CH419851A - Schubablenk- und Umkehrvorrichtung - Google Patents

Schubablenk- und Umkehrvorrichtung

Info

Publication number
CH419851A
CH419851A CH1159464A CH1159464A CH419851A CH 419851 A CH419851 A CH 419851A CH 1159464 A CH1159464 A CH 1159464A CH 1159464 A CH1159464 A CH 1159464A CH 419851 A CH419851 A CH 419851A
Authority
CH
Switzerland
Prior art keywords
reversing device
thrust deflector
deflector
thrust
reversing
Prior art date
Application number
CH1159464A
Other languages
English (en)
Inventor
Richard Erwin John
Original Assignee
Gen Electric
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.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Publication of CH419851A publication Critical patent/CH419851A/de

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
    • F02K1/56—Reversing jet main flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
CH1159464A 1963-09-18 1964-09-04 Schubablenk- und Umkehrvorrichtung CH419851A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US309657A US3241771A (en) 1963-09-18 1963-09-18 Thrust deflector and reverser

Publications (1)

Publication Number Publication Date
CH419851A true CH419851A (de) 1966-08-31

Family

ID=23199111

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1159464A CH419851A (de) 1963-09-18 1964-09-04 Schubablenk- und Umkehrvorrichtung

Country Status (6)

Country Link
US (1) US3241771A (de)
BE (1) BE653265A (de)
CH (1) CH419851A (de)
DE (1) DE1260319B (de)
GB (1) GB1014208A (de)
NL (1) NL6410679A (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2757570A1 (fr) * 1996-12-19 1998-06-26 Hispano Suiza Sa Inverseur de poussee de turboreacteur a guidage du flux d'inversion ameliore

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3299638A (en) * 1965-03-12 1967-01-24 Ltv Aerospace Corp Variable flow deflection means
GB1132423A (en) * 1967-05-24 1968-10-30 Rolls Royce Aircraft power plant comprising a vertical lift jet engine
US3493195A (en) * 1967-12-22 1970-02-03 Frank O Nelson Propulsion unit for aircraft and other vehicles
US3614030A (en) * 1969-12-10 1971-10-19 Paul S Moller Aircraft
BE756228R (de) * 1970-03-02 1971-03-01 Gen Electric
US3940092A (en) * 1974-11-07 1976-02-24 The Boeing Company Jet flow deflector for aircraft
US6648268B2 (en) * 2002-02-13 2003-11-18 Dupont Anthony A. Control system for vertical take off and land (VTOL) aircraft
DE10237341A1 (de) * 2002-08-14 2004-02-26 Siemens Ag Modell, Berechnung und Anwendung periodisch erzeugter Kantenwirbel im Turbomaschinenbau
EP2074311B1 (de) * 2006-10-12 2013-09-11 United Technologies Corporation Gondelanordnung für ein Gasturbinentriebwerk mit hohem Nebenstromverhältnis, zugehöriges Gasturbinentriebwerk mit hohem Nebenstromverhältnis und Verfahren zur Querschnittsverstellung der Austrittsdüse eines Gebläses
FR2922958B1 (fr) * 2007-10-25 2009-11-20 Aircelle Sa Inverseur de poussee a grilles
GB2567199A (en) * 2017-10-05 2019-04-10 Autonomous Devices Ltd Control system for fluid borne vehicles
CN110496713B (zh) * 2019-09-20 2024-06-18 常熟华东汽车有限公司 除雪车用的矢量喷口结构
CN112443423B (zh) * 2020-11-24 2022-04-05 南京航空航天大学 一种气驱动涵道风扇喷气推进动力系统

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE21627C (de) * TH. J. B. JANSEN in Bonn Neuerungen an Regulir-Füllöfen
US2681548A (en) * 1948-10-27 1954-06-22 Peter G Kappus Reversible thrust nozzle for jet engines
BE523637A (de) * 1952-10-21
US2932164A (en) * 1955-08-03 1960-04-12 Lockheed Aircraft Corp Thrust reverser and control mechanism therefor
US2929580A (en) * 1956-06-18 1960-03-22 Piasecki Aircraft Corp Aircraft for vertical or short takeoff, and integrated propulsion lifting and propeller slip stream deflecting unit therefor
US2879014A (en) * 1957-07-02 1959-03-24 Bell Aircraft Corp Jet propelled airplane with jet diverter
DE1057881B (de) * 1957-08-23 1959-05-21 Entwicklungsbau Pirna Veb Einrichtung zum Umlenken eines mit grosser Energie stroemenden Gasstrahles, insbesondere des Schubstrahles eines Rueckstossantriebes fuer Fahrzeuge
US3016700A (en) * 1958-07-07 1962-01-16 Curtiss Wright Corp Thrust reverser for jet engines
US3028121A (en) * 1959-11-27 1962-04-03 Gen Electric Thrust augmenting means for aircraft
US3035792A (en) * 1959-12-28 1962-05-22 Gen Electric Thrust augmenting powerplant for aircraft
US3087303A (en) * 1960-03-29 1963-04-30 Northrop Corp Jet propelled aircraft with jet deflecting means
GB913312A (en) * 1960-05-06 1962-12-19 Rolls Royce Jet propulsion engine
US3096954A (en) * 1960-11-10 1963-07-09 Snecma Improvements to jet-propelled aircraft with directional discharge-nozzles for vertical take-off
FR1304033A (fr) * 1961-06-14 1962-09-21 Northrop Corp Aéronef à propulsion par réaction comportant un dispositif de déflexion des gaz d'échappement
US3040524A (en) * 1961-07-28 1962-06-26 United Aircraft Corp Ducted fan engine thrust reverser
GB922645A (en) * 1961-11-07 1963-04-03 Rolls Royce Jet propulsion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2757570A1 (fr) * 1996-12-19 1998-06-26 Hispano Suiza Sa Inverseur de poussee de turboreacteur a guidage du flux d'inversion ameliore

Also Published As

Publication number Publication date
DE1260319B (de) 1968-02-01
BE653265A (de) 1965-01-18
US3241771A (en) 1966-03-22
GB1014208A (en) 1965-12-22
NL6410679A (de) 1965-03-19

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