IT945912B - Invertitori di spinta per motori a turbina a gas - Google Patents
Invertitori di spinta per motori a turbina a gasInfo
- Publication number
- IT945912B IT945912B IT24183/71A IT2418371A IT945912B IT 945912 B IT945912 B IT 945912B IT 24183/71 A IT24183/71 A IT 24183/71A IT 2418371 A IT2418371 A IT 2418371A IT 945912 B IT945912 B IT 945912B
- Authority
- IT
- Italy
- Prior art keywords
- gas turbine
- turbine engines
- thrust inverters
- inverters
- thrust
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 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
-
- 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
- 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
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 |
---|---|---|---|
GB2181070 | 1970-05-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
IT945912B true IT945912B (it) | 1973-05-10 |
Family
ID=10169203
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT24183/71A IT945912B (it) | 1970-05-06 | 1971-05-06 | Invertitori di spinta per motori a turbina a gas |
Country Status (4)
Country | Link |
---|---|
US (1) | US3717304A (it) |
DE (1) | DE2122005A1 (it) |
FR (1) | FR2088393A1 (it) |
IT (1) | IT945912B (it) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1506588A (en) * | 1975-10-11 | 1978-04-05 | Rolls Royce | Gas turbine engine power plants for aircraft |
FR2559838B1 (fr) * | 1984-02-21 | 1988-05-13 | Hurel Dubois Avions | Procede et dispositif permettant le controle du jet inverse dans les moteurs a reaction a inverseur de poussee |
US6568172B2 (en) * | 2001-09-27 | 2003-05-27 | The Nordam Group, Inc. | Converging nozzle thrust reverser |
FR2922958B1 (fr) * | 2007-10-25 | 2009-11-20 | Aircelle Sa | Inverseur de poussee a grilles |
FR2956162B1 (fr) * | 2010-02-08 | 2012-11-16 | Snecma | Tuyere de flux froid d'un turboreacteur a double flux a flux separes incorporant un inverseur de poussee a grilles |
FR2983173B1 (fr) * | 2011-11-24 | 2014-02-28 | Aircelle Sa | Actionneur pour nacelle de turboreacteur d'aeronef a partie arriere notamment annulaire monobloc |
US10145335B2 (en) * | 2012-09-28 | 2018-12-04 | United Technologies Corporation | Turbomachine thrust reverser |
DE102015203219A1 (de) * | 2015-02-23 | 2016-08-25 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerksverkleidung einer Gasturbine mit Schubumkehrvorrichtung und im Querschnitt verstellbarer Ausströmdüse |
DE102015206093A1 (de) * | 2015-04-02 | 2016-10-06 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerksverkleidung einer Fluggasturbine |
US10648426B2 (en) | 2016-01-14 | 2020-05-12 | Honeywell International Inc. | Single row vane assembly for a thrust reverser |
US10337454B2 (en) * | 2016-01-25 | 2019-07-02 | Honeywell International Inc. | Thrust reverser with asymmetric vane geometry |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3262268A (en) * | 1965-06-07 | 1966-07-26 | Gen Electric | Thrust reverser |
US3262269A (en) * | 1965-06-07 | 1966-07-26 | Gen Electric | Thrust reverser |
US3262271A (en) * | 1965-07-30 | 1966-07-26 | Gen Electric | Thrust reverser |
-
1971
- 1971-05-03 US US00139693A patent/US3717304A/en not_active Expired - Lifetime
- 1971-05-04 DE DE19712122005 patent/DE2122005A1/de active Pending
- 1971-05-06 IT IT24183/71A patent/IT945912B/it active
- 1971-05-06 FR FR7116395A patent/FR2088393A1/fr active Pending
Also Published As
Publication number | Publication date |
---|---|
DE2122005A1 (de) | 1972-02-17 |
FR2088393A1 (it) | 1972-01-07 |
US3717304A (en) | 1973-02-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CH541716A (de) | Gasturbinentriebwerk | |
IT998522B (it) | Apparato di combustione per motori a turbina a gas | |
CA939522A (en) | Gas turbine engine | |
CA938797A (en) | Wall structure for a gas turbine engine | |
IT1002233B (it) | Assieme di turbomotore a gas con turbina di potenza | |
CH538048A (de) | Axial-Gasturbine | |
IT997686B (it) | Motore a turbina a gas | |
IT945731B (it) | Invertitore di spinta per turbo motore | |
IT938772B (it) | Motore a turbina a gas con ventola intubata per aeromobil | |
CA938796A (en) | Gas turbine engine | |
IT962232B (it) | Paletta per l impiego in motori a turbina a gas | |
IT975686B (it) | Rotore di turbina per turbine a gas particolarmente per autoveicoli | |
IT940595B (it) | Schermo para fiamma per motore a turbina a gas | |
AU447212B2 (en) | Gas turbine engines | |
CA933369A (en) | Gas turbine engine | |
IT962211B (it) | Rotore per turbine a gas | |
IT945912B (it) | Invertitori di spinta per motori a turbina a gas | |
IT942542B (it) | Girante palettata per motori a turbina a gas | |
AT307821B (de) | Gasturbine | |
IT940430B (it) | Supporti per motori di aeromobili | |
IT940943B (it) | Perfezionamento nelle turbine a gas particolarmente per aeromobili | |
IT948555B (it) | Impianto alimentatore di combusti bile per motori a turbina a gas | |
IT961721B (it) | Pompa di combustibile per motori a turbina a gas | |
IT941175B (it) | Impianto di regolazione per turbine a gas | |
IT948358B (it) | Regolatore di carburante parti colarmente per motori a turbina |