CN107554754A - A kind of aircraft lift(Or thrust)Device - Google Patents
A kind of aircraft lift(Or thrust)Device Download PDFInfo
- Publication number
- CN107554754A CN107554754A CN201710798399.6A CN201710798399A CN107554754A CN 107554754 A CN107554754 A CN 107554754A CN 201710798399 A CN201710798399 A CN 201710798399A CN 107554754 A CN107554754 A CN 107554754A
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- CN
- China
- Prior art keywords
- ware
- bucket
- thrust
- lift
- inner bottom
- 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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Abstract
The present invention relates to a kind of aircraft lift (or thrust) device, particularly small size, larger lift unit;This device is tubbiness, shallow tubbiness or ware shape, built-in flabellum, and lift (or thrust) is produced by rotating, and its is compact-sized, is different from the lift unit of existing aircraft, makes it possible following transatmospheric vehicle miniaturization popularization.
Description
Technical field:
The present invention relates to a kind of aircraft lift (or thrust) device, particularly small size, larger lift unit, contribute to
The miniaturization of aircraft.
Background technology:
With the continuous development of society, the land transportation that can't bear the heavy load can not increasingly meet the trip requirements of the mankind;
Currently, or numerous aircraft use level wings, or using external propeller, there is many particular/special requirements to use condition,
The shortcomings that unconquerable be present, be not suitable with the change of tomorrow requirement.In order to greatly develop air traffic, there is an urgent need to a kind of external form
It is compact, relatively low transatmospheric vehicle is required to environmental condition.
The content of the invention:
In order to realize above target, its difficult point is the miniaturization of lift unit.The present invention just overcomes above difficulty very well,
This device has a tubbiness, shallow tubbiness or ware shape shell 1, and outer casing bottom is closed, and top is into openning shape;On bucket (ware) inner bottom surface around
Central axis is uniformly arranged several pieces air draft flabellums 2, the lower edge of flabellum 2 be close to inner bottom surface be connected as a single entity with inner bottom surface or from
Inner bottom surface, side edge is close to bucket (ware) inwall or is connected as a single entity with bucket (ware) inwall, along consistent in the height and bucket of blade.
Brief description of the drawings:
Fig. 1 general views
Fig. 2 front views
Fig. 3 A-A sectional views
1 in Fig. 1:Shell;2:Flabellum
Shell plays a part of to protect and supports flabellum and connect drive device outside, and the effect of flabellum is excluded in bucket (ware)
Gas, both, which are incorporated in, completes the function of producing lift (or thrust) under the driving of external driver device.
Embodiment:
When device ceaselessly rotates around direction of the central shaft along the air draft of flabellum 2, the gas in bucket (ware) is in flabellum 2
Ceaselessly it is discharged under effect, makes the gradual step-down of air pressure inside, external pressure is that atmospheric pressure keeps constant, inside and outside so as to produce
Bottom surface pressure difference, just generated on bucket (ware) bottom plate it is upward lift power, this lifts power and rotating speed, flabellum, base areas size
Relevant etc. factor, if the selection of each parameter is proper, lift power just can produce lift-off more than gravity.
Claims (2)
- A kind of 1. aircraft lift (or thrust) device, it is characterised in that:Including tubbiness, shallow tubbiness or ware shape shell and built-in row Fan leaf;Wherein, the outer casing bottom is closed, open top;The air draft flabellum, around central axis on bucket (ware) inner bottom surface Uniformly arrangement, lower edge are close to inner bottom surface or are connected as a single entity with inner bottom surface or from inner bottom surface, side along be close to bucket (ware) inwall or Be connected as a single entity with bucket (ware) inwall, highly with bucket (ware) along consistent, variable amounts.
- The method of work of lift described in claim 1 2. (or thrust) device is as follows:Rotated around central shaft along flabellum discharge directions, produce the inside and outside bottom surface pressure difference of housing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710798399.6A CN107554754A (en) | 2017-09-06 | 2017-09-06 | A kind of aircraft lift(Or thrust)Device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710798399.6A CN107554754A (en) | 2017-09-06 | 2017-09-06 | A kind of aircraft lift(Or thrust)Device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN107554754A true CN107554754A (en) | 2018-01-09 |
Family
ID=60978215
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710798399.6A Pending CN107554754A (en) | 2017-09-06 | 2017-09-06 | A kind of aircraft lift(Or thrust)Device |
Country Status (1)
Country | Link |
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CN (1) | CN107554754A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111001542A (en) * | 2019-12-05 | 2020-04-14 | 深圳供电局有限公司 | Overhead conductor spraying robot |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2382652Y (en) * | 1999-07-24 | 2000-06-14 | 史绵武 | Composite rotary wing of aeroplane |
US6595753B1 (en) * | 1999-05-21 | 2003-07-22 | A. Vortex Holding Company | Vortex attractor |
CN1521085A (en) * | 2003-02-10 | 2004-08-18 | 卢桢干 | General lift propulsion system |
CN2646045Y (en) * | 2003-10-24 | 2004-10-06 | 尚光辉 | Culvert fan type screw propeller |
CN101046208A (en) * | 2006-03-29 | 2007-10-03 | 日本伺服株式会社 | Multiple fans of cascade connection |
CN102020015A (en) * | 2010-11-09 | 2011-04-20 | 任永斌 | Centrifugal lift device |
CN102774495A (en) * | 2012-07-15 | 2012-11-14 | 张雄伟 | Elevating-force thruster |
CN204488375U (en) * | 2014-11-24 | 2015-07-22 | 中国计量学院 | Wheel type screw propeller |
CN104973235A (en) * | 2014-04-04 | 2015-10-14 | 李维农 | Novel sailing propeller utilizing Bernoulli principle |
CN106542096A (en) * | 2015-09-18 | 2017-03-29 | 楚亮 | Aircraft |
-
2017
- 2017-09-06 CN CN201710798399.6A patent/CN107554754A/en active Pending
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6595753B1 (en) * | 1999-05-21 | 2003-07-22 | A. Vortex Holding Company | Vortex attractor |
CN2382652Y (en) * | 1999-07-24 | 2000-06-14 | 史绵武 | Composite rotary wing of aeroplane |
CN1521085A (en) * | 2003-02-10 | 2004-08-18 | 卢桢干 | General lift propulsion system |
CN2646045Y (en) * | 2003-10-24 | 2004-10-06 | 尚光辉 | Culvert fan type screw propeller |
CN101046208A (en) * | 2006-03-29 | 2007-10-03 | 日本伺服株式会社 | Multiple fans of cascade connection |
CN102020015A (en) * | 2010-11-09 | 2011-04-20 | 任永斌 | Centrifugal lift device |
CN102774495A (en) * | 2012-07-15 | 2012-11-14 | 张雄伟 | Elevating-force thruster |
CN104973235A (en) * | 2014-04-04 | 2015-10-14 | 李维农 | Novel sailing propeller utilizing Bernoulli principle |
CN204488375U (en) * | 2014-11-24 | 2015-07-22 | 中国计量学院 | Wheel type screw propeller |
CN106542096A (en) * | 2015-09-18 | 2017-03-29 | 楚亮 | Aircraft |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111001542A (en) * | 2019-12-05 | 2020-04-14 | 深圳供电局有限公司 | Overhead conductor spraying robot |
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