CN105857596A - Vertical-rising land-benefit amphibious aircraft construction method - Google Patents
Vertical-rising land-benefit amphibious aircraft construction method Download PDFInfo
- Publication number
- CN105857596A CN105857596A CN201610292023.3A CN201610292023A CN105857596A CN 105857596 A CN105857596 A CN 105857596A CN 201610292023 A CN201610292023 A CN 201610292023A CN 105857596 A CN105857596 A CN 105857596A
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- CN
- China
- Prior art keywords
- aircraft
- power source
- airplane
- tunnel type
- wind
- 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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Links
- 238000010276 construction Methods 0.000 title abstract 3
- 238000000034 method Methods 0.000 claims abstract description 12
- 241000272525 Anas platyrhynchos Species 0.000 claims abstract description 9
- 210000001015 abdomen Anatomy 0.000 claims abstract description 9
- 230000003068 static effect Effects 0.000 claims description 4
- 230000001105 regulatory effect Effects 0.000 claims description 2
- 230000000630 rising effect Effects 0.000 abstract 1
- 230000002153 concerted effect Effects 0.000 description 10
- 241000237858 Gastropoda Species 0.000 description 4
- 230000005484 gravity Effects 0.000 description 2
- 230000033001 locomotion Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
- B64D2041/002—Mounting arrangements for auxiliary power units (APU's)
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
The invention provides a vertical-rising land-benefit amphibious aircraft construction method, and relates to a novel airplane construction method. In order to solve the technical problems, the method comprises the steps that a direct power source of an airplane is installed in a wind tunnel type airplane body, and a high-speed airflow is produced by the direct power source in the wind tunnel type airplane body to serve as a second power source to improve the vertical rising function of the airplane; in order to capture and utilize the second power source, tension-resistance stretchable films are installed on the inner wall of the upper portion of the wind tunnel type airplane body, and differential pressure generated inside and outside the tension-resistance stretchable films form the second power source for propelling flying of the airplane; in order to effectively adjust and control the second power source, adjusting air bags are installed at a high-speed airflow inlet of the airplane to adjust and control the second power source; in order to increase the benefit of the airplane and the amphibious function, a duck abdomen type cargo cabin is installed on the outer wall of the lower portion of the wind tunnel type airplane body of the airplane. Accordingly, the airplane has good buoyancy and cargo carrying space, and by means of the duck abdomen type cargo cabin, good land benefit can be achieved, and the land benefit can be utilized by the cargo cabin and wings more effectively.
Description
Technical field
The present invention relates to the constructive method of a kind of type aircraft, i.e. go straight up to ground benefit amphibious aircraft constructive method.
Background technology
Currently known aircraft is used mostly the reaction force power as aircraft of screw or jet, and efficiency low-function is poor, especially
It is that jet power is not easy the power as helicopter.
Summary of the invention
In order to overcome the deficiency of existing aircraft, the present invention provides the constructive method of a kind of type aircraft, i.e. goes straight up to ground benefit amphibious
Aircraft constructive method, the method use the reaction force of screw or jet as aircraft direct driving force source simultaneously, then make it produce
Air-flow produce as the second power source and make a concerted effort common advance aircraft flight and increase aircraft vertical and play drop.
The present invention solves the scheme that its technical problem used: the direct driving force source of this aircraft is arranged in wind-tunnel type body,
Make its high velocity air produced in wind-tunnel type body as the second power source.Catch and utilize the second power source, Wo Men to flutter
Wind-tunnel type body upper inwall installs stretching resistance Flexible film.It is static pressure between stretching resistance Flexible film and wind-tunnel type body inwall, and tension
High velocity air outside power Flexible film produces dynamic pressure to stretching resistance Flexible film and is significantly less than static pressure.The inside and outside pressure produced of stretching resistance Flexible film
Difference pushes the rightabout of high velocity air to stretching resistance Flexible film and the wind-tunnel type body that is installed together with it, is formed and advances aircraft
Second power source of flight.Direct driving force source and the second power source produce makes a concerted effort, and makes this aircraft have the ability VTOL.In order to effectively
Regulation controls stretching resistance Flexible film and forms the second power source, and we are at this aircraft high velocity air entrance, in wind-tunnel type body and tension
Between power Flexible film, the regulation air bag being similar to tube is installed, by regulating the relaxation of air bag, controls stretching resistance Flexible film
Relaxation, regulation controls the second power source.Because the second power source is to be produced by 360 degree of wind-tunnel type bodies of periphery and stretching resistance Flexible film
Raw makes a concerted effort what union centre to centre heart line was formed, so wind-tunnel type body center line is exactly, the center line of the second power source power is also with straight
Connecing power source and form identical the making a concerted effort in direction, the centrostigma made a concerted effort the second power source near aircraft top (stretch to by the direction i.e. made a concerted effort
Aircraft top sky).The weight (center of gravity) of aircraft is the direct driving force source of bottom in this aircraft wind-tunnel type body.So, root
According to object of which movement law, when make a concerted effort more than centrifugal force and in opposite direction with centrifugal force time, carrier can be made with joint efforts to the earth's core phase negative side
To motion, carry when making a concerted effort aircraft enter aerial time, due to make a concerted effort centrostigma center of gravity surface (i.e. make a concerted effort direction stretch to
Aircraft top sky), which forms aircraft skyborne tumbler pattern, the safest stable mode i.e. gone straight up to, the most not
Separately add external force and can not change the pattern of aircraft orthostatism aloft.When aircraft horizontal flight, reduce to improve air speed
Flight resistance, aircraft needs to extract the air in regulation air bag out, makes stretching resistance Flexible film be close to wind-tunnel type body inwall.Aircraft relies on
Direct driving force and airfoil lift high-speed flight.In order to increase this aircraft ground benefit and amphibious function, we are at this aircraft wind-tunnel
Type underpart outer wall installs roomy duck abdomen type cargo hold.This aircraft is made not only to have good buoyancy and cargo space but also it is roomy
Duck abdomen type cargo hold can also produce good ground benefit and together with wing more effective profit land-use utility, thus substantially increase
The loading capacity of this aircraft and the scope of application.
The invention has the beneficial effects as follows the new method being found that flight gone straight up to by aircraft, open the frontier of aircraft flight transport.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the vertical section structural map of the present embodiment.
1. wind-tunnel type body, 2. stretching resistance Flexible film in figure, 3. regulation air bag, 4. four snail fan engines, 5. control system, 6.
Wing, 7. duck abdomen type cargo hold, 8. undercarriage.
Detailed description of the invention:
In FIG, wind-tunnel type body (1) upper inside wall installs stretching resistance Flexible film (2), wind-tunnel type body (1) and tension
Install between power Flexible film (2) and regulate air bag (3), uniform four snail fan engines (4) in wind-tunnel type body (1), four
Installation control system (5) in the middle of snail fan engine (4), wing (6) crosses wind-tunnel type body (1) and not only strengthens wind-tunnel type
Body (1) and make four snail fan engines (4) position simple, wind-tunnel type body (1) bottom outer wall install duck abdomen type
Cargo hold (7), undercarriage (8) is installed in duck abdomen type cargo hold (7) bottom.
Claims (4)
1. go straight up to ground benefit amphibious aircraft constructive method, it is characterized in that: the direct driving force source of this aircraft is arranged on wind-tunnel type body
In so that it is the high velocity air produced in wind-tunnel type body increases aircraft vertical as the second power source and plays drop.
The most according to claim 1 go straight up to ground benefit amphibious aircraft constructive method, it is characterized in that: catch and utilize the to flutter
Two power sources, we install stretching resistance Flexible film, stretching resistance Flexible film and wind-tunnel type body inwall at wind-tunnel type body upper inwall
Between be static pressure, and the high velocity air outside stretching resistance Flexible film to stretching resistance Flexible film produce dynamic pressure be significantly less than static pressure, stretching resistance is stretched
The inside and outside pressure reduction produced of contracting film pushes the phase negative side of high velocity air to stretching resistance Flexible film and the wind-tunnel type body that is installed together with it
To, form the second power source advancing aircraft flight.
The most according to claim 1 go straight up to ground benefit amphibious aircraft constructive method, it is characterized in that: in order to effectively regulate control
Stretching resistance Flexible film forms the second power source, and we are at this aircraft high velocity air entrance, at wind-tunnel type body and stretching resistance Flexible film
Between, the regulation air bag of similar tube is installed, by regulating the relaxation of air bag, control the relaxation of stretching resistance Flexible film, adjust
Joint controls the second power source.
The most according to claim 1 go straight up to ground benefit amphibious aircraft constructive method, it is characterized in that: in order to increase this aircraft ground
Benefit and amphibious function, we install roomy duck abdomen type cargo hold at this aircraft wind-tunnel type underpart outer wall.Make this aircraft
Not only there are good buoyancy and cargo space but also its roomy duck abdomen type cargo hold can also produce good ground benefit and together with wing
More effectively profit land-use utility.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610292023.3A CN105857596A (en) | 2016-05-05 | 2016-05-05 | Vertical-rising land-benefit amphibious aircraft construction method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610292023.3A CN105857596A (en) | 2016-05-05 | 2016-05-05 | Vertical-rising land-benefit amphibious aircraft construction method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105857596A true CN105857596A (en) | 2016-08-17 |
Family
ID=56631201
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610292023.3A Pending CN105857596A (en) | 2016-05-05 | 2016-05-05 | Vertical-rising land-benefit amphibious aircraft construction method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105857596A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2012511C1 (en) * | 1993-08-31 | 1994-05-15 | Фирма "ВИСТ" | Hybrid flying vehicle |
| CN2646046Y (en) * | 2003-02-08 | 2004-10-06 | 杨清太 | Novel helicopter |
| CN1944188A (en) * | 2005-10-03 | 2007-04-11 | 王新云 | Aircraft with centrifugal fan capable of vertically taking off and landing |
| RO127094A2 (en) * | 2010-08-18 | 2012-02-28 | Marius Brebenel | Lenticular aircraft with blades |
-
2016
- 2016-05-05 CN CN201610292023.3A patent/CN105857596A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2012511C1 (en) * | 1993-08-31 | 1994-05-15 | Фирма "ВИСТ" | Hybrid flying vehicle |
| CN2646046Y (en) * | 2003-02-08 | 2004-10-06 | 杨清太 | Novel helicopter |
| CN1944188A (en) * | 2005-10-03 | 2007-04-11 | 王新云 | Aircraft with centrifugal fan capable of vertically taking off and landing |
| RO127094A2 (en) * | 2010-08-18 | 2012-02-28 | Marius Brebenel | Lenticular aircraft with blades |
| RO127094B1 (en) * | 2010-08-18 | 2015-11-27 | Marius Brebenel | Lenticular aircraft with blades |
Non-Patent Citations (1)
| Title |
|---|
| 陈浮等: "《空气动力学基础》", 31 January 2015, 哈尔滨工业大学出版社 * |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160817 |
|
| RJ01 | Rejection of invention patent application after publication |