JPH01132499U - - Google Patents

Info

Publication number
JPH01132499U
JPH01132499U JP2923288U JP2923288U JPH01132499U JP H01132499 U JPH01132499 U JP H01132499U JP 2923288 U JP2923288 U JP 2923288U JP 2923288 U JP2923288 U JP 2923288U JP H01132499 U JPH01132499 U JP H01132499U
Authority
JP
Japan
Prior art keywords
wing
suction port
blade
jet flow
flow outlet
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
JP2923288U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP2923288U priority Critical patent/JPH01132499U/ja
Publication of JPH01132499U publication Critical patent/JPH01132499U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Jet Pumps And Other Pumps (AREA)

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本考案の第1実施例の断面図、第2図
は本考案の第2実施例の断面図、第3図は本考案
の実施例と従来例との迎え角に対する揚力係数の
比較曲線図、第4図、第5図は各々従来例の断面
図である。 1……翼、2,2a,2b……吹出口、3……
吸込み口、4……送付装置、5……仕切り、6a
,6b……開閉軸、7a,7b……蓋。
Fig. 1 is a cross-sectional view of the first embodiment of the present invention, Fig. 2 is a cross-sectional view of the second embodiment of the present invention, and Fig. 3 is a graph showing the lift coefficient with respect to the angle of attack of the embodiment of the present invention and the conventional example. The comparative curve diagrams, FIGS. 4 and 5, are sectional views of conventional examples. 1...Blade, 2, 2a, 2b...Blowout port, 3...
Suction port, 4... sending device, 5... partition, 6a
, 6b...opening/closing shaft, 7a, 7b...lid.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] その断面が翼型、円筒、楕円体、卵型等をなし
流れの中に設置されて揚力を発生する翼体におい
て、揚力を発生する翼面の適当な個所に翼面に沿
つて設けられたジエツト流の吹出口と、同吹出口
の下流に翼面に沿つて設けられた流体の吸込み口
と、同吸込み口側を流体取入れ側とし上記吹出口
側を吐出側として翼内に設置された吐出装置とを
具備してなることを特徴とする高揚力発生翼。
In a wing body whose cross section is an airfoil, cylinder, ellipsoid, oval, etc., and which is installed in a flow and generates lift, it is installed along the wing surface at an appropriate location on the wing surface that generates lift. A jet flow outlet, a fluid suction port provided along the blade surface downstream of the jet flow outlet, and a fluid suction port installed in the blade with the suction port side as the fluid intake side and the above blowout port side as the discharge side. A high-lift force generating wing comprising a discharge device.
JP2923288U 1988-03-07 1988-03-07 Pending JPH01132499U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2923288U JPH01132499U (en) 1988-03-07 1988-03-07

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2923288U JPH01132499U (en) 1988-03-07 1988-03-07

Publications (1)

Publication Number Publication Date
JPH01132499U true JPH01132499U (en) 1989-09-08

Family

ID=31253266

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2923288U Pending JPH01132499U (en) 1988-03-07 1988-03-07

Country Status (1)

Country Link
JP (1) JPH01132499U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009504511A (en) * 2005-08-09 2009-02-05 ザ・ボーイング・カンパニー Lift augmentation system and related methods
JP2009504481A (en) * 2005-08-09 2009-02-05 ザ・ボーイング・カンパニー System and associated method for aerodynamic flow
JP2010505063A (en) * 2006-09-29 2010-02-18 エアバス フランス Aircraft jet engine nacelle and aircraft equipped with the nacelle
JP2020032938A (en) * 2018-08-31 2020-03-05 幸福の科学 Flight body

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009504511A (en) * 2005-08-09 2009-02-05 ザ・ボーイング・カンパニー Lift augmentation system and related methods
JP2009504481A (en) * 2005-08-09 2009-02-05 ザ・ボーイング・カンパニー System and associated method for aerodynamic flow
JP2010505063A (en) * 2006-09-29 2010-02-18 エアバス フランス Aircraft jet engine nacelle and aircraft equipped with the nacelle
JP2020032938A (en) * 2018-08-31 2020-03-05 幸福の科学 Flight body

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