AU2003289606A1 - A Wing ASSEMBLY CAPABLE OF INCREASIGN THE LIFT AND THE ANGLE OF STALL - Google Patents

A Wing ASSEMBLY CAPABLE OF INCREASIGN THE LIFT AND THE ANGLE OF STALL

Info

Publication number
AU2003289606A1
AU2003289606A1 AU2003289606A AU2003289606A AU2003289606A1 AU 2003289606 A1 AU2003289606 A1 AU 2003289606A1 AU 2003289606 A AU2003289606 A AU 2003289606A AU 2003289606 A AU2003289606 A AU 2003289606A AU 2003289606 A1 AU2003289606 A1 AU 2003289606A1
Authority
AU
Australia
Prior art keywords
increasign
stall
lift
angle
assembly capable
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.)
Abandoned
Application number
AU2003289606A
Inventor
Shangxiang Zhu
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of AU2003289606A1 publication Critical patent/AU2003289606A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/54—Varying in area

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AU2003289606A 2003-01-17 2003-12-04 A Wing ASSEMBLY CAPABLE OF INCREASIGN THE LIFT AND THE ANGLE OF STALL Abandoned AU2003289606A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CN02133862.0 2003-01-17
CNB021338620A CN100513256C (en) 2003-01-17 2003-01-17 Sail wing for increasing lift force and stalling attack angle
PCT/CN2003/001035 WO2004092009A1 (en) 2003-01-17 2003-12-04 A Wing ASSEMBLY CAPABLE OF INCREASIGN THE LIFT AND THE ANGLE OF STALL

Publications (1)

Publication Number Publication Date
AU2003289606A1 true AU2003289606A1 (en) 2004-11-04

Family

ID=34231318

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003289606A Abandoned AU2003289606A1 (en) 2003-01-17 2003-12-04 A Wing ASSEMBLY CAPABLE OF INCREASIGN THE LIFT AND THE ANGLE OF STALL

Country Status (3)

Country Link
CN (1) CN100513256C (en)
AU (1) AU2003289606A1 (en)
WO (1) WO2004092009A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009006212A1 (en) * 2009-01-27 2010-09-23 Fritz Unger Method for increasing lifting of e.g. aerofoil, for use in aerodynamically-flying aircraft, involves arranging body above another body in aerodynamic-flow, and moving aerofoil upwardly by parts during application of air flow
US8882470B2 (en) 2011-01-07 2014-11-11 Fritz Unger Rotor for a wind power generator
US9016637B2 (en) * 2012-02-10 2015-04-28 The Boeing Company High-positioned 3-position variable camber krueger
CN113968341B (en) * 2021-12-08 2024-01-26 北京航空航天大学 Miniature unmanned aerial vehicle using bionic winglet
CN114506442B (en) * 2022-01-28 2024-07-05 中国商用飞机有限责任公司 Wing with turbulence auxiliary device and flight device comprising wing

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2237254A (en) * 1989-10-25 1991-05-01 Richard Harry Barnard Secondary lifting surfaces using separated flow
CN2095830U (en) * 1991-04-22 1992-02-12 林永克 Air propeller
DE4140139A1 (en) * 1991-12-05 1993-06-09 Klaus Dipl.-Werkmeister 6600 Saarbruecken De Lellig Aircraft which can be converted from biplane to monoplane - has short take-off and landing capability but high cruising speed
CN2186706Y (en) * 1994-01-24 1995-01-04 南京理工大学 High lift eddy catching wing
US5772155A (en) * 1996-06-01 1998-06-30 Nowak; Dieter K. Aircraft wing flaps

Also Published As

Publication number Publication date
CN1517269A (en) 2004-08-04
WO2004092009A1 (en) 2004-10-28
CN100513256C (en) 2009-07-15

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase