SG11201404965WA - Gas turbine engine thrust reverser system - Google Patents
Gas turbine engine thrust reverser systemInfo
- Publication number
- SG11201404965WA SG11201404965WA SG11201404965WA SG11201404965WA SG11201404965WA SG 11201404965W A SG11201404965W A SG 11201404965WA SG 11201404965W A SG11201404965W A SG 11201404965WA SG 11201404965W A SG11201404965W A SG 11201404965WA SG 11201404965W A SG11201404965W A SG 11201404965WA
- Authority
- SG
- Singapore
- Prior art keywords
- gas turbine
- turbine engine
- thrust reverser
- engine thrust
- reverser system
- 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
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
-
- 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
- F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
-
- 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
- F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/431,356 US9097209B2 (en) | 2012-03-27 | 2012-03-27 | Gas turbine engine thrust reverser system |
PCT/US2013/033172 WO2014007875A2 (en) | 2012-03-27 | 2013-03-20 | Gas turbine engine thrust reverser system |
Publications (1)
Publication Number | Publication Date |
---|---|
SG11201404965WA true SG11201404965WA (en) | 2014-10-30 |
Family
ID=49233016
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG11201404965WA SG11201404965WA (en) | 2012-03-27 | 2013-03-20 | Gas turbine engine thrust reverser system |
Country Status (4)
Country | Link |
---|---|
US (1) | US9097209B2 (de) |
EP (1) | EP2831402B1 (de) |
SG (1) | SG11201404965WA (de) |
WO (1) | WO2014007875A2 (de) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9108736B2 (en) | 2012-06-05 | 2015-08-18 | United Technologies Corporation | Nacelle inner flow structure leading edge latching system |
WO2014197029A2 (en) | 2013-03-14 | 2014-12-11 | United Technologies Corporation | Latching actuation mechanism for nacelle mounted latching system |
US20150107222A1 (en) * | 2013-10-18 | 2015-04-23 | Rohr, Inc. | Thrust reverser fan ramp partially formed on aft end of fan case |
US9534562B2 (en) * | 2014-04-25 | 2017-01-03 | Rohr, Inc. | System and apparatus for a thrust reverser |
FR3078951B1 (fr) | 2018-03-13 | 2020-02-28 | Airbus Operations | Turboreacteur comportant une nacelle equipee d'un carter de soufflante et d'une structure fixe |
CN112796882B (zh) * | 2020-12-30 | 2022-03-15 | 长江大学 | 一种涡轮螺旋桨发动机反推系统 |
EP4180636A1 (de) * | 2021-11-12 | 2023-05-17 | Raytheon Technologies Corporation | Radialstrebenrahmenverbindung zwischen fangehäuse und kerngehäuse in einem gasturbinenmotor |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5239822A (en) * | 1992-01-14 | 1993-08-31 | The Boeing Company | Composite structure for thrust reverser torque box |
FR2730763B1 (fr) | 1995-02-21 | 1997-03-14 | Hispano Suiza Sa | Inverseur de poussee a volets aval pour turboreacteur |
US5806302A (en) | 1996-09-24 | 1998-09-15 | Rohr, Inc. | Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser |
FR2759418B1 (fr) | 1997-02-13 | 1999-03-19 | Snecma | Inverseur de poussee pour turbosoufflante a tres grand taux de dilution |
US6637186B1 (en) * | 1997-11-11 | 2003-10-28 | United Technologies Corporation | Fan case liner |
US6170254B1 (en) * | 1998-12-18 | 2001-01-09 | Rohr, Inc. | Translating sleeve for cascade type thrust reversing system for fan gas turbine engine for an aircraft |
GB0505184D0 (en) | 2005-03-14 | 2005-04-20 | Rolls Royce Plc | Thrust reverser mounting structure |
US20080063508A1 (en) * | 2006-09-08 | 2008-03-13 | Barry Barnett | Fan case abradable |
EP2181262B1 (de) | 2007-08-08 | 2012-05-16 | Rohr, Inc. | Veränderliche fächerdüse mit bypass-strom |
US7735778B2 (en) | 2007-11-16 | 2010-06-15 | Pratt & Whitney Canada Corp. | Pivoting fairings for a thrust reverser |
US8172175B2 (en) | 2007-11-16 | 2012-05-08 | The Nordam Group, Inc. | Pivoting door thrust reverser for a turbofan gas turbine engine |
US8091827B2 (en) | 2007-11-16 | 2012-01-10 | The Nordam Group, Inc. | Thrust reverser door |
US8201390B2 (en) * | 2007-12-12 | 2012-06-19 | Spirit Aerosystems, Inc. | Partial cascade thrust reverser |
FR2925607B1 (fr) | 2007-12-21 | 2013-05-10 | Aircelle Sa | Nacelle pour moteur d'aeronef a tuyere de section variable |
US8127531B2 (en) | 2008-11-11 | 2012-03-06 | The Boeing Company | Radially translating fan nozzle nacelle |
US8127532B2 (en) * | 2008-11-26 | 2012-03-06 | The Boeing Company | Pivoting fan nozzle nacelle |
GB0917057D0 (en) | 2009-09-29 | 2009-11-11 | Goodrich Actuation Systems Ltd | Thrust reverser actuation |
US8869507B2 (en) | 2010-01-13 | 2014-10-28 | United Technologies Corporation | Translatable cascade thrust reverser |
-
2012
- 2012-03-27 US US13/431,356 patent/US9097209B2/en active Active
-
2013
- 2013-03-20 WO PCT/US2013/033172 patent/WO2014007875A2/en active Application Filing
- 2013-03-20 SG SG11201404965WA patent/SG11201404965WA/en unknown
- 2013-03-20 EP EP13813553.8A patent/EP2831402B1/de active Active
Also Published As
Publication number | Publication date |
---|---|
EP2831402B1 (de) | 2017-07-12 |
WO2014007875A3 (en) | 2014-03-13 |
EP2831402A4 (de) | 2015-12-16 |
EP2831402A2 (de) | 2015-02-04 |
US9097209B2 (en) | 2015-08-04 |
US20130255225A1 (en) | 2013-10-03 |
WO2014007875A2 (en) | 2014-01-09 |
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