CN103640695A - Novel vertical lift fixed wing aircraft - Google Patents
Novel vertical lift fixed wing aircraft Download PDFInfo
- Publication number
- CN103640695A CN103640695A CN201310636105.1A CN201310636105A CN103640695A CN 103640695 A CN103640695 A CN 103640695A CN 201310636105 A CN201310636105 A CN 201310636105A CN 103640695 A CN103640695 A CN 103640695A
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- China
- Prior art keywords
- fixed wing
- engine
- wing aircraft
- vertical lift
- horizontal direction
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Abstract
The invention relates to a novel vertical lift fixed wing aircraft. The novel vertical lift fixed wing aircraft comprises an airframe, a fixed wing and a horizontal direction propelling engine, and is characterized in that a cantilever is crossed and fixed on a wing parallel to the propelling airflow of the horizontal direction propelling engine, and each of two ends of the cantilever is respectively provided with a vertical downward propelling engine.
Description
technical field:
The present invention relates to a kind of aircraft, specifically a kind of new vertical lifting fixed wing aircraft.
background technology:
Existing vertical lift fixed wing aircraft, by hydraulic efficiency pressure system adjust screw propeller towards controlling aircraft vertical lift or horizontal flight, due to awing adjust screw propeller towards time aircraft less stable, so frequently cause the accident and personal casualty.
summary of the invention:
The technical problem to be solved in the present invention is to provide a kind of new vertical lifting fixed wing aircraft.
In order to solve the problems of the technologies described above, new vertical lifting fixed wing aircraft of the present invention comprises airframe, fixed-wing, horizontal direction advances engine, it is characterized in that, on the wing of the propulsive gas stream parallel orientation with horizontal direction propelling engine, intersect and fix a cantilever, the two ends of cantilever respectively arrange one and advance vertically downward engine.
When needing vertical lift, advance vertically downward engine work, horizontal direction advances engine to stop, and makes aircraft produce lifting drive, opens horizontal direction advance engine when flight when certain altitude needs horizontal flight, progressively closes and advances vertically downward engine.
The invention has the beneficial effects as follows: horizontal flight, vertical lift overlaps independently engine by two to be controlled, and the stability of system is higher.
Accompanying drawing explanation
Fig. 1 is the structural representation of new vertical lifting fixed wing aircraft of the present invention.
The specific embodiment
Below in conjunction with the drawings and specific embodiments, new vertical lifting fixed wing aircraft of the present invention is described in further detail.
As shown in the figure, new vertical lifting fixed wing aircraft of the present invention comprises airframe 1, fixed-wing 2, horizontal direction advances engine 3, it is characterized in that, on the wing of the propulsive gas stream parallel orientation with horizontal direction propelling engine 3, intersect and fix a cantilever 4, the two ends of cantilever 4 respectively arrange one and advance vertically downward engine 5.
Claims (1)
1. a new vertical lifting fixed wing aircraft comprises airframe (1), fixed-wing (2), horizontal direction advances engine (3), it is characterized in that, on the wing of the propulsive gas stream parallel orientation with horizontal direction propelling engine (3), intersect and fix a cantilever (4), the two ends of cantilever (4) respectively arrange one and advance vertically downward engine (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310636105.1A CN103640695A (en) | 2013-12-03 | 2013-12-03 | Novel vertical lift fixed wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310636105.1A CN103640695A (en) | 2013-12-03 | 2013-12-03 | Novel vertical lift fixed wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103640695A true CN103640695A (en) | 2014-03-19 |
Family
ID=50246035
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310636105.1A Pending CN103640695A (en) | 2013-12-03 | 2013-12-03 | Novel vertical lift fixed wing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103640695A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081098A (en) * | 2016-08-24 | 2016-11-09 | 广州朱雀航空科技有限公司 | A kind of unmanned plane |
| CN106240812A (en) * | 2016-08-30 | 2016-12-21 | 广州三飞航空科技有限公司 | One lifts unmanned plane easily |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6843447B2 (en) * | 2003-01-06 | 2005-01-18 | Brian H. Morgan | Vertical take-off and landing aircraft |
| RU2448869C1 (en) * | 2010-12-03 | 2012-04-27 | Дмитрий Сергеевич Дуров | Multipurpose multi-tiltrotor helicopter-aircraft |
| EP2570345A1 (en) * | 2011-09-16 | 2013-03-20 | EMT Ingenieurgesellschaft Dipl.-Ing. Hartmut Euer mbH | Airplane |
| CN103079955A (en) * | 2010-07-19 | 2013-05-01 | 吉·埃罗公司 | Personal aircraft |
| SK1462011A3 (en) * | 2011-12-28 | 2013-08-02 | Alexander Kalisky | Auxiliary multicopter |
-
2013
- 2013-12-03 CN CN201310636105.1A patent/CN103640695A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6843447B2 (en) * | 2003-01-06 | 2005-01-18 | Brian H. Morgan | Vertical take-off and landing aircraft |
| CN103079955A (en) * | 2010-07-19 | 2013-05-01 | 吉·埃罗公司 | Personal aircraft |
| RU2448869C1 (en) * | 2010-12-03 | 2012-04-27 | Дмитрий Сергеевич Дуров | Multipurpose multi-tiltrotor helicopter-aircraft |
| EP2570345A1 (en) * | 2011-09-16 | 2013-03-20 | EMT Ingenieurgesellschaft Dipl.-Ing. Hartmut Euer mbH | Airplane |
| SK1462011A3 (en) * | 2011-12-28 | 2013-08-02 | Alexander Kalisky | Auxiliary multicopter |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081098A (en) * | 2016-08-24 | 2016-11-09 | 广州朱雀航空科技有限公司 | A kind of unmanned plane |
| CN106240812A (en) * | 2016-08-30 | 2016-12-21 | 广州三飞航空科技有限公司 | One lifts unmanned plane easily |
| CN106240812B (en) * | 2016-08-30 | 2018-08-03 | 广州三飞航空科技有限公司 | It is a kind of to lift easily unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140319 |