FR1463420A - Réacteur comportant une buse d'éjection perfectionnée - Google Patents

Réacteur comportant une buse d'éjection perfectionnée

Info

Publication number
FR1463420A
FR1463420A FR45498A FR45498A FR1463420A FR 1463420 A FR1463420 A FR 1463420A FR 45498 A FR45498 A FR 45498A FR 45498 A FR45498 A FR 45498A FR 1463420 A FR1463420 A FR 1463420A
Authority
FR
France
Prior art keywords
reactor
ejection nozzle
improved ejection
improved
nozzle
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
Application number
FR45498A
Other languages
English (en)
Inventor
John Anthony Jones Rees
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1463420A publication Critical patent/FR1463420A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Supercharger (AREA)
FR45498A 1965-01-11 1966-01-11 Réacteur comportant une buse d'éjection perfectionnée Expired FR1463420A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1258/65A GB1060051A (en) 1965-01-11 1965-01-11 Improvements in or relating to gas turbine engines

Publications (1)

Publication Number Publication Date
FR1463420A true FR1463420A (fr) 1966-12-23

Family

ID=9718854

Family Applications (1)

Application Number Title Priority Date Filing Date
FR45498A Expired FR1463420A (fr) 1965-01-11 1966-01-11 Réacteur comportant une buse d'éjection perfectionnée

Country Status (4)

Country Link
US (1) US3348380A (fr)
DE (1) DE1290434B (fr)
FR (1) FR1463420A (fr)
GB (1) GB1060051A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016108021A1 (fr) 2014-12-30 2016-07-07 Aledia Dispositif optoélectronique a diodes électroluminescentes

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3380661A (en) * 1966-04-12 1968-04-30 United Aircraft Corp Thrust deflector
US3986687A (en) * 1975-06-30 1976-10-19 General Electric Company Aircraft propulsion system with flight maneuverable exhaust nozzle
DE2540537C2 (de) * 1975-09-11 1977-11-10 Motoren- und Turbinen-Union München GmbH, 8000 München Gasturbinenstrahltriebwerk zum Antrieb und zur Steuerung eines Flugzeugs
US5076512A (en) * 1989-02-08 1991-12-31 Boeing Canada Ltd. Ventral segmented nozzles for promoting rapid temperature and pressure decay
US5062588A (en) * 1989-02-08 1991-11-05 Boeing Of Canada Ltd. Segmented rotatable nozzles
US6477829B1 (en) * 2000-05-09 2002-11-12 Lockheed Martin Corporation Combined cycle pulse combustion/gas turbine engine
US7493914B2 (en) * 2005-07-20 2009-02-24 Welker, Inc. Newtonian thrust cowl array

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
US2944393A (en) * 1955-04-15 1960-07-12 Phillips Petroleum Co Aerodynamic braking of jet engine aircraft
US2857119A (en) * 1956-03-21 1958-10-21 Morguloff Daniel Jet steering and braking system for aircraft
DE1064817B (de) * 1958-02-14 1959-09-03 Daimler Benz Ag Strahltriebwerk, insbesondere fuer Luftfahrzeuge, mit Nachverbrennung und Strahlumlenkung
DE1085767B (de) * 1958-12-15 1960-07-21 Bmw Triebwerkbau Ges M B H Fluggeraet mit Strahltriebwerk und Nachbrennkammer
IT649857A (fr) * 1960-05-06

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016108021A1 (fr) 2014-12-30 2016-07-07 Aledia Dispositif optoélectronique a diodes électroluminescentes

Also Published As

Publication number Publication date
GB1060051A (en) 1967-02-22
DE1290434B (de) 1969-03-06
US3348380A (en) 1967-10-24

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