GB1181746A - Thrust Reverser for Jet Propulsion Plant - Google Patents
Thrust Reverser for Jet Propulsion PlantInfo
- Publication number
- GB1181746A GB1181746A GB2918568A GB2918568A GB1181746A GB 1181746 A GB1181746 A GB 1181746A GB 2918568 A GB2918568 A GB 2918568A GB 2918568 A GB2918568 A GB 2918568A GB 1181746 A GB1181746 A GB 1181746A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flaps
- duct
- casing
- gases
- flow
- 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
Links
- 239000007789 gas Substances 0.000 abstract 7
- 230000001141 propulsive effect Effects 0.000 abstract 4
- 230000013011 mating Effects 0.000 abstract 2
- 210000002105 tongue Anatomy 0.000 abstract 1
- 238000011144 upstream manufacturing Methods 0.000 abstract 1
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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
Abstract
1,181,746. Deflecting propulsive gases. ROLLS-ROYCE Ltd. 19 June, 1968, No. 29185/68. Heading B7G. A thrust reverser for a front fan gas turbine engine, or other engine, comprises a plurality of thrust reverser flaps 24, each pivoted about its centre of pressure 25, the pivot pin at 25 being attached to the double walled casing of a duct 16 in which a front fan 17 rotates. The duct 16 is supported by stays 20 extending radially from the upstream portions of an engine casing 11. The flaps 24 may be pivoted about points 25 from an inoperative position in which they merge with the walls of the duct 16, rearward flow of propulsive gases being unimpeded, to an operative position, Fig. 2, in which flow of gases to the rear of duct 16 is impeded and the. propulsive gases are caused to flow radially through gaps 32 as indicated by arrow A and produce forward thrust. The flow of gases through the radially disposed gaps 32 in the casing of the duct 16 is aided by shaped members 36, which members are movable fore and aft between the two walls 26, 27 of the casing 16 and are connected at their rearward ends to flaps 24 by struts 42. The forward ends of members 36 are connected to rams or screw jacks, so that coupled movement of members 36 and flaps 24 is possible. Loss of propulsive gases through gaps 32 when flaps 24 are in inoperative positions is minimized by mating tongues and recesses 44 and 45 and by mating surfaces 34, 33 on the flaps and casing.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2918568A GB1181746A (en) | 1968-06-19 | 1968-06-19 | Thrust Reverser for Jet Propulsion Plant |
| FR6919387A FR2030034A1 (en) | 1968-06-19 | 1969-06-11 | |
| DE19691930829 DE1930829A1 (en) | 1968-06-19 | 1969-06-18 | Thrust reverser for jet propulsion |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2918568A GB1181746A (en) | 1968-06-19 | 1968-06-19 | Thrust Reverser for Jet Propulsion Plant |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1181746A true GB1181746A (en) | 1970-02-18 |
Family
ID=10287514
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2918568A Expired GB1181746A (en) | 1968-06-19 | 1968-06-19 | Thrust Reverser for Jet Propulsion Plant |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE1930829A1 (en) |
| FR (1) | FR2030034A1 (en) |
| GB (1) | GB1181746A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4960243A (en) * | 1988-10-20 | 1990-10-02 | Societe Anonyme Dite Hispano-Suiza | Thrust reverser for a turbojet engine |
| US4976466A (en) * | 1988-07-18 | 1990-12-11 | Societe Anonyme Dite Hispano-Suiza | Thrust reverser for a turbojet engine |
| US5090197A (en) * | 1989-08-23 | 1992-02-25 | Societe Anonyme Dite Hispano Suiza | Pivoting door cascade thrust reverser |
| GB2256175A (en) * | 1991-05-31 | 1992-12-02 | Rolls Royce Plc | Thrust reverser for high bypass ducted fan gas turbine engine. |
| US8783010B2 (en) | 2010-04-28 | 2014-07-22 | Aircelle | Cascade type thrust reverser having a pivoting door |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2621082A1 (en) * | 1987-09-30 | 1989-03-31 | Hispano Suiza Sa | PUSH INVERTER OF TURBOJET WITH DOORS PROVIDED WITH A VEIN PROFILE PLATE |
| DE3844188C1 (en) * | 1988-12-29 | 1990-05-17 | Mtu Muenchen Gmbh | |
| FR2730764B1 (en) * | 1995-02-21 | 1997-03-14 | Hispano Suiza Sa | PUSH INVERTER WITH DOORS ASSOCIATED WITH A DOWNSTREAM PANEL |
| FR2736682B1 (en) * | 1995-07-12 | 1997-08-14 | Hispano Suiza Sa | DOUBLE FLOW TURBOMACHINE DRIVE INVERTER WITH DISSYMMETRIC DOORS |
| FR2740834B1 (en) | 1995-11-02 | 1997-12-05 | Hispano Suiza Sa | DOUBLE FLOW TURBOREACTOR DRIVE INVERTER WITH SECONDARY DOORS |
| FR2741910B1 (en) * | 1995-11-30 | 1998-01-02 | Hispano Suiza Sa | DOOR REVERSER OF TURBOJET WITH DOORS WITH ARTICULATED REAR PANEL |
| FR2748525B1 (en) * | 1996-05-09 | 1998-06-19 | Hispano Suiza Sa | TURBOREACTOR DRIVE INVERTER WITH DOORS WITH DEFLECTIVE BLADES |
| FR2748779B1 (en) * | 1996-05-15 | 1998-06-19 | Hispano Suiza Sa | TURBOREACTOR DRIVE INVERTER WITH DOORS ASSOCIATED WITH A UPSTREAM PANEL |
| FR2748778B1 (en) * | 1996-05-15 | 1998-06-19 | Hispano Suiza Sa | TURBOREACTOR DRIVE INVERTER WITH DOORS ASSOCIATED WITH A UPSTREAM PANEL |
| FR2751377B1 (en) * | 1996-07-18 | 1998-09-04 | Hispano Suiza Sa | DOOR TURBOREACTOR THRUST CHANGEOVER WITH SLIDING PANEL |
| FR2752017B1 (en) * | 1996-08-01 | 1998-10-16 | Hispano Suiza Sa | TURBOREACTOR DRIVE INVERTER WITH SCOOPING DOORS |
| FR2754313B1 (en) * | 1996-10-03 | 1999-01-08 | Hispano Suiza Sa | DOOR REVERSER WITH OPTIMIZED CONTROL JACK INSTALLATION |
| FR2754565B1 (en) * | 1996-10-10 | 1999-01-08 | Hispano Suiza Sa | PUSH INVERTER WITH CONTROLLED LEAKAGE FLOW DOORS |
| FR2757215B1 (en) * | 1996-12-12 | 1999-01-22 | Hispano Suiza Sa | DOOR TURBORATOR PUSH INVERTER HAVING DEFLECTIVE VANES ASSOCIATED WITH THE FIXED STRUCTURE |
| FR2760047B1 (en) * | 1997-02-27 | 1999-05-07 | Hispano Suiza Sa | TURBOJET DRIVE INVERTER WITH DOORS ASSOCIATED WITH A CONTROL SYNCHRONIZATION DEVICE |
| FR2760788B1 (en) * | 1997-03-13 | 1999-05-07 | Hispano Suiza Sa | PUSH INVERTER WITH TURBO JET WITH PLATED EXTERNAL STRUCTURE |
| FR2760789B1 (en) * | 1997-03-13 | 2001-09-07 | Hispano Suiza Sa | PUSH INVERTER OF TURBO JET WITH SELF-SUPPORTED EXTERNAL STRUCTURE |
| FR2764340B1 (en) * | 1997-06-05 | 1999-07-16 | Hispano Suiza Sa | TURBOREACTOR DRIVE INVERTER WITH OPTIMIZED DRIVE MOBILE SPOILER |
| FR2764644B1 (en) * | 1997-06-12 | 1999-07-16 | Hispano Suiza Sa | DOUBLE-FLOW TURBOREACTOR ASSOCIATED WITH A PUSH INVERTER WITH AN ADJUSTED FAIRING IN THE FLUID Vein |
| FR2764643B1 (en) * | 1997-06-12 | 1999-07-16 | Hispano Suiza Sa | PUSH INVERTER WITH TURBOREACTOR DOORS WITH VARIABLE EJECTION SECTION |
| FR2799796B1 (en) | 1999-10-14 | 2002-08-30 | Hispano Suiza Sa | CENTER PIVOT DOOR TURBOREACTOR DRIVE INVERTER |
| US6968675B2 (en) | 2002-10-29 | 2005-11-29 | Rohr, Inc. | Cascadeless fan thrust reverser with plume control |
| FR2927956A1 (en) * | 2008-02-26 | 2009-08-28 | Aircelle Sa | THRUST INVERTER FOR DOUBLE FLOW TURBOREACTOR NACELLE |
-
1968
- 1968-06-19 GB GB2918568A patent/GB1181746A/en not_active Expired
-
1969
- 1969-06-11 FR FR6919387A patent/FR2030034A1/fr not_active Withdrawn
- 1969-06-18 DE DE19691930829 patent/DE1930829A1/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4976466A (en) * | 1988-07-18 | 1990-12-11 | Societe Anonyme Dite Hispano-Suiza | Thrust reverser for a turbojet engine |
| US4960243A (en) * | 1988-10-20 | 1990-10-02 | Societe Anonyme Dite Hispano-Suiza | Thrust reverser for a turbojet engine |
| US5090197A (en) * | 1989-08-23 | 1992-02-25 | Societe Anonyme Dite Hispano Suiza | Pivoting door cascade thrust reverser |
| GB2256175A (en) * | 1991-05-31 | 1992-12-02 | Rolls Royce Plc | Thrust reverser for high bypass ducted fan gas turbine engine. |
| US8783010B2 (en) | 2010-04-28 | 2014-07-22 | Aircelle | Cascade type thrust reverser having a pivoting door |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2030034A1 (en) | 1970-10-30 |
| DE1930829A1 (en) | 1970-03-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1181746A (en) | Thrust Reverser for Jet Propulsion Plant | |
| GB1085780A (en) | Improvements in thrust reverser | |
| GB1104764A (en) | Improvements in thrust reverters for jet propulsion powerplants | |
| GB1130268A (en) | Improvements in or relating to gas turbine by-pass engines | |
| US3608314A (en) | Thrust reverser | |
| GB937829A (en) | Deflector assembly defining convergent nozzles | |
| GB1318748A (en) | Gas turgine ducted fan engines for aircraft | |
| GB933612A (en) | Jet engine thrust reversers | |
| GB1085619A (en) | Gas turbine engine | |
| GB1247691A (en) | Improvements in or relating to fan ducts for gas turbine ducted fan engines | |
| GB1111219A (en) | Gas turbine engine | |
| GB1033583A (en) | Thrust reverser for a jet propulsion engine | |
| GB874496A (en) | Jet propulsion nozzle noise suppression means and thrust reverser | |
| GB1479149A (en) | Variable pitch ducted fan gas turbine power plant | |
| GB1047990A (en) | Aircraft jet propulsion power plant | |
| GB1276265A (en) | Improvements in or relating to thrust deflectors for gas turbine ducted fan engines | |
| GB1139005A (en) | Improvements in or relating to gas turbine by-pass engines | |
| GB1340817A (en) | Dual-flow gas turbine jet engines | |
| GB1161949A (en) | Improvements in Aircraft Gas Generator Exhaust Nozzle Structures | |
| GB882424A (en) | Improvements in or relating to aircraft jet propulsion apparatus | |
| GB1278801A (en) | Jet nozzle for a gas turbine engine | |
| GB1136339A (en) | Gas turbine by-pass engine | |
| GB1209098A (en) | Thrust reverser for a gas turbine engine | |
| GB1449230A (en) | Turbojet-engine powered aircraft having thrust reversing means | |
| GB1066268A (en) | Jet propulsion power plant |