ES2060407T3 - Dispositivo de inversion de empuje para un propulsor propfan. - Google Patents
Dispositivo de inversion de empuje para un propulsor propfan.Info
- Publication number
- ES2060407T3 ES2060407T3 ES91918014T ES91918014T ES2060407T3 ES 2060407 T3 ES2060407 T3 ES 2060407T3 ES 91918014 T ES91918014 T ES 91918014T ES 91918014 T ES91918014 T ES 91918014T ES 2060407 T3 ES2060407 T3 ES 2060407T3
- Authority
- ES
- Spain
- Prior art keywords
- push
- investment
- wrap
- envelope
- investment device
- 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 - Lifetime
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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
- F02K1/66—Reversing fan flow using reversing fan blades
-
- 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
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)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
UN ACCIONAMIENTO PROPULSOR A HELICE CON ENVOLTURA (2) PARA UN AVION, PRESENTA PARA LA INVERSION DEL EMPUJE, PALETAS DE ROTOR REGULABLES (3) PARA INVERTIR LA DIRECCION DEL FLUJO EN EL INTERIOR DE LA ENVOLTURA Y UN ANILLO DE TOBERA (4) EN EL EXTREMO POSTERIOR DE LA ENVOLTURA, EL CUAL FAVORECE DURANTE LA INVERSION DE LA DIRECCION DEL CHORRO DEL FLUJO EL REFLUJO DEL FINAL DE LA ENVOLTURA. ESTA EJECUCION PRESENTA LA VENTAJA DE QUE LAS PALETAS DEL ROTOR DURANTE EL SERVICIO DE LA INVERSION DEL EMPUJE ESTAN SOMETIDAS A UNA TURBULENCIA MENOR Y CONSECUENTEMENTE GENERAN UN MAYOR EMPUJE DE INVERSION.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4039810A DE4039810C1 (es) | 1990-12-13 | 1990-12-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2060407T3 true ES2060407T3 (es) | 1994-11-16 |
Family
ID=6420234
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES91918014T Expired - Lifetime ES2060407T3 (es) | 1990-12-13 | 1991-10-29 | Dispositivo de inversion de empuje para un propulsor propfan. |
Country Status (7)
Country | Link |
---|---|
US (1) | US5343696A (es) |
EP (1) | EP0561791B1 (es) |
JP (1) | JPH06505781A (es) |
DE (2) | DE4039810C1 (es) |
ES (1) | ES2060407T3 (es) |
RU (1) | RU2094639C1 (es) |
WO (1) | WO1992010660A1 (es) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5516061A (en) * | 1994-09-19 | 1996-05-14 | Lockheed Corporation | Shroud for a reversible thrust fan |
FR2737256B1 (fr) * | 1995-07-26 | 1997-10-17 | Aerospatiale | Turboreacteur a double flux a portes d'inversion de poussee non soumises au flux secondaire dans leur position inactive |
US5730392A (en) * | 1995-09-22 | 1998-03-24 | Aeronautical Concept Of Exhaust, Ltd. | Adjustable fairing for thrust reversers |
FR2757901B1 (fr) * | 1996-12-26 | 1999-01-29 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a double flux a coquilles aval |
FR2766522B1 (fr) * | 1997-07-24 | 1999-09-03 | Hispano Suiza Sa | Inverseur de poussee de turbosoufflante a obstacle a guidage axial lies au capot primaire |
DE10041619A1 (de) | 2000-05-22 | 2001-11-29 | Bayer Ag | Selektive Herbizide auf Basis von Heteroaryloxyacetamiden |
US6669875B2 (en) * | 2000-12-18 | 2003-12-30 | 3M Innovative Properties Company | Method for making a dental mill blank assembly |
US6938408B2 (en) * | 2001-04-26 | 2005-09-06 | Propulsion Vectoring, L.P. | Thrust vectoring and variable exhaust area for jet engine nozzle |
DE10146591A1 (de) | 2001-09-21 | 2003-04-10 | Bayer Cropscience Ag | Herbizide auf Basis von substituierten Thien-3-yl-sulfonylamino(thio)carbonyl-triazolin(thi)onen |
DE102004010813A1 (de) | 2004-03-05 | 2005-11-10 | Bayer Cropscience Ag | Neue Herbizide auf Basis von substituierten Thien-3-yl-sulfonylamino(thio)carbonyltriazolin(thi)onen und 4-HPPD-Hemmstoffen |
US7665689B2 (en) * | 2006-11-24 | 2010-02-23 | The Boeing Company | Unconventional integrated propulsion systems and methods for blended wing body aircraft |
US7966828B2 (en) * | 2007-01-08 | 2011-06-28 | United Technologies Corporation | Variable area nozzle with woven sleeve extension |
US8959889B2 (en) | 2008-11-26 | 2015-02-24 | The Boeing Company | Method of varying a fan duct nozzle throat area of a gas turbine engine |
US8127532B2 (en) | 2008-11-26 | 2012-03-06 | The Boeing Company | Pivoting fan nozzle nacelle |
FR2958910B1 (fr) * | 2010-04-20 | 2012-04-27 | Aircelle Sa | Nacelle pour moteur d'aeronef a tuyere de section variable |
US10400629B2 (en) | 2012-01-31 | 2019-09-03 | United Technologies Corporation | Gas turbine engine shaft bearing configuration |
US8402741B1 (en) | 2012-01-31 | 2013-03-26 | United Technologies Corporation | Gas turbine engine shaft bearing configuration |
US8863491B2 (en) | 2012-01-31 | 2014-10-21 | United Technologies Corporation | Gas turbine engine shaft bearing configuration |
US10113508B2 (en) | 2014-11-21 | 2018-10-30 | General Electric Company | Gas turbine engine and method of assembling the same |
US10465538B2 (en) * | 2014-11-21 | 2019-11-05 | General Electric Company | Gas turbine engine with reversible fan |
US10502160B2 (en) | 2016-02-09 | 2019-12-10 | General Electric Company | Reverse thrust engine |
JP6299792B2 (ja) * | 2016-03-24 | 2018-03-28 | トヨタ自動車株式会社 | 移動体の姿勢制御のための空気噴出式推力発生装置 |
FR3052191B1 (fr) * | 2016-06-01 | 2019-07-12 | Safran Aircraft Engines | Inversion de poussee dans une turbomachine avec soufflante a calage variable |
PL417832A1 (pl) * | 2016-07-04 | 2018-01-15 | General Electric Company | Zespół rozszerzenia kielichowego, zwłaszcza do dyszy i sposób jego rozkładania oraz silnik turbowentylatorowy zawierający ten zespół |
US11053888B2 (en) * | 2017-11-01 | 2021-07-06 | The Boeing Company | Fan cowl with a serrated trailing edge providing attached flow in reverse thrust mode |
PL235797B1 (pl) * | 2018-02-21 | 2020-10-19 | Gen Electric | Zespół dyszy dzwonowej do silników turbogazowych oraz sposób odwracania ciągu silnika turbowentylatorowego |
FR3082186B1 (fr) * | 2018-06-07 | 2021-02-12 | Safran | Ensemble de propulsion pour un aeronef a decollage et atterrissage verticaux |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2570629A (en) * | 1945-10-05 | 1951-10-09 | Anxionnaz | Adjustable pipe for the intake of air and expansion of the driving gases in reactionjet propellers for projectiles and vehicles |
GB861819A (en) * | 1957-07-29 | 1961-03-01 | Boeing Co | Noise suppressor and thrust reverser for jet propulsion engines |
DE2446548A1 (de) * | 1973-10-11 | 1975-04-17 | United Aircraft Corp | Triebwerk mit ummanteltem geblaese |
GB1565212A (en) * | 1975-12-22 | 1980-04-16 | British Hovercraft Corp Ltd | Ductecd fan propulsors |
GB2070691B (en) * | 1980-01-11 | 1983-08-24 | Rolls Royce | Radial splitter for reversible pitch fan propulsion unit |
US4802629A (en) * | 1982-10-22 | 1989-02-07 | The Boeing Company | Plug-type exhaust nozzle having a variable centerbody and translating shroud |
-
1990
- 1990-12-13 DE DE4039810A patent/DE4039810C1/de not_active Expired - Lifetime
-
1991
- 1991-10-29 WO PCT/EP1991/002040 patent/WO1992010660A1/de active IP Right Grant
- 1991-10-29 ES ES91918014T patent/ES2060407T3/es not_active Expired - Lifetime
- 1991-10-29 JP JP3517057A patent/JPH06505781A/ja active Pending
- 1991-10-29 US US08/075,510 patent/US5343696A/en not_active Expired - Fee Related
- 1991-10-29 RU RU9193032370A patent/RU2094639C1/ru active
- 1991-10-29 EP EP91918014A patent/EP0561791B1/de not_active Expired - Lifetime
- 1991-10-29 DE DE59102584T patent/DE59102584D1/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0561791A1 (en) | 1993-09-29 |
EP0561791B1 (de) | 1994-08-17 |
JPH06505781A (ja) | 1994-06-30 |
WO1992010660A1 (de) | 1992-06-25 |
US5343696A (en) | 1994-09-06 |
DE4039810C1 (es) | 1991-10-17 |
DE59102584D1 (de) | 1994-09-22 |
RU2094639C1 (ru) | 1997-10-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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