DE3675372D1 - Vorfluegelenteisungseinrichtung fuer eine tragflaeche. - Google Patents
Vorfluegelenteisungseinrichtung fuer eine tragflaeche.Info
- Publication number
- DE3675372D1 DE3675372D1 DE8686201474T DE3675372T DE3675372D1 DE 3675372 D1 DE3675372 D1 DE 3675372D1 DE 8686201474 T DE8686201474 T DE 8686201474T DE 3675372 T DE3675372 T DE 3675372T DE 3675372 D1 DE3675372 D1 DE 3675372D1
- Authority
- DE
- Germany
- Prior art keywords
- wing
- slider
- defrosting device
- defrosting
- slider defrosting
- 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 - Fee Related
Links
- 238000010257 thawing Methods 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/04—Hot gas application
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Train Traffic Observation, Control, And Security (AREA)
- Tires In General (AREA)
- Connection Of Plates (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/814,603 US4752049A (en) | 1985-12-30 | 1985-12-30 | Leading edge slat/anti-icing system and method for airfoil |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3675372D1 true DE3675372D1 (de) | 1990-12-06 |
Family
ID=25215533
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8686201474T Expired - Fee Related DE3675372D1 (de) | 1985-12-30 | 1986-08-27 | Vorfluegelenteisungseinrichtung fuer eine tragflaeche. |
DE19863642791 Withdrawn DE3642791A1 (de) | 1985-12-30 | 1986-12-15 | Vorderkantenvorfluegel/antivereisungsanordnung und -verfahren fuer ein flugzeug |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19863642791 Withdrawn DE3642791A1 (de) | 1985-12-30 | 1986-12-15 | Vorderkantenvorfluegel/antivereisungsanordnung und -verfahren fuer ein flugzeug |
Country Status (4)
Country | Link |
---|---|
US (1) | US4752049A (de) |
EP (1) | EP0230684B1 (de) |
JP (1) | JPS62157898A (de) |
DE (2) | DE3675372D1 (de) |
Families Citing this family (50)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4860534A (en) * | 1988-08-24 | 1989-08-29 | General Motors Corporation | Inlet particle separator with anti-icing means |
US5114100A (en) * | 1989-12-29 | 1992-05-19 | The Boeing Company | Anti-icing system for aircraft |
US5544847A (en) * | 1993-11-10 | 1996-08-13 | The Boeing Company | Leading edge slat/wing combination |
US5865400A (en) * | 1996-06-17 | 1999-02-02 | Senior Flexonics Inc. Stainless Steel Products Division | Multipiece, slidable duct assembly for aircraft anit-icing conduit systems |
US5873544A (en) * | 1996-06-17 | 1999-02-23 | Senior Flexonics, Inc. | Slidable duct assembly for aircraft anti-icing conduit systems |
US6113036A (en) * | 1997-02-04 | 2000-09-05 | Degraffenried; Albert L. | Boundary layer control system |
US6092765A (en) * | 1997-06-09 | 2000-07-25 | White; Richard P. | Infrared deicing system for aircraft |
US6371411B1 (en) | 1999-11-23 | 2002-04-16 | The Boeing Company | Method and apparatus for aircraft inlet ice protection |
US6688558B2 (en) | 1999-11-23 | 2004-02-10 | The Boeing Company | Method and apparatus for aircraft inlet ice protection |
FR2803821B1 (fr) * | 2000-01-17 | 2002-04-05 | Dassault Aviat | Bec de voilure d'aeronef equipe d'un dispositif d'antigivrage, voilure equipee d'un tel bec, et aeronef equipe d'une telle voilure |
US6454219B1 (en) * | 2000-12-04 | 2002-09-24 | Rohr, Inc. | Aircraft wing and method for reducing airframe-generated noise |
US6702233B1 (en) * | 2001-02-07 | 2004-03-09 | Rohr, Inc. | Airfoil anti-icing assembly and method |
NZ511661A (en) | 2001-05-11 | 2003-09-26 | Graham Bond Grove | An improved aerofoil |
BE1014254A3 (fr) | 2001-06-20 | 2003-07-01 | Sonaca Sa | Structure tubulaire mince cloisonnee et son procede de fabrication. |
US6910659B2 (en) * | 2002-10-22 | 2005-06-28 | The Boeing Company | Method and apparatus for liquid containment, such as for aircraft fuel vessels |
US7175136B2 (en) * | 2003-04-16 | 2007-02-13 | The Boeing Company | Method and apparatus for detecting conditions conducive to ice formation |
CA2535885C (en) * | 2003-08-20 | 2014-04-15 | The Boeing Company | Methods and systems for detecting icing conditions |
US7331421B2 (en) * | 2005-03-30 | 2008-02-19 | The Boeing Company | Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods |
US7249735B2 (en) * | 2005-06-30 | 2007-07-31 | The Boeing Company | Translating conduit apparatus for an airplane or equipment |
EP1757519B1 (de) * | 2005-08-25 | 2010-03-31 | GKN Aerospace Services Limited | Vorflügel für eine Flugzeugtragfläche |
FR2917066B1 (fr) * | 2007-06-07 | 2010-05-21 | Messier Bugatti | Procede pour collecter une information relative a une surface aerodynamique mobile d'aeronef |
BE1017685A3 (fr) * | 2007-07-13 | 2009-03-03 | Sonaca Sociutu Anonyme | Chaine porteuse de cables pour volet mobile de bord d'attaque d'une aile d'aeronef. |
US9169779B2 (en) * | 2007-10-09 | 2015-10-27 | United Technologies Corp. | Systems and methods for altering inlet airflow of gas turbine engines |
FR2924409B1 (fr) * | 2007-12-03 | 2010-05-14 | Airbus France | Nacelle d'aeronef comprenant des moyens d'evacuations d'air chaud |
DE102007061590A1 (de) * | 2007-12-20 | 2009-08-13 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug mit einem Hauptflügel und einem verstellbaren Vorflügel |
US8052089B2 (en) * | 2008-11-03 | 2011-11-08 | The Boeing Company | Anti-icing apparatus for honeycomb structures |
US8424810B1 (en) | 2010-03-31 | 2013-04-23 | The Boeing Company | Low noise wing slat system with rigid cove-filled slat |
US8276852B2 (en) | 2010-03-31 | 2012-10-02 | The Boeing Company | Low noise wing slat system with deployable wing leading edge elements |
US8864083B1 (en) * | 2010-03-31 | 2014-10-21 | The Boeing Company | Low noise wing slat system with a fixed wing leading edge and deployable bridging panels |
GB201101335D0 (en) | 2011-01-26 | 2011-03-09 | Airbus Uk Ltd | Aircraft slat assembly with anti-icing system |
DE202011100733U1 (de) * | 2011-05-14 | 2011-06-29 | Kortz, Sebastian, Dr. Ing., 65719 | Verminderung des Reibungswiderstands durch Einblasen von Heißgas in die Strömungsgrenzschicht des Flugzeugrumpfs |
FR2981049B1 (fr) * | 2011-10-07 | 2014-04-11 | Aircelle Sa | Procede de fabrication d'un panneau d'absorption acoustique |
WO2013172914A2 (en) * | 2012-02-27 | 2013-11-21 | Sinhatech | Self adjusting deturbulator enhanced flap and wind deflector |
US9505485B2 (en) * | 2012-05-08 | 2016-11-29 | Lockheed Martin Corporation | Vortex generation |
CN103600845A (zh) * | 2013-08-23 | 2014-02-26 | 中国航空工业集团公司西安飞机设计研究所 | 一种热气通道面积可调式缝翼防冰设计方法 |
US9488067B2 (en) * | 2014-01-14 | 2016-11-08 | The Boeing Company | Aircraft anti-icing systems having deflector vanes |
US9896190B1 (en) * | 2014-05-07 | 2018-02-20 | The Boeing Company | Wing leading edge architecture suitable for laminar flow |
JP6666159B2 (ja) | 2016-01-21 | 2020-03-13 | 三菱航空機株式会社 | 防氷装置、及び、航空機 |
IT201600098196A1 (it) * | 2016-09-30 | 2018-03-30 | Torino Politecnico | Aeromobile dotato di sistema antighiaccio strutturalmente integrato. |
US10569888B2 (en) * | 2016-12-20 | 2020-02-25 | Airbus Operations Gmbh | Leading edge ice-protection system |
GB2571542A (en) | 2018-02-28 | 2019-09-04 | Airbus Operations Ltd | Apparatus and method for heating an aircraft structure |
US20190359341A1 (en) * | 2018-05-25 | 2019-11-28 | The Boeing Company | Method of thermal ice protection for an aircraft wing |
US11440665B2 (en) | 2018-10-23 | 2022-09-13 | Airbus Operations Gmbh | Vented leading-edge assembly and method for manufacturing a vented leading-edge assembly |
US11286034B2 (en) * | 2018-11-22 | 2022-03-29 | Airbus Operations Gmbh | Leading-edge slat for an aircraft |
EP4140877A1 (de) * | 2019-01-18 | 2023-03-01 | Asco Industries NV | Vorflügel für einen flugzeugflügel, verfahren zur herstellung solch eines vorflügels |
US11453477B2 (en) * | 2019-02-28 | 2022-09-27 | Airbus Operations Gmbh | Wing leading edge device and a wing having such a wing leading edge device |
DE102019114098A1 (de) | 2019-05-27 | 2020-12-03 | Airbus Operations Gmbh | Strömungskörper für ein Luftfahrzeug mit einer massiven Hinterkantenkomponente |
CN113365918A (zh) * | 2019-06-27 | 2021-09-07 | 空中客车德国运营有限责任公司 | 用于飞行器的前缘布置结构 |
US11577844B2 (en) | 2020-03-12 | 2023-02-14 | Rohr, Inc. | Variable diameter piccolo tube for anti-icing system |
US20220111951A1 (en) * | 2020-10-08 | 2022-04-14 | The Boeing Company | Air acceleration at leading edge of wing |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2157281A (en) * | 1936-01-10 | 1939-05-09 | Brev Et Procedes Coanada Soc C | Propelling device |
DE746714C (de) * | 1938-07-30 | 1944-12-27 | Einrichtung zur Verhinderung der Eisbildung an dem mit Hilfsfluegeln ausgeruesteten Flugzeugtragwerk | |
FR1026745A (fr) * | 1948-10-23 | 1953-04-30 | Sncase | Procédé de réparatition et d'écoulement d'un fluide pour échange thermique, dispositifs permettant la mise en oeuvre de ce procédé et leurs applications, en particulier aux aérodynes |
FR1103426A (fr) * | 1954-02-26 | 1955-11-03 | Onera (Off Nat Aerospatiale) | Perfectionnements apportés aux voilures d'aérodynes |
US2886264A (en) * | 1957-05-17 | 1959-05-12 | Lockheed Aircraft Corp | Stall roll control device for vertical take-off airplane |
GB991405A (en) * | 1960-05-19 | 1965-05-05 | Dehavilland Aircraft | Improvements relating to aircraft |
US3275265A (en) * | 1962-07-27 | 1966-09-27 | Alvarcz-Calderon Alberto | Boundary layer control flaps and apparatus thereof |
US3596854A (en) * | 1969-06-09 | 1971-08-03 | William R Haney Jr | Vortex generator for airfoil structures |
US3705700A (en) * | 1970-10-23 | 1972-12-12 | Willard R Custer | Air flow control means for channel winged aircraft |
US3889903A (en) * | 1973-03-09 | 1975-06-17 | Boeing Co | Airfoil leading edge structure with boundary layer control |
US3917193A (en) * | 1974-01-21 | 1975-11-04 | Boeing Co | Boundary layer control and anti-icing apparatus for an aircraft wing |
US3933327A (en) * | 1974-08-30 | 1976-01-20 | Rohr Industries, Inc. | Aircraft anti-icing plenum |
US4099691A (en) * | 1976-12-13 | 1978-07-11 | The Boeing Company | Boundary layer control system for aircraft |
US4285482A (en) * | 1979-08-10 | 1981-08-25 | The Boeing Company | Wing leading edge high lift device |
US4398688A (en) * | 1979-12-26 | 1983-08-16 | Lockheed Corporation | Leading edge flap for an airfoil |
-
1985
- 1985-12-30 US US06/814,603 patent/US4752049A/en not_active Expired - Fee Related
-
1986
- 1986-08-27 EP EP86201474A patent/EP0230684B1/de not_active Expired
- 1986-08-27 DE DE8686201474T patent/DE3675372D1/de not_active Expired - Fee Related
- 1986-12-10 JP JP61294621A patent/JPS62157898A/ja active Pending
- 1986-12-15 DE DE19863642791 patent/DE3642791A1/de not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
JPS62157898A (ja) | 1987-07-13 |
US4752049A (en) | 1988-06-21 |
EP0230684A1 (de) | 1987-08-05 |
DE3642791A1 (de) | 1987-07-02 |
EP0230684B1 (de) | 1990-10-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |