FR998659A - Turbojet overload accessories control device - Google Patents

Turbojet overload accessories control device

Info

Publication number
FR998659A
FR998659A FR998659DA FR998659A FR 998659 A FR998659 A FR 998659A FR 998659D A FR998659D A FR 998659DA FR 998659 A FR998659 A FR 998659A
Authority
FR
France
Prior art keywords
turbojet
overload
control device
accessories control
accessories
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
Other languages
French (fr)
Inventor
Rene Anxionnaz
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.)
Rateau SA
Original Assignee
Rateau SA
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 Rateau SA filed Critical Rateau SA
Application granted granted Critical
Publication of FR998659A publication Critical patent/FR998659A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
FR998659D 1949-09-30 1949-09-30 Turbojet overload accessories control device Expired FR998659A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR998659T 1949-09-30

Publications (1)

Publication Number Publication Date
FR998659A true FR998659A (en) 1952-01-22

Family

ID=9559510

Family Applications (1)

Application Number Title Priority Date Filing Date
FR998659D Expired FR998659A (en) 1949-09-30 1949-09-30 Turbojet overload accessories control device

Country Status (1)

Country Link
FR (1) FR998659A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1043722B (en) * 1954-01-16 1958-11-13 Oskar August Schaetzle Dipl In Three-shaft jet engine with rigid transmission links
DE1131467B (en) * 1959-04-30 1962-06-14 Daimler Benz Ag Compound engine for propulsion of aircraft
DE1247073B (en) * 1961-09-12 1967-08-10 Bristol Siddeley Engines Ltd Method and device for cooling a supersonic gas turbine jet engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1043722B (en) * 1954-01-16 1958-11-13 Oskar August Schaetzle Dipl In Three-shaft jet engine with rigid transmission links
DE1131467B (en) * 1959-04-30 1962-06-14 Daimler Benz Ag Compound engine for propulsion of aircraft
DE1247073B (en) * 1961-09-12 1967-08-10 Bristol Siddeley Engines Ltd Method and device for cooling a supersonic gas turbine jet engine

Similar Documents

Publication Publication Date Title
FR1023003A (en) Hydraulic control device
FR946867A (en) Control device
FR998659A (en) Turbojet overload accessories control device
FR1015720A (en) Quick-acting control device
FR60237E (en) Sprayer device
FR986867A (en) Advanced rewinder device
FR993087A (en) Weighing device
FR1012114A (en) Chassis control device
FR975507A (en) Advanced device for controlling electrical circuits
FR1024836A (en) Lock control device
FR981161A (en) Cycle control device
FR1022898A (en) Advanced control device
FR986185A (en) Weed control device for hooks
FR1004154A (en) Control device
FR1047884A (en) Control device for generator set
FR1003908A (en) Combined mechanism control
FR967552A (en) Navigation control device
FR1012454A (en) Toy control device
FR984229A (en) Electric meter control device
CH286250A (en) Circuit breaker control device.
FR1015687A (en) Aircraft in-flight control device
FR1003637A (en) Reversible lever control device
FR1028271A (en) Hopper trap control device
FR1023231A (en) Advanced dye box control device
FR1017398A (en) Contactor-circuit breaker control device