IT996422B - Invertitore di spinta per condotto di scarico di motore a getto - Google Patents
Invertitore di spinta per condotto di scarico di motore a gettoInfo
- Publication number
- IT996422B IT996422B IT53598/73A IT5359873A IT996422B IT 996422 B IT996422 B IT 996422B IT 53598/73 A IT53598/73 A IT 53598/73A IT 5359873 A IT5359873 A IT 5359873A IT 996422 B IT996422 B IT 996422B
- Authority
- IT
- Italy
- Prior art keywords
- exhaust duct
- engine exhaust
- jet engine
- thrust inverter
- thrust
- 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
-
- 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
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/827—Sound absorbing structures or liners
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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00329770A US3831376A (en) | 1973-02-05 | 1973-02-05 | Thrust reverser |
Publications (1)
Publication Number | Publication Date |
---|---|
IT996422B true IT996422B (it) | 1975-12-10 |
Family
ID=23286937
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT53598/73A IT996422B (it) | 1973-02-05 | 1973-11-09 | Invertitore di spinta per condotto di scarico di motore a getto |
Country Status (2)
Country | Link |
---|---|
US (1) | US3831376A (it) |
IT (1) | IT996422B (it) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4075833A (en) * | 1976-01-02 | 1978-02-28 | General Electric Company | Variable area inlet for a gas turbine engine |
US5092525A (en) * | 1984-11-02 | 1992-03-03 | United Technologies Corporation | Exhaust nozzle with reverser exhaust door mechanism |
GB2189550A (en) * | 1986-04-25 | 1987-10-28 | Rolls Royce | A gas turbine engine powerplant with flow control devices |
FR2712929B1 (fr) * | 1993-11-24 | 1995-12-29 | Hispano Suiza Sa | Inverseur de poussée de turboréacteur à double flux. |
FR2730764B1 (fr) * | 1995-02-21 | 1997-03-14 | Hispano Suiza Sa | Inverseur de poussee a portes associees a un panneau aval |
FR2748779B1 (fr) * | 1996-05-15 | 1998-06-19 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes associees a un panneau amont |
US5987880A (en) * | 1997-07-08 | 1999-11-23 | Mcdonnell Douglas Corporation | Supersonic engine, multi-port thrust reversing system |
FR2787513B1 (fr) * | 1998-12-17 | 2001-01-19 | Turbomeca | Dispositif d'echappement multicanal de turbomachine traite acoustiquement |
FR2900980B1 (fr) * | 2006-05-10 | 2011-08-19 | Aircelle Sa | Nacelle pour turboreacteur double flux a grand taux de dilution |
US8316632B2 (en) * | 2009-02-25 | 2012-11-27 | Spirit Aerosystems, Inc. | Thrust reverser configuration for a short fan duct |
FR2947868B1 (fr) * | 2009-07-08 | 2011-12-16 | Airbus Operations Sas | Nacelle d'aeronef incorporant un dispositif pour inverser la poussee |
FR2952681B1 (fr) * | 2009-11-18 | 2017-10-06 | Aircelle Sa | Inverseur de poussee |
FR2953490B1 (fr) * | 2009-12-07 | 2012-02-24 | Aircelle Sa | Ensemble arriere de nacelle pour turboreacteur |
DE102012002885A1 (de) * | 2012-02-14 | 2013-08-14 | Rolls-Royce Deutschland Ltd & Co Kg | Fluggasturbinenschubumkehrvorrichtung |
US9783315B2 (en) * | 2012-02-24 | 2017-10-10 | Rohr, Inc. | Nacelle with longitudinal translating cowling and rotatable sleeves |
US9068532B2 (en) * | 2012-07-24 | 2015-06-30 | Rohr, Inc. | Translating sleeve thrust reverser with movable cascade |
US9623976B2 (en) * | 2012-07-25 | 2017-04-18 | Rohr, Inc. | Nacelle for a high bypass ratio engine with multiple flow paths |
US20160017815A1 (en) * | 2013-03-12 | 2016-01-21 | United Technologies Corporation | Expanding shell flow control device |
US20160076484A1 (en) * | 2013-06-07 | 2016-03-17 | Aircelle | Turbojet engine nacelle thrust reverser comprising cascades secured to the mobile cowls |
FR3010146B1 (fr) | 2013-08-30 | 2015-12-18 | Aircelle Sa | Nacelle a dispositif d’inversion de poussee a grilles mobiles maintenues |
US10309343B2 (en) | 2014-11-06 | 2019-06-04 | Rohr, Inc. | Split sleeve hidden door thrust reverser |
US10018151B2 (en) | 2015-01-14 | 2018-07-10 | The Boeing Company | Methods and apparatus to vary reverse thrust of aircraft engines |
US9874176B2 (en) | 2015-01-14 | 2018-01-23 | The Boeing Company | Methods and apparatus to vary reverse thrust of aircraft engines |
US10208708B2 (en) * | 2015-01-29 | 2019-02-19 | Rohr, Inc. | Translating cascade hidden blocker door thrust reverser |
US10030608B2 (en) * | 2015-05-15 | 2018-07-24 | Rohr Inc. | Variable area fan nozzle actuation system |
US20180128206A1 (en) * | 2016-11-09 | 2018-05-10 | General Electric Company | Gas turbine engine |
US11022071B2 (en) | 2016-12-21 | 2021-06-01 | The Boeing Company | Load distribution panel assembly, system and method |
US10767596B2 (en) | 2017-07-26 | 2020-09-08 | Raytheon Technologies Corporation | Nacelle |
US11046445B2 (en) | 2017-07-26 | 2021-06-29 | Raytheon Technologies Corporation | Nacelle |
US10794328B2 (en) | 2018-07-06 | 2020-10-06 | Rohr, Inc. | Thrust reverser with blocker door folding linkage |
EP3702603B1 (en) * | 2019-02-28 | 2023-12-13 | Airbus Operations GmbH | Thrust reverser assembly for an engine nacelle of an aircraft |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3465524A (en) * | 1966-03-02 | 1969-09-09 | Rolls Royce | Fan gas turbine engine |
US3477231A (en) * | 1967-12-26 | 1969-11-11 | Gen Electric | Noise reduction |
US3542152A (en) * | 1968-04-08 | 1970-11-24 | Gen Electric | Sound suppression panel |
GB1211923A (en) * | 1968-08-30 | 1970-11-11 | Rolls Royce | Thrust reverser for gas turbine jet propulsion engine |
GB1253071A (it) * | 1968-09-14 | 1971-11-10 | ||
US3481427A (en) * | 1968-11-29 | 1969-12-02 | Mc Donnell Douglas Corp | Acoustical panel structure |
US3600894A (en) * | 1970-04-28 | 1971-08-24 | Rohr Corp | Thrust reversing apparatus |
-
1973
- 1973-02-05 US US00329770A patent/US3831376A/en not_active Expired - Lifetime
- 1973-11-09 IT IT53598/73A patent/IT996422B/it active
Also Published As
Publication number | Publication date |
---|---|
US3831376A (en) | 1974-08-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IT996422B (it) | Invertitore di spinta per condotto di scarico di motore a getto | |
IT945731B (it) | Invertitore di spinta per turbo motore | |
IT938772B (it) | Motore a turbina a gas con ventola intubata per aeromobil | |
IT997686B (it) | Motore a turbina a gas | |
IT1031936B (it) | Struttura di cofano per motore a turboventilatore | |
NO143508C (no) | Ekshaustdyse for jetmotor. | |
IT1067171B (it) | Motore a turbina a gas con supporto perfezionato del condotto di transizione | |
IT1041149B (it) | Motore per generazione di potenza | |
IT1048656B (it) | Complesso integrato motore gondola di turbomotore a gas | |
IT1041998B (it) | Struttura di statore per un motore a turbina a gas | |
IT996837B (it) | Motore a getto provvisto di mezzi per attenuare il rumore | |
IT1022179B (it) | Ciclo per motore a turbina a gas | |
SE7513787L (sv) | Skiljevegg for raketmotorer | |
IT1020195B (it) | Motore a turbina per aerei a ciclo doppio | |
IT1029533B (it) | Dispositivo di scarico per motori mapini | |
IT1048186B (it) | Lama per un motore a turbina a gas | |
IT973079B (it) | Carcassa di turbina per un motore a turbina a gas | |
IT945912B (it) | Invertitori di spinta per motori a turbina a gas | |
IT1002931B (it) | Ugello estensibile per un motore a razzo o simile | |
IT1035761B (it) | Impianto di alimentazione di combustibili per motori dieseel | |
IT1203685B (it) | Invertitore di spinta senza sportelli per motore a getto | |
IT1016461B (it) | Turbo motore | |
IT971846B (it) | Motori a turbina a gas a ventola intubata | |
IT1007676B (it) | Motore a scoppio a spinta tangenziale | |
IT1031496B (it) | Cuscinetto per testa a croce di un motore a combustione i nternadiesel |