DE60102840D1 - Vorflügelenteisungseinrichtung für eine Tragfläche eines Flugzeuges - Google Patents
Vorflügelenteisungseinrichtung für eine Tragfläche eines FlugzeugesInfo
- Publication number
- DE60102840D1 DE60102840D1 DE60102840T DE60102840T DE60102840D1 DE 60102840 D1 DE60102840 D1 DE 60102840D1 DE 60102840 T DE60102840 T DE 60102840T DE 60102840 T DE60102840 T DE 60102840T DE 60102840 D1 DE60102840 D1 DE 60102840D1
- Authority
- DE
- Germany
- Prior art keywords
- slat
- aircraft wing
- icing device
- icing
- wing
- 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
Links
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)
- Nozzles (AREA)
- Cold Air Circulating Systems And Constructional Details In Refrigerators (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Drying Of Solid Materials (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0000525A FR2803821B1 (fr) | 2000-01-17 | 2000-01-17 | Bec de voilure d'aeronef equipe d'un dispositif d'antigivrage, voilure equipee d'un tel bec, et aeronef equipe d'une telle voilure |
FR0000525 | 2000-01-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60102840D1 true DE60102840D1 (de) | 2004-05-27 |
DE60102840T2 DE60102840T2 (de) | 2005-04-28 |
Family
ID=8845970
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60102840T Expired - Lifetime DE60102840T2 (de) | 2000-01-17 | 2001-01-15 | Vorflügelenteisungseinrichtung für eine Tragfläche eines Flugzeuges |
Country Status (7)
Country | Link |
---|---|
US (1) | US6467730B2 (de) |
EP (1) | EP1116656B1 (de) |
BR (1) | BR0100086B1 (de) |
CA (1) | CA2330397C (de) |
DE (1) | DE60102840T2 (de) |
FR (1) | FR2803821B1 (de) |
IL (1) | IL140885A (de) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6739553B2 (en) * | 2000-04-05 | 2004-05-25 | Bell Helicopter Textrom, Inc. | K-spar configuration for bonded wing construction |
US7178760B2 (en) | 2003-05-30 | 2007-02-20 | Bombardier Aéronautique | Method and apparatus for inhibiting accretion of airborne material on a surface of an aircraft |
US7331421B2 (en) * | 2005-03-30 | 2008-02-19 | The Boeing Company | Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods |
US7157663B1 (en) | 2005-10-12 | 2007-01-02 | The Boeing Company | Conducting-fiber deicing systems and methods |
US20070080481A1 (en) * | 2005-10-12 | 2007-04-12 | The Boeing Company | Apparatus and methods for fabrication of composite components |
GB2440133A (en) * | 2006-07-18 | 2008-01-23 | Gkn Aerospace Transparency Sys | A de-icing heated leading edge component of an aircraft |
US7980515B2 (en) * | 2006-08-25 | 2011-07-19 | 0832042 B.C. Ltd. | Aircraft wing modification and related methods |
US8052089B2 (en) * | 2008-11-03 | 2011-11-08 | The Boeing Company | Anti-icing apparatus for honeycomb structures |
US8061657B2 (en) * | 2008-12-31 | 2011-11-22 | General Electric Company | Method and apparatus for aircraft anti-icing |
US8100364B2 (en) * | 2009-01-15 | 2012-01-24 | Textron Innovations Inc. | Anti-icing piccolo tube standoff |
FR2954279B1 (fr) * | 2009-12-18 | 2014-08-22 | Airbus Operations Sas | Entree d'air d'une nacelle d'aeronef integrant des moyens d'injection en air chaud pour le traitement du givre optimises |
JP2011183922A (ja) * | 2010-03-08 | 2011-09-22 | Mitsubishi Heavy Ind Ltd | 航空機における翼前縁部の防除氷装置及び航空機主翼 |
DE102012002132A1 (de) | 2012-02-03 | 2013-08-08 | Airbus Operations Gmbh | Vereisungsschutzsystem für ein Flugzeug und Verfahren zum Betreiben eines Vereisungsschutzsystems |
JP6193691B2 (ja) * | 2013-09-11 | 2017-09-06 | 三菱航空機株式会社 | 防氷システム、及び、航空機 |
US9896190B1 (en) * | 2014-05-07 | 2018-02-20 | The Boeing Company | Wing leading edge architecture suitable for laminar flow |
US10393020B2 (en) * | 2015-08-26 | 2019-08-27 | Rohr, Inc. | Injector nozzle configuration for swirl anti-icing system |
US9815558B2 (en) | 2015-12-09 | 2017-11-14 | King Fahd University Of Petroleum And Minerals | Anti-icing apparatus and system |
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 |
JP2017136893A (ja) * | 2016-02-01 | 2017-08-10 | 三菱航空機株式会社 | 防氷装置、及び、航空機 |
JP6839920B2 (ja) * | 2016-02-12 | 2021-03-10 | 三菱航空機株式会社 | 防氷装置、及び、航空機 |
CA3028442A1 (en) * | 2016-06-29 | 2018-01-04 | Bombardier Inc. | Temperature monitoring unit for aircraft wing structure and associated installation method |
GB201710385D0 (en) * | 2017-06-29 | 2017-08-16 | Airbus Operations Gmbh | Aerofoil structure and method of assembly |
CN107905961B (zh) * | 2017-11-09 | 2019-12-20 | 新疆金风科技股份有限公司 | 叶片的加热除冰系统及其方法、叶片和风力发电机组 |
ES2943266T3 (es) * | 2017-12-28 | 2023-06-12 | Airbus Operations Gmbh | Estructura de borde de ataque para un sistema de control de flujo de una aeronave |
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 |
US20210024221A1 (en) * | 2019-07-25 | 2021-01-28 | Airbus Operations Sas | Leading edge member for an airfoil of an aircraft |
BE1028506B1 (fr) * | 2020-12-24 | 2022-02-11 | Sonaca Sa | Système pour aeronef de protection contre le givre par air chaud souffle a penalite energetique reduite |
US20240077018A1 (en) * | 2022-09-02 | 2024-03-07 | Rohr, Inc. | Thermal anti-icing system for an aircraft propulsion system |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2320870A (en) * | 1940-09-20 | 1943-06-01 | Lockheed Aircraft Corp | Anti-icing duct |
FR979460A (fr) * | 1942-05-07 | 1951-04-26 | Dispositif du dégivrage par réchauffage du bord d'attaque des ailes | |
US2556736A (en) * | 1945-06-22 | 1951-06-12 | Curtiss Wright Corp | Deicing system for aircraft |
US2581760A (en) * | 1946-04-02 | 1952-01-08 | Douglas Aircraft Co Inc | Airplane deicing construction |
US2470128A (en) * | 1947-10-07 | 1949-05-17 | Glenn L Martin Co | Airplane wing leading edge construction |
GB1032681A (en) * | 1961-05-12 | 1966-06-15 | Napier & Son Ltd | Ice protection systems for aerofoil surfaces |
US4099691A (en) * | 1976-12-13 | 1978-07-11 | The Boeing Company | Boundary layer control system for aircraft |
US4615499A (en) * | 1983-08-12 | 1986-10-07 | The Boeing Company | Wing slat anti-ice air duct system |
US4741499A (en) * | 1984-12-31 | 1988-05-03 | The Boeing Company | Anti-icing system for aircraft |
US4752049A (en) * | 1985-12-30 | 1988-06-21 | The Boeing Company | Leading edge slat/anti-icing system and method for airfoil |
US4688745A (en) * | 1986-01-24 | 1987-08-25 | Rohr Industries, Inc. | Swirl anti-ice system |
US5088277A (en) * | 1988-10-03 | 1992-02-18 | General Electric Company | Aircraft engine inlet cowl anti-icing system |
US5011098A (en) * | 1988-12-30 | 1991-04-30 | The Boeing Company | Thermal anti-icing system for aircraft |
US5807454A (en) * | 1995-09-05 | 1998-09-15 | Honda Giken Kogyo Kabushiki Kaisha | Method of maufacturing a leading edge structure for aircraft |
-
2000
- 2000-01-17 FR FR0000525A patent/FR2803821B1/fr not_active Expired - Fee Related
-
2001
- 2001-01-09 CA CA002330397A patent/CA2330397C/en not_active Expired - Fee Related
- 2001-01-14 IL IL14088501A patent/IL140885A/en not_active IP Right Cessation
- 2001-01-15 EP EP01400098A patent/EP1116656B1/de not_active Expired - Lifetime
- 2001-01-15 DE DE60102840T patent/DE60102840T2/de not_active Expired - Lifetime
- 2001-01-16 BR BRPI0100086-1A patent/BR0100086B1/pt not_active IP Right Cessation
- 2001-01-17 US US09/760,715 patent/US6467730B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE60102840T2 (de) | 2005-04-28 |
EP1116656B1 (de) | 2004-04-21 |
US20010023909A1 (en) | 2001-09-27 |
IL140885A (en) | 2004-01-04 |
BR0100086B1 (pt) | 2009-01-13 |
CA2330397C (en) | 2008-10-28 |
US6467730B2 (en) | 2002-10-22 |
FR2803821B1 (fr) | 2002-04-05 |
BR0100086A (pt) | 2001-08-28 |
IL140885A0 (en) | 2002-02-10 |
EP1116656A1 (de) | 2001-07-18 |
CA2330397A1 (en) | 2001-07-17 |
FR2803821A1 (fr) | 2001-07-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |