CN107554754A - A kind of aircraft lift(Or thrust)Device - Google Patents

A kind of aircraft lift(Or thrust)Device Download PDF

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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
Authority
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.)
Pending
Application number
CN201710798399.6A
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Chinese (zh)
Inventor
不公告发明人
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Deng Andi
Original Assignee
Deng Andi
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Deng Andi filed Critical Deng Andi
Priority to CN201710798399.6A priority Critical patent/CN107554754A/en
Publication of CN107554754A publication Critical patent/CN107554754A/en
Pending legal-status Critical Current

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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

A kind of aircraft lift (or thrust) device
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)

  1. 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.
  2. 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.
CN201710798399.6A 2017-09-06 2017-09-06 A kind of aircraft lift(Or thrust)Device Pending CN107554754A (en)

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
CN (1) CN107554754A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (10)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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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