DE602006000224D1 - Fluggerät mit drehbarer Vorderkante des Rumpfes und der Tragflügel - Google Patents

Fluggerät mit drehbarer Vorderkante des Rumpfes und der Tragflügel

Info

Publication number
DE602006000224D1
DE602006000224D1 DE602006000224T DE602006000224T DE602006000224D1 DE 602006000224 D1 DE602006000224 D1 DE 602006000224D1 DE 602006000224 T DE602006000224 T DE 602006000224T DE 602006000224 T DE602006000224 T DE 602006000224T DE 602006000224 D1 DE602006000224 D1 DE 602006000224D1
Authority
DE
Germany
Prior art keywords
leading edge
fuselage
wings
aircraft
rotatable leading
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.)
Active
Application number
DE602006000224T
Other languages
English (en)
Other versions
DE602006000224T2 (de
Inventor
Allen A Arata
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.)
Northrop Grumman Corp
Original Assignee
Northrop Grumman Corp
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 Northrop Grumman Corp filed Critical Northrop Grumman Corp
Publication of DE602006000224D1 publication Critical patent/DE602006000224D1/de
Application granted granted Critical
Publication of DE602006000224T2 publication Critical patent/DE602006000224T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
DE602006000224T 2005-02-25 2006-02-24 Fluggerät mit drehbarer Vorderkante des Rumpfes und der Tragflügel Active DE602006000224T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/066,354 US7246770B2 (en) 2005-02-25 2005-02-25 Aircraft with rotatable leading edge of fuselage and wings
US66354 2005-02-25

Publications (2)

Publication Number Publication Date
DE602006000224D1 true DE602006000224D1 (de) 2007-12-27
DE602006000224T2 DE602006000224T2 (de) 2008-09-18

Family

ID=36179036

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006000224T Active DE602006000224T2 (de) 2005-02-25 2006-02-24 Fluggerät mit drehbarer Vorderkante des Rumpfes und der Tragflügel

Country Status (5)

Country Link
US (1) US7246770B2 (de)
EP (1) EP1695903B1 (de)
AT (1) ATE378250T1 (de)
DE (1) DE602006000224T2 (de)
ES (1) ES2297796T3 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7204454B2 (en) * 2005-02-25 2007-04-17 Northrop Grumman Corporation Aircraft with articulated leading edge of fuselage and wings
US20120141278A1 (en) * 2011-09-06 2012-06-07 General Electric Company Rotor blade assembly and method for modifying load characteristic of rotor blade in wind turbine
EP3231702B1 (de) 2016-04-11 2020-06-17 Asco Industries NV Hochauftriebsvorrichtung
CN115571323A (zh) * 2022-12-08 2023-01-06 中国空气动力研究与发展中心计算空气动力研究所 一种亚声速扁平融合体布局飞行器
CN116985994B (zh) * 2023-09-21 2023-11-28 中国空气动力研究与发展中心计算空气动力研究所 一种隐形飞行器

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US6179248B1 (en) * 1999-11-04 2001-01-30 Aereon Corporation Aircraft
US6475933B1 (en) 2000-01-27 2002-11-05 Northrop Grumman Corporation Highly conductive elastomeric sheet
US6343768B1 (en) * 2000-05-16 2002-02-05 Patrick John Muldoon Vertical/short take-off and landing aircraft
US6659394B1 (en) * 2000-05-31 2003-12-09 The United States Of America As Represented By The Secretary Of The Air Force Compound tilting wing for high lift stability and control of aircraft
US6375126B1 (en) 2000-11-16 2002-04-23 The Boeing Company Variable camber leading edge for an airfoil
GB0114634D0 (en) 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
US6634594B1 (en) * 2002-05-03 2003-10-21 The Boeing Company Hypersonic waverider variable leading edge flaps
CA2444869A1 (en) * 2002-10-21 2004-04-21 The Boeing Company Method and apparatus for actuating movable components, including canards, over multiple ranges

Also Published As

Publication number Publication date
EP1695903B1 (de) 2007-11-14
EP1695903A1 (de) 2006-08-30
US7246770B2 (en) 2007-07-24
ES2297796T3 (es) 2008-05-01
ATE378250T1 (de) 2007-11-15
US20070102586A1 (en) 2007-05-10
DE602006000224T2 (de) 2008-09-18

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