CH324501A - Gasturbinen-Strahltriebwerk - Google Patents

Gasturbinen-Strahltriebwerk

Info

Publication number
CH324501A
CH324501A CH324501DA CH324501A CH 324501 A CH324501 A CH 324501A CH 324501D A CH324501D A CH 324501DA CH 324501 A CH324501 A CH 324501A
Authority
CH
Switzerland
Prior art keywords
gas turbine
jet engine
turbine jet
engine
gas
Prior art date
Application number
Other languages
German (de)
English (en)
Inventor
Henry Kerry Thomas
Robert Robinson Norman
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH324501A publication Critical patent/CH324501A/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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
    • 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
    • F02K1/123—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
CH324501D 1953-02-16 1954-02-16 Gasturbinen-Strahltriebwerk CH324501A (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB324501X 1953-02-16
GB110254X 1954-02-11

Publications (1)

Publication Number Publication Date
CH324501A true CH324501A (de) 1957-09-30

Family

ID=26247958

Family Applications (1)

Application Number Title Priority Date Filing Date
CH324501D CH324501A (de) 1953-02-16 1954-02-16 Gasturbinen-Strahltriebwerk

Country Status (4)

Country Link
BE (1) BE526525A (instruction)
CH (1) CH324501A (instruction)
FR (1) FR1097287A (instruction)
GB (1) GB750307A (instruction)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1164754B (de) * 1952-08-15 1964-03-05 United Aircraft Corp Schubduese fuer ein Flugzeugstrahltriebwerk

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3049875A (en) * 1952-08-15 1962-08-21 United Aircraft Corp Variable flap plug type nozzle
US2930186A (en) * 1954-11-26 1960-03-29 Ashwood Peter Frederick Discharge nozzles for propulsive jets
US2982089A (en) * 1955-06-24 1961-05-02 Gen Motors Corp Afterburner nozzle
US3032974A (en) * 1956-08-24 1962-05-08 United Aircraft Corp Exhaust nozzle
US3004385A (en) * 1958-06-25 1961-10-17 Gen Motors Corp Variable convergent-divergent jet nozzle
US3038304A (en) * 1959-04-17 1962-06-12 Gen Electric Variable exhaust nozzle configuration
GB951130A (en) * 1961-07-28 1964-03-04 Rolls Royce Improvements relating to jet engines
GB1127826A (en) * 1966-06-17 1968-09-18 Rolls Royce Gas turbine engine
FR2732408A1 (fr) * 1983-03-16 1996-10-04 Snecma Tuyere, en particulier pour turboreacteur
US6318070B1 (en) 2000-03-03 2001-11-20 United Technologies Corporation Variable area nozzle for gas turbine engines driven by shape memory alloy actuators
US6543224B1 (en) * 2002-01-29 2003-04-08 United Technologies Corporation System and method for controlling shape memory alloy actuators
US7546727B2 (en) 2004-11-12 2009-06-16 The Boeing Company Reduced noise jet engine
US7340883B2 (en) 2004-11-12 2008-03-11 The Boeing Company Morphing structure
US7216831B2 (en) 2004-11-12 2007-05-15 The Boeing Company Shape changing structure
WO2008045062A1 (en) 2006-10-12 2008-04-17 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system
WO2014200403A1 (en) * 2013-06-14 2014-12-18 Saab Ab Variable-geometry exhaust nozzle for a jet engine and a method for varying the nozzle
FR3051228B1 (fr) * 2016-05-12 2020-02-14 Herakles Rigidification de la liaison entre volets dans une tuyere a section variable
CN110159454B (zh) * 2019-06-17 2023-11-24 西安航空学院 固冲发动机可调喷管

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1164754B (de) * 1952-08-15 1964-03-05 United Aircraft Corp Schubduese fuer ein Flugzeugstrahltriebwerk

Also Published As

Publication number Publication date
GB750307A (en) 1956-06-13
BE526525A (instruction)
FR1097287A (fr) 1955-07-04

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