PL417165A1 - Zespół odwracacza ciągu - Google Patents
Zespół odwracacza ciąguInfo
- Publication number
- PL417165A1 PL417165A1 PL417165A PL41716516A PL417165A1 PL 417165 A1 PL417165 A1 PL 417165A1 PL 417165 A PL417165 A PL 417165A PL 41716516 A PL41716516 A PL 41716516A PL 417165 A1 PL417165 A1 PL 417165A1
- Authority
- PL
- Poland
- Prior art keywords
- engine
- thrust reverser
- proper
- nacelle
- reverser unit
- Prior art date
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
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
- F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- 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
- F02K1/76—Control or regulation of thrust reversers
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- 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
- F02K1/76—Control or regulation of thrust reversers
- F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
-
- 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
- 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/34—Arrangement of components translated
-
- 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
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
Zespół odwracacza ciągu dla silnika turbospalinowego, zawierającego silnik właściwy (14), gondolę otaczającą (12) co najmniej część silnika właściwego dla wyznaczania kanału zewnętrznego między gondolą a silnikiem właściwym, zawierający osłonę przesuwną, przemieszczalną między pierwszym położeniem a drugim położeniem, klapę przegrodową przemieszczalną między położeniem schowania a położeniem rozłożenia. Zespół odwracacza ciągu zawiera pewną liczbę zespołów siłowników, zarówno do przesuwania osłony, jak i rozkładania klapy przegrodowej.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL417165A PL417165A1 (pl) | 2016-05-12 | 2016-05-12 | Zespół odwracacza ciągu |
EP17169552.1A EP3244052B1 (en) | 2016-05-12 | 2017-05-04 | Thrust reverser assembly |
US15/592,270 US10570853B2 (en) | 2016-05-12 | 2017-05-11 | Thrust reverser assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL417165A PL417165A1 (pl) | 2016-05-12 | 2016-05-12 | Zespół odwracacza ciągu |
Publications (1)
Publication Number | Publication Date |
---|---|
PL417165A1 true PL417165A1 (pl) | 2017-11-20 |
Family
ID=58669747
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL417165A PL417165A1 (pl) | 2016-05-12 | 2016-05-12 | Zespół odwracacza ciągu |
Country Status (3)
Country | Link |
---|---|
US (1) | US10570853B2 (pl) |
EP (1) | EP3244052B1 (pl) |
PL (1) | PL417165A1 (pl) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3016863B1 (fr) * | 2014-01-29 | 2017-05-26 | Snecma | Nacelle pour turboreacteur d'avion |
US10393065B2 (en) * | 2017-11-09 | 2019-08-27 | United Technologies Corporation | Variable nozzle apparatus |
FR3074854B1 (fr) * | 2017-12-08 | 2020-09-11 | Airbus Operations Sas | Turboreacteur comportant une nacelle equipee d'un systeme inverseur comportant des portes |
FR3077605A1 (fr) * | 2018-02-02 | 2019-08-09 | Airbus Operations | Turboreacteur comportant une nacelle equipee d'un systeme inverseur comportant des portes |
US10794328B2 (en) * | 2018-07-06 | 2020-10-06 | Rohr, Inc. | Thrust reverser with blocker door folding linkage |
CN113864079B (zh) * | 2020-06-30 | 2022-07-12 | 中国航发商用航空发动机有限责任公司 | 反推力装置和航空发动机 |
US11891964B1 (en) * | 2023-08-14 | 2024-02-06 | Rolls-Royce North American Technologies Inc. | Method of manufacture of plug nozzle with thrust reverser |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3829020A (en) * | 1973-06-13 | 1974-08-13 | Boeing Co | Translating sleeve variable area nozzle and thrust reverser |
GB1545089A (en) | 1976-09-11 | 1979-05-02 | Rolls Royce | Jet engine thrust reverser and cowl structure |
US4278220A (en) | 1979-03-30 | 1981-07-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thrust reverser for a long duct fan engine |
US5228641A (en) | 1991-08-15 | 1993-07-20 | Rohr, Inc. | Cascade type aircraft engine thrust reverser with hidden link actuator |
US7124981B2 (en) * | 2003-03-04 | 2006-10-24 | The Boeing Company | Thrust reverser utilizing integrated structural bypass duct |
GB0606982D0 (en) * | 2006-04-07 | 2006-05-17 | Rolls Royce Plc | Aeroengine thrust reverser |
FR2946094B1 (fr) | 2009-06-02 | 2014-04-18 | Aircelle Sa | Inverseur de poussee pour nacelle de turboreacteur double flux. |
FR2966883B1 (fr) | 2010-11-03 | 2012-11-02 | Aircelle Sa | Dispositif d'inversion de poussee sans bielle dans la veine |
US9181898B2 (en) | 2011-09-20 | 2015-11-10 | United Technologies Corporation | Thrust reverser for a gas turbine engine with moveable doors |
US9518534B2 (en) | 2013-06-19 | 2016-12-13 | Rohr, Inc. | Reverse scissor thrust reverser for a turbine engine |
FR3009584B1 (fr) * | 2013-08-07 | 2018-03-30 | Safran Nacelles | Inverseur a volets integres |
GB201314527D0 (en) | 2013-08-14 | 2013-09-25 | Rolls Royce Deutschland | Thrust reverser unit |
US9322360B2 (en) * | 2013-10-22 | 2016-04-26 | Rohr, Inc. | Hydraulic blocker door deployment systems |
US9925732B2 (en) | 2013-12-20 | 2018-03-27 | United Technologies Corporation | Metallic-coated polymer thrust reverser cascades |
US9828943B2 (en) | 2014-06-09 | 2017-11-28 | United Technologies Corporation | Variable area nozzle for gas turbine engine |
US10208708B2 (en) * | 2015-01-29 | 2019-02-19 | Rohr, Inc. | Translating cascade hidden blocker door thrust reverser |
-
2016
- 2016-05-12 PL PL417165A patent/PL417165A1/pl unknown
-
2017
- 2017-05-04 EP EP17169552.1A patent/EP3244052B1/en active Active
- 2017-05-11 US US15/592,270 patent/US10570853B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP3244052A1 (en) | 2017-11-15 |
US20170328306A1 (en) | 2017-11-16 |
US10570853B2 (en) | 2020-02-25 |
EP3244052B1 (en) | 2020-01-01 |
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