CH269899A - Procedure for the regulation of turbo jet engines and device for the execution of the procedure. - Google Patents

Procedure for the regulation of turbo jet engines and device for the execution of the procedure.

Info

Publication number
CH269899A
CH269899A CH269899DA CH269899A CH 269899 A CH269899 A CH 269899A CH 269899D A CH269899D A CH 269899DA CH 269899 A CH269899 A CH 269899A
Authority
CH
Switzerland
Prior art keywords
procedure
regulation
execution
jet engines
turbo jet
Prior art date
Application number
Other languages
German (de)
Inventor
Cie Aktiengesellschaft Boveri
Original Assignee
Bbc Brown Boveri & Cie
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 Bbc Brown Boveri & Cie filed Critical Bbc Brown Boveri & Cie
Publication of CH269899A publication Critical patent/CH269899A/en

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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/30—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
CH269899D 1954-11-25 1948-10-21 Procedure for the regulation of turbo jet engines and device for the execution of the procedure. CH269899A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1140440X 1954-11-25

Publications (1)

Publication Number Publication Date
CH269899A true CH269899A (en) 1950-07-31

Family

ID=10877151

Family Applications (1)

Application Number Title Priority Date Filing Date
CH269899D CH269899A (en) 1954-11-25 1948-10-21 Procedure for the regulation of turbo jet engines and device for the execution of the procedure.

Country Status (3)

Country Link
CH (1) CH269899A (en)
FR (2) FR1006139A (en)
GB (2) GB654344A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1085720B (en) * 1954-04-27 1960-07-21 Napier & Son Ltd Jet engine
DE1139702B (en) * 1958-10-08 1962-11-15 Snecma Device for adapting a convergent-divergent nozzle to variable relaxation conditions

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1073242B (en) * 1960-01-14 Power Jets (Research &. Develop ment) Limited London Jet propulsion nozzle
US2957306A (en) * 1955-06-16 1960-10-25 John S Attinello Gas jets for controlling entrance and/or exit flow effective diameter
US2994193A (en) * 1956-06-14 1961-08-01 Gen Motors Corp Jet thrust reversing means for jet engines
US3109284A (en) * 1956-06-14 1963-11-05 Power Jets Res & Dev Ltd Discharge nozzles for propulsive jets
GB820059A (en) * 1956-07-30 1959-09-16 Bristol Aero Engines Ltd Improvements in or relating to jet propulsion nozzles
US2986002A (en) * 1957-06-05 1961-05-30 Curtiss Wright Corp Leaky-type exhaust nozzle for jet propulsion devices
US3098387A (en) * 1957-08-19 1963-07-23 Thompson Ramo Wooldridge Inc Turbine
FR1182810A (en) * 1957-09-16 1959-06-30 Snecma Improvements to adjustable section ejection nozzles
US2971327A (en) * 1957-11-26 1961-02-14 Westinghouse Electric Corp Discharge control of an overexpanding propulsion nozzle
US3049873A (en) * 1958-02-04 1962-08-21 Westinghouse Electric Corp Exhaust nozzle having a flow area of variable convergency and divergency
US3010280A (en) * 1958-03-25 1961-11-28 United Aircraft Corp Variable-expansion nozzle
US3032977A (en) * 1958-06-05 1962-05-08 Gen Electric Correlated bypass inlet and outlet control for a supersonic reaction powerplant
US3041825A (en) * 1958-11-18 1962-07-03 Gen Electric Flow stabilizing means for converging-diverging nozzle
US3044258A (en) * 1958-11-25 1962-07-17 Gen Electric Adjustable converging-diverging nozzle
US2959917A (en) * 1959-04-06 1960-11-15 Boeing Co Sound suppressor for jet engines
US2957310A (en) * 1959-05-11 1960-10-25 Orenda Engines Ltd Convergent-divergent nozzle assembly
US3095696A (en) * 1959-09-25 1963-07-02 Roy W Rumble Combustion-engine exhaust systems
US3048973A (en) * 1959-10-29 1962-08-14 Marcus C Benedict Exhaust nozzle
NL262125A (en) * 1960-04-01
DE1230620B (en) * 1963-01-09 1966-12-15 Rolls Royce Vertical lift engine system for aircraft
US4018384A (en) * 1976-02-13 1977-04-19 Chandler Evans Inc. Flow attachment device for thrust vector control
US5683033A (en) * 1989-02-08 1997-11-04 United Technologies Corporation Rocket nozzle for a rocket engine
US5619851A (en) * 1989-02-08 1997-04-15 United Technologies Corporation Rocket nozzle for a rocket engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1085720B (en) * 1954-04-27 1960-07-21 Napier & Son Ltd Jet engine
DE1139702B (en) * 1958-10-08 1962-11-15 Snecma Device for adapting a convergent-divergent nozzle to variable relaxation conditions

Also Published As

Publication number Publication date
FR1006139A (en) 1952-04-21
GB654344A (en) 1951-06-13
GB788316A (en) 1957-12-23
FR1140440A (en) 1957-07-22

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