CN107444662A - Three-dimensional aircraft - Google Patents
Three-dimensional aircraft Download PDFInfo
- Publication number
- CN107444662A CN107444662A CN201710871243.6A CN201710871243A CN107444662A CN 107444662 A CN107444662 A CN 107444662A CN 201710871243 A CN201710871243 A CN 201710871243A CN 107444662 A CN107444662 A CN 107444662A
- Authority
- CN
- China
- Prior art keywords
- engine
- aircraft
- straight
- boarding
- plane
- 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.)
- Pending
Links
- 230000008450 motivation Effects 0.000 description 1
Classifications
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
A kind of three-dimensional aircraft, category Electromechanical Transportation field.Solve the problems, such as to take off without runway.There are first level aircraft engine (3) and the second horizontal aircraft engine in right side on aircraft（4）；There is the first straight engine of boarding a plane under aircraft tripe（2）With the second straight engine of boarding a plane（5）；Aircraft wing has straight engine（1）；Straight engine left and right each one；Each horizontal aircraft engine, each engine and each straight aircraft engine three right angle condition each other of directly boarding a plane.For communications and transportation.
Description
Technical field
A kind of three-dimensional aircraft, category Electromechanical Transportation field.
Background technology
At present, aircraft all must have runway, can just take off.
The content of the invention
Here a kind of three-dimensional aircraft is invented, runway can not had to, can be taken off yet.
The invention is such：There are first level aircraft engine (3) and the second horizontal aircraft engine in right side on aircraft
Machine（4）；There is the first straight engine of boarding a plane under aircraft tripe（2）With the second straight engine of boarding a plane（5）；Aircraft wing has directly
Enter engine（1）；Straight engine left and right each one；Each horizontal aircraft engine, each engine and each of directly boarding a plane
Straight aircraft engine three right angle condition each other.When a moving object simultaneously by three active forces when, and these three make
It is firmly mutually at a right angle, i.e., horizontal aircraft engine, it is straight board a plane engine and straight aircraft engine mutually at a right angle when, this fortune
The running orbit of animal is into movement in a curve.When these three active forces are at a right angle and have two active forces equal, the moving object
Running orbit is into screw.When these three active forces are at a right angle and three active forces are all equal, then the operation of the moving object
Track globulate motion.When there was only two engines on board the aircraft, such as only directly board a plane engine and straight aircraft engine
Machine, i.e., on a moving object simultaneously by two active forces when, the curved motion of running orbit of this moving object.When the two
When active force is equal, the running orbit of this moving object circumferentially moves.When aircraft goes up to the air, only start straight and straight upper hair
Motivation, after lift-off, just stop directly upper engine.When aircraft will translate, just start horizontal engine.
Due to using above-mentioned design so that aircraft can start straight engine of boarding a plane, thus, this aircraft need not
Runway.
Brief description of the drawings
Fig. 1 is three-dimensional aircraft full figure.
Embodiment
In Fig. 1, there are first level aircraft engine (3) and the second horizontal aircraft engine in right side on aircraft（4）；Fly
There is the first straight engine of boarding a plane under row device tripe（2）With the second straight engine of boarding a plane（5）；Aircraft wing has straight engine
（1）；Straight engine left and right each one；Each horizontal aircraft engine, each engine and each straight aircraft of directly boarding a plane
Engine three right angle condition each other.
Claims (1)
1. a kind of three-dimensional aircraft, it is characterized in that：Right side has first level aircraft engine (3) and the second level to fly on aircraft
Machine engine（4）；There is the first straight engine of boarding a plane under aircraft tripe（2）With the second straight engine of boarding a plane（5）；Aircraft machine
The wing has straight engine（1）；Straight engine left and right each one；Each horizontal aircraft engine, each engine of directly boarding a plane
With each straight aircraft engine three right angle condition each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710871243.6A CN107444662A (en) | 2017-09-25 | 2017-09-25 | Three-dimensional aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710871243.6A CN107444662A (en) | 2017-09-25 | 2017-09-25 | Three-dimensional aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107444662A true CN107444662A (en) | 2017-12-08 |
Family
ID=60498095
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710871243.6A Pending CN107444662A (en) | 2017-09-25 | 2017-09-25 | Three-dimensional aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107444662A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4482108A (en) * | 1982-09-29 | 1984-11-13 | The Boeing Company | Tilt wing short takeoff aircraft and method |
| CN1281409A (en) * | 1997-12-10 | 2001-01-24 | 佛朗哥·卡潘纳 | System to transform horizontal take-off and self-sustained horizontal flight airplane into self-sustained horizontal flight, vertical landing and take-off, hybrid integrated airplane |
| CN102730192A (en) * | 2011-04-14 | 2012-10-17 | 戴瑾 | Vertical take-off and landing aircraft |
| CN103832582A (en) * | 2012-11-28 | 2014-06-04 | 陈昌志 | Multifunctional helicopter |
| US20160101853A1 (en) * | 2014-10-10 | 2016-04-14 | David Wayne Toppenberg | Vertical take off and landing aircraft |
| CN106428548A (en) * | 2016-10-12 | 2017-02-22 | 曹萍 | Vertical take-off and landing unmanned aerial vehicle |
| CN106809395A (en) * | 2017-03-10 | 2017-06-09 | 佛山市神风航空科技有限公司 | The launching apparatus and method of a kind of fixed wing aircraft |
-
2017
- 2017-09-25 CN CN201710871243.6A patent/CN107444662A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4482108A (en) * | 1982-09-29 | 1984-11-13 | The Boeing Company | Tilt wing short takeoff aircraft and method |
| CN1281409A (en) * | 1997-12-10 | 2001-01-24 | 佛朗哥·卡潘纳 | System to transform horizontal take-off and self-sustained horizontal flight airplane into self-sustained horizontal flight, vertical landing and take-off, hybrid integrated airplane |
| CN102730192A (en) * | 2011-04-14 | 2012-10-17 | 戴瑾 | Vertical take-off and landing aircraft |
| CN103832582A (en) * | 2012-11-28 | 2014-06-04 | 陈昌志 | Multifunctional helicopter |
| US20160101853A1 (en) * | 2014-10-10 | 2016-04-14 | David Wayne Toppenberg | Vertical take off and landing aircraft |
| CN106428548A (en) * | 2016-10-12 | 2017-02-22 | 曹萍 | Vertical take-off and landing unmanned aerial vehicle |
| CN106809395A (en) * | 2017-03-10 | 2017-06-09 | 佛山市神风航空科技有限公司 | The launching apparatus and method of a kind of fixed wing aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20171208 |