DE602005007536D1 - Bremsverfahren für Flugzeuge und Nebenstromluftstrahltriebwerk zur Umsetzung des Verfahrens - Google Patents
Bremsverfahren für Flugzeuge und Nebenstromluftstrahltriebwerk zur Umsetzung des VerfahrensInfo
- Publication number
- DE602005007536D1 DE602005007536D1 DE602005007536T DE602005007536T DE602005007536D1 DE 602005007536 D1 DE602005007536 D1 DE 602005007536D1 DE 602005007536 T DE602005007536 T DE 602005007536T DE 602005007536 T DE602005007536 T DE 602005007536T DE 602005007536 D1 DE602005007536 D1 DE 602005007536D1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft
- implement
- jet engine
- bypass jet
- braking
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
- B64C7/02—Nacelles
-
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
- F02K1/563—Reversing jet main flow in specified direction, e.g. to obviate its reinjection
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H99/00—Subject matter not provided for in other groups of this subclass
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/90—Braking
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/90—Braking
- F05D2260/901—Braking using aerodynamic forces, i.e. lift or drag
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Turbines (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Retarders (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0406697A FR2871776B1 (fr) | 2004-06-21 | 2004-06-21 | Procede de freinage d'un avion et turboreacteur a double flux pour la mise en oeuvre du procede |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602005007536D1 true DE602005007536D1 (de) | 2008-07-31 |
Family
ID=34940204
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602005007536T Active DE602005007536D1 (de) | 2004-06-21 | 2005-06-17 | Bremsverfahren für Flugzeuge und Nebenstromluftstrahltriebwerk zur Umsetzung des Verfahrens |
Country Status (5)
Country | Link |
---|---|
US (1) | US7469528B2 (de) |
EP (1) | EP1609719B1 (de) |
DE (1) | DE602005007536D1 (de) |
FR (1) | FR2871776B1 (de) |
RU (1) | RU2415287C2 (de) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2431626A (en) | 2005-10-26 | 2007-05-02 | Avcen Ltd | Bypass turbofan engine |
FR2958688B1 (fr) | 2010-04-09 | 2013-02-22 | Aircelle Sa | Ensemble propulsif pour aeronef muni de moyens d'inversion de poussee |
US8857761B2 (en) | 2010-10-27 | 2014-10-14 | Ata Engineering, Inc. | Variable geometry aircraft pylon structure and related operation techniques |
US9567867B2 (en) | 2011-09-14 | 2017-02-14 | Ata Engineering, Inc. | Methods and apparatus for deployable swirl vanes |
US9038367B2 (en) * | 2011-09-16 | 2015-05-26 | United Technologies Corporation | Fan case thrust reverser |
FR3043650B1 (fr) * | 2015-11-16 | 2018-11-30 | Safran Aircraft Engines | Aube de stator de turbomachine, carter de soufflante comprenant une telle aube, systeme d'inversion de poussee d'une turbomachine equipee d'une telle aube et turbomachine equipee de ladite aube, dudit carter ou dudit systeme |
US10935093B2 (en) | 2018-03-29 | 2021-03-02 | Honeywell International Inc. | Active brake cooling using nitrogen enriched air |
RU2711743C2 (ru) * | 2018-06-07 | 2020-01-21 | Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Устройство отклонения вектора реверсированной тяги турбореактивного двигателя |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1197028A (en) * | 1968-10-24 | 1970-07-01 | Rolls Royce | Thrust Reverser for Jet-Propulsion Engines |
GB1365491A (en) * | 1971-01-02 | 1974-09-04 | Dowty Rotol Ltd | Gas turbine ducted fan engines and fans therefor |
GB1388406A (en) * | 1971-12-15 | 1975-03-26 | Rolls Royce | Gas turbine ducted fan engines |
GB1424193A (en) * | 1972-03-21 | 1976-02-11 | Rolls Royce | Gas turbine ducted fan engines |
FR2506843B1 (fr) * | 1981-05-29 | 1987-04-24 | Hurel Dubois Avions | Dispositif d'inversion de poussee pour turboreacteur d'avion |
US4541237A (en) * | 1983-10-17 | 1985-09-17 | Avco Corporation | Sub-idle speed control apparatus for an airplane turbine engine |
US5315821A (en) * | 1993-02-05 | 1994-05-31 | General Electric Company | Aircraft bypass turbofan engine thrust reverser |
-
2004
- 2004-06-21 FR FR0406697A patent/FR2871776B1/fr not_active Expired - Fee Related
-
2005
- 2005-06-17 EP EP05105407A patent/EP1609719B1/de active Active
- 2005-06-17 DE DE602005007536T patent/DE602005007536D1/de active Active
- 2005-06-20 US US11/155,511 patent/US7469528B2/en active Active
- 2005-06-20 RU RU2005119132/06A patent/RU2415287C2/ru active
Also Published As
Publication number | Publication date |
---|---|
FR2871776B1 (fr) | 2007-11-02 |
FR2871776A1 (fr) | 2005-12-23 |
RU2415287C2 (ru) | 2011-03-27 |
US7469528B2 (en) | 2008-12-30 |
EP1609719B1 (de) | 2008-06-18 |
EP1609719A1 (de) | 2005-12-28 |
RU2005119132A (ru) | 2006-12-27 |
US20050279081A1 (en) | 2005-12-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |