ATE382014T1 - Fluggerät mit vorwärts ausfahrbarer vorderkante des rumpfes und der tragflügel - Google Patents
Fluggerät mit vorwärts ausfahrbarer vorderkante des rumpfes und der tragflügelInfo
- Publication number
- ATE382014T1 ATE382014T1 AT06075435T AT06075435T ATE382014T1 AT E382014 T1 ATE382014 T1 AT E382014T1 AT 06075435 T AT06075435 T AT 06075435T AT 06075435 T AT06075435 T AT 06075435T AT E382014 T1 ATE382014 T1 AT E382014T1
- Authority
- AT
- Austria
- Prior art keywords
- leading edge
- wings
- aircraft
- fuse
- forward extendable
- Prior art date
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)
- Toys (AREA)
- Tires In General (AREA)
- Fertilizing (AREA)
- Window Of Vehicle (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/066,341 US7216835B2 (en) | 2005-02-25 | 2005-02-25 | Aircraft with extendable leading edge of fuselage and wings |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE382014T1 true ATE382014T1 (de) | 2008-01-15 |
Family
ID=36190623
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT06075435T ATE382014T1 (de) | 2005-02-25 | 2006-02-24 | Fluggerät mit vorwärts ausfahrbarer vorderkante des rumpfes und der tragflügel |
Country Status (5)
Country | Link |
---|---|
US (1) | US7216835B2 (de) |
EP (1) | EP1695905B1 (de) |
AT (1) | ATE382014T1 (de) |
DE (1) | DE602006000356T2 (de) |
ES (1) | ES2299135T3 (de) |
Families Citing this family (6)
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 |
GB0708335D0 (en) * | 2007-04-30 | 2007-06-06 | Airbus Uk Ltd | Aerofoil |
EP3231702B1 (de) | 2016-04-11 | 2020-06-17 | Asco Industries NV | Hochauftriebsvorrichtung |
US10800511B2 (en) | 2018-05-31 | 2020-10-13 | The Boeing Company | End seal device for a high-lift device of an aircraft |
GB2582149A (en) * | 2019-03-12 | 2020-09-16 | Airbus Operations Ltd | Slat for an aircraft wing |
USD942321S1 (en) * | 2019-09-13 | 2022-02-01 | The Boeing Company | Unmanned aircraft |
Family Cites Families (53)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1215295A (en) * | 1916-03-14 | 1917-02-06 | Donald Mackay | Aeroplane. |
US1353666A (en) * | 1920-07-06 | 1920-09-21 | Handley Page Ltd | Wing and similar member of aircraft |
US1414200A (en) * | 1921-04-27 | 1922-04-25 | Handley Page Ltd | Wing and similar member of aircraft |
US1427012A (en) * | 1922-01-04 | 1922-08-22 | Handley Page Ltd | Wing and similar member of aircraft |
US1606117A (en) * | 1926-06-16 | 1926-11-09 | Joseph A Caples | Combination aeroplane |
US1730249A (en) * | 1926-10-04 | 1929-10-01 | Schmidt John | Airplane |
US1867013A (en) * | 1929-06-15 | 1932-07-12 | Herbert J Kratzer | Pilot vane for the aerofoil wings of airplanes |
US1818000A (en) * | 1930-03-19 | 1931-08-11 | Curtiss Aeroplane & Motor Co | Aerofoil operating mechanism |
US1891261A (en) * | 1931-10-05 | 1932-12-20 | Charles H Gunn | Safety wing for airplanes |
US1945254A (en) * | 1931-11-02 | 1934-01-30 | Charles C Bittner | Aeroplane |
US2500512A (en) * | 1947-03-08 | 1950-03-14 | Bell Aircraft Corp | Wing lift modification means |
US2793826A (en) * | 1956-03-23 | 1957-05-28 | Willy A Fiedler | Split aircraft wing |
US3170657A (en) * | 1960-05-02 | 1965-02-23 | John M Riebe | Landing arrangement for aerial vehicle |
US3153523A (en) * | 1963-05-27 | 1964-10-20 | Iii Jefferson S Lowman | Variable lift aircraft wing pivotally mounted for movement about a skewed longitudinal axis |
FR94080E (fr) * | 1963-12-27 | 1969-06-27 | Breguet Aviat | Avion a configuration variable. |
US3447761A (en) * | 1967-06-12 | 1969-06-03 | Boeing Co | Supersonic airplane variable-sweep integrated airfoil system |
US3425650A (en) * | 1967-10-02 | 1969-02-04 | Joseph Silva | Air deflector for supersonic aircraft |
US3486720A (en) * | 1967-12-07 | 1969-12-30 | Boeing Co | Continuous slot forming leading edge slats for cranked wings |
US3630471A (en) * | 1969-03-07 | 1971-12-28 | Occidental Aircraft Corp | Nose slat fuselage lifting body |
DE1917532C3 (de) * | 1969-04-05 | 1974-05-30 | Dornier Gmbh, 7990 Friedrichshafen | Spaltklappenanordnung an Tragflügeln für Luftfahrzeuge |
US3847369A (en) * | 1973-03-08 | 1974-11-12 | Us Navy | Control surface deployment mechanism |
US4008867A (en) * | 1974-08-16 | 1977-02-22 | Kaniut Herbert M | Aircraft with safety tail unit |
DE2656692C2 (de) * | 1976-12-15 | 1982-07-29 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Entenflugzeug |
GB2003807A (en) | 1977-08-23 | 1979-03-21 | British Aircraft Corp Ltd | Aircraft |
DE2751361C2 (de) * | 1977-11-17 | 1984-09-27 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verfahren zur Flugzeugsteuerung durch Steuerung abgelöster Flügelvorderkanten-Wirbelströme |
FR2492337A1 (fr) * | 1980-10-16 | 1982-04-23 | Aerospatiale | Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile |
DE3122137A1 (de) | 1981-06-04 | 1982-12-23 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Vorderkantenklappensystem fuer flugzeugfluegel |
US4494713A (en) * | 1982-06-24 | 1985-01-22 | Kyusik Kim | Shockcone and channeled disk-airframe |
US4729528A (en) * | 1983-02-28 | 1988-03-08 | Northrop Corporation | Aeroelastic control flap |
US4585192A (en) * | 1983-03-30 | 1986-04-29 | British Aerospace Public Limited Company | Leading edge arrangements for aircraft wings |
US4667898A (en) * | 1985-08-02 | 1987-05-26 | The United States Of America As Represented By The Secretary Of The Navy | Aircraft with single surface membranous airfoils |
USD314366S (en) * | 1989-04-19 | 1991-02-05 | Northrop Corporation | Aircraft |
US5056741A (en) * | 1989-09-29 | 1991-10-15 | The Boeing Company | Apparatus and method for aircraft wing stall control |
US5062595A (en) * | 1990-04-26 | 1991-11-05 | University Of Southern California | Delta wing with lift enhancing flap |
US5897076A (en) * | 1991-07-08 | 1999-04-27 | Tracy; Richard R. | High-efficiency, supersonic aircraft |
US5158252A (en) | 1991-10-24 | 1992-10-27 | The Boeing Company | Three-position variable camber Krueger leading edge flap |
US5312070A (en) * | 1992-04-02 | 1994-05-17 | Grumman Aerospace Corporation | Segmented variable sweep wing aircraft |
US5681013A (en) | 1995-12-26 | 1997-10-28 | The Boeing Company | Vortex leading edge flap assembly for supersonic airplanes |
US5927656A (en) | 1996-06-26 | 1999-07-27 | The Boeing Company | Wing leading edge flap and method therefor |
US5921506A (en) * | 1997-09-25 | 1999-07-13 | Northrop Grumman Corporation | Extendible leading edge flap |
US6073889A (en) * | 1997-10-16 | 2000-06-13 | The Boeing Company | Wing flap seal bump |
US6220551B1 (en) * | 1998-01-14 | 2001-04-24 | Manuel Munoz Saiz | Flight controls with automatic balance |
US6068219A (en) * | 1998-04-13 | 2000-05-30 | Northrop Grumman Corporation | Single surface multi axis aircraft control |
DE69916360T3 (de) * | 1998-05-21 | 2008-06-05 | Mcdonnell Douglas Corp. | Flügelprofil |
GB9816936D0 (en) * | 1998-08-05 | 1998-09-30 | British Aerospace | An aerofoil having a slat |
US6129308A (en) * | 1998-09-21 | 2000-10-10 | Northrop Grumman Corporation | Delta-shaped aircraft with variable camber fuselage and wing |
US6328265B1 (en) * | 1999-05-25 | 2001-12-11 | Faruk Dizdarevic | Slot forming segments and slot changing spoilers |
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 |
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 |
-
2005
- 2005-02-25 US US11/066,341 patent/US7216835B2/en not_active Expired - Fee Related
-
2006
- 2006-02-24 AT AT06075435T patent/ATE382014T1/de not_active IP Right Cessation
- 2006-02-24 DE DE602006000356T patent/DE602006000356T2/de active Active
- 2006-02-24 ES ES06075435T patent/ES2299135T3/es active Active
- 2006-02-24 EP EP06075435A patent/EP1695905B1/de not_active Not-in-force
Also Published As
Publication number | Publication date |
---|---|
DE602006000356D1 (de) | 2008-02-07 |
US7216835B2 (en) | 2007-05-15 |
EP1695905A1 (de) | 2006-08-30 |
ES2299135T3 (es) | 2008-05-16 |
EP1695905B1 (de) | 2007-12-26 |
DE602006000356T2 (de) | 2008-12-11 |
US20070069084A1 (en) | 2007-03-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |