RU2094639C1 - Силовая установка с воздушным винтом или пропеллером (варианты) - Google Patents

Силовая установка с воздушным винтом или пропеллером (варианты) Download PDF

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Publication number
RU2094639C1
RU2094639C1 RU9193032370A RU93032370A RU2094639C1 RU 2094639 C1 RU2094639 C1 RU 2094639C1 RU 9193032370 A RU9193032370 A RU 9193032370A RU 93032370 A RU93032370 A RU 93032370A RU 2094639 C1 RU2094639 C1 RU 2094639C1
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RU
Russia
Prior art keywords
propeller
shell
annular
rear tail
annular nozzle
Prior art date
Application number
RU9193032370A
Other languages
English (en)
Russian (ru)
Other versions
RU93032370A (ru
Inventor
Рора Алоис
Траксдорф Петер
Original Assignee
Мту Моторен-Унд Турбинен-Унион Мюнхен Гмбх
Priority date (The priority date 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 date listed.)
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Publication date
Application filed by Мту Моторен-Унд Турбинен-Унион Мюнхен Гмбх filed Critical Мту Моторен-Унд Турбинен-Унион Мюнхен Гмбх
Publication of RU93032370A publication Critical patent/RU93032370A/ru
Application granted granted Critical
Publication of RU2094639C1 publication Critical patent/RU2094639C1/ru

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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)
RU9193032370A 1990-12-13 1991-10-29 Силовая установка с воздушным винтом или пропеллером (варианты) RU2094639C1 (ru)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DEP4039810.2 1990-12-13
DE4039810.2 1990-12-13
DE4039810A DE4039810C1 (enExample) 1990-12-13 1990-12-13
PCT/EP1991/002040 WO1992010660A1 (de) 1990-12-13 1991-10-29 Schubumkehrvorrichtung für ein propfantriebwerk

Publications (2)

Publication Number Publication Date
RU93032370A RU93032370A (ru) 1997-01-27
RU2094639C1 true RU2094639C1 (ru) 1997-10-27

Family

ID=6420234

Family Applications (1)

Application Number Title Priority Date Filing Date
RU9193032370A RU2094639C1 (ru) 1990-12-13 1991-10-29 Силовая установка с воздушным винтом или пропеллером (варианты)

Country Status (7)

Country Link
US (1) US5343696A (enExample)
EP (1) EP0561791B1 (enExample)
JP (1) JPH06505781A (enExample)
DE (2) DE4039810C1 (enExample)
ES (1) ES2060407T3 (enExample)
RU (1) RU2094639C1 (enExample)
WO (1) WO1992010660A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2553833C2 (ru) * 2010-04-20 2015-06-20 Эрсель Гондола для двигателя летательного аппарата с соплом переменного поперечного сечения

Families Citing this family (27)

* Cited by examiner, † Cited by third party
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
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
US10400629B2 (en) 2012-01-31 2019-09-03 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
US20240401546A1 (en) * 2023-06-01 2024-12-05 General Electric Company Turbine engine having a thrust reverser system

Family Cites Families (6)

* Cited by examiner, † Cited by third party
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

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
GB, патент, 1565212, кл.F 02K 11/00, 1960. *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2553833C2 (ru) * 2010-04-20 2015-06-20 Эрсель Гондола для двигателя летательного аппарата с соплом переменного поперечного сечения

Also Published As

Publication number Publication date
ES2060407T3 (es) 1994-11-16
US5343696A (en) 1994-09-06
EP0561791B1 (de) 1994-08-17
DE4039810C1 (enExample) 1991-10-17
EP0561791A1 (en) 1993-09-29
DE59102584D1 (de) 1994-09-22
JPH06505781A (ja) 1994-06-30
WO1992010660A1 (de) 1992-06-25

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