DE69813296D1 - Geteiltes querruder für ein starrflügelflugzeug - Google Patents

Geteiltes querruder für ein starrflügelflugzeug

Info

Publication number
DE69813296D1
DE69813296D1 DE69813296T DE69813296T DE69813296D1 DE 69813296 D1 DE69813296 D1 DE 69813296D1 DE 69813296 T DE69813296 T DE 69813296T DE 69813296 T DE69813296 T DE 69813296T DE 69813296 D1 DE69813296 D1 DE 69813296D1
Authority
DE
Germany
Prior art keywords
wing aircraft
fixed wing
split aileron
aileron
split
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.)
Expired - Lifetime
Application number
DE69813296T
Other languages
English (en)
Other versions
DE69813296T2 (de
Inventor
Lawrence Y Lam
Michael Lam
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 DE69813296D1 publication Critical patent/DE69813296D1/de
Application granted granted Critical
Publication of DE69813296T2 publication Critical patent/DE69813296T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/06—Adjustable control surfaces or members, e.g. rudders with two or more independent movements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
DE69813296T 1997-12-18 1998-12-03 Geteiltes querruder für ein starrflügelflugzeug Expired - Lifetime DE69813296T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US993241 1997-12-18
US08/993,241 US6079672A (en) 1997-12-18 1997-12-18 Aileron for fixed wing aircraft
PCT/US1998/025199 WO1999030967A1 (en) 1997-12-18 1998-12-03 Improved aileron for fixed wing aircraft

Publications (2)

Publication Number Publication Date
DE69813296D1 true DE69813296D1 (de) 2003-05-15
DE69813296T2 DE69813296T2 (de) 2004-01-22

Family

ID=25539287

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69813296T Expired - Lifetime DE69813296T2 (de) 1997-12-18 1998-12-03 Geteiltes querruder für ein starrflügelflugzeug

Country Status (8)

Country Link
US (2) US6079672A (de)
EP (1) EP1042165B1 (de)
AU (1) AU1799399A (de)
BR (1) BR9813661A (de)
CA (1) CA2315167C (de)
DE (1) DE69813296T2 (de)
IL (1) IL136779A (de)
WO (1) WO1999030967A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109835464A (zh) * 2017-11-28 2019-06-04 波音公司 具有气动复原门的飞行器机翼襟翼

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US8939394B1 (en) * 2010-09-09 2015-01-27 Groen Brothers Aviation, Inc. Anemometer drive apparatus and method
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FR2968634B1 (fr) * 2010-12-08 2013-08-02 Snecma Pylone de fixation d'un moteur d'aeronef a helices propulsives non carenees
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CN103231795A (zh) * 2013-04-12 2013-08-07 成都飞机设计研究所 一种公务机的发动机上置及前掠翼鸭式布局
US9846432B2 (en) * 2013-07-25 2017-12-19 Lam Aviation, Inc. Aircraft wing structure and control system
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CN105966600B (zh) * 2016-05-16 2018-04-17 北京航空航天大学 一种可连续变形阻力方向舵
FR3053956B1 (fr) * 2016-07-18 2019-06-28 Airbus Operations Gouverne crocodile pour aeronef
US10479481B2 (en) * 2016-09-28 2019-11-19 The Boeing Company Process and machine for reducing a drag component of a horizontal stabilizer on an aircraft
US10545511B2 (en) 2016-09-28 2020-01-28 The Boeing Company Process and machine for increasing a pitch authority of an aircraft
US11352123B2 (en) * 2018-06-28 2022-06-07 Lucas Kai-Luen Hung Wing assembly for a high endurance aircraft
EP3670330B1 (de) 2018-12-20 2022-02-09 Bombardier Inc. Flugzeugklappenausfahrsystem
CN111348180A (zh) * 2018-12-20 2020-06-30 庞巴迪公司 用于控制飞行器飞行控制面的系统和方法
US12049299B2 (en) * 2019-03-11 2024-07-30 Lam Aviation, Inc. Airfoil system
CN110654190A (zh) * 2019-10-31 2020-01-07 南京航空航天大学 一种倾转无轴涵道旋翼飞行汽车及其工作方法
US11548616B1 (en) 2020-03-02 2023-01-10 Lucas Kai-Luen Hung Split-flap wing assembly for a high endurance aircraft
CN112498661B (zh) * 2020-12-04 2024-01-30 中国航空工业集团公司沈阳飞机设计研究所 一种多功能舵面结构
CN114313218A (zh) * 2021-12-21 2022-04-12 中国科学院工程热物理研究所 阻力方向舵的传动机构及飞行器

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109835464A (zh) * 2017-11-28 2019-06-04 波音公司 具有气动复原门的飞行器机翼襟翼

Also Published As

Publication number Publication date
EP1042165B1 (de) 2003-04-09
WO1999030967A1 (en) 1999-06-24
CA2315167A1 (en) 1999-06-24
AU1799399A (en) 1999-07-05
US6079672A (en) 2000-06-27
EP1042165A1 (de) 2000-10-11
DE69813296T2 (de) 2004-01-22
IL136779A0 (en) 2001-06-14
US6554229B1 (en) 2003-04-29
IL136779A (en) 2003-09-17
CA2315167C (en) 2007-04-10
BR9813661A (pt) 2002-02-13

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Legal Events

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8364 No opposition during term of opposition