市金福娃智能科技有限公司 | Integrated foldaway locomotory apparatus suitable to land, ice, snow, water, and air |
| CN201224498Y (en) * | 2008-06-16 | 2009-04-22 | 湖南山河科技股份有限公司 | Power delta wing aerocraft suitable for amphibious takeoff and landing |
-
2008
- 2008-06-16 CN CNA2008100315063A patent/CN101607596A/en active Pending
-
2009
- 2009-06-15 WO PCT/CN2009/072263 patent/WO2009152750A1/en active Application Filing
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106218333A (en) * | 2015-11-10 | 2016-12-14 | 刘思佳 | Pure electronic hovercar |
| CN106671713A (en) * | 2015-11-10 | 2017-05-17 | 刘思佳 | Pure electric flying car |
| CN106671712A (en) * | 2015-11-10 | 2017-05-17 | 刘思佳 | Flight electric vehicle |
| CN106671713B (en) * | 2015-11-10 | 2020-01-03 | 刘思佳 | Pure electric aerocar |
| CN106671712B (en) * | 2015-11-10 | 2020-01-07 | 刘思佳 | Flying electric vehicle |
| CN109795686A (en) * | 2019-03-13 | 2019-05-24 | 青岛翼飞冲天科技有限公司 | Dalta wing airship waterborne |
| CN109795686B (en) * | 2019-03-13 | 2024-01-09 | 青岛翼飞冲天科技有限公司 | Waterborne delta wing airship |
| JP2020157816A (en) * | 2019-03-25 | 2020-10-01 | 高木 英治 | Ground surface effect sliding machine |
| CN110341405A (en) * | 2019-07-09 | 2019-10-18 | 西安理工大学 | A kind of imitative amphibious walking robot of basilisk lizard |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2009152750A1 (en) | 2009-12-23 |
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| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Open date: 20091223 |