FR1382214A - Post-combustion charge limiter - Google Patents

Post-combustion charge limiter

Info

Publication number
FR1382214A
FR1382214A FR951560A FR951560A FR1382214A FR 1382214 A FR1382214 A FR 1382214A FR 951560 A FR951560 A FR 951560A FR 951560 A FR951560 A FR 951560A FR 1382214 A FR1382214 A FR 1382214A
Authority
FR
France
Prior art keywords
post
combustion charge
charge limiter
limiter
combustion
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
FR951560A
Other languages
French (fr)
Inventor
Jacques Aubert
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR951560A priority Critical patent/FR1382214A/en
Priority to GB4305964A priority patent/GB1084957A/en
Priority to DE1964S0093840 priority patent/DE1289680B/en
Application granted granted Critical
Publication of FR1382214A publication Critical patent/FR1382214A/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
    • 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
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control
    • 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
    • F02K1/15—Control or regulation
    • 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
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control
    • F02K1/17—Control or regulation conjointly with another control with control of fuel supply

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
FR951560A 1963-10-23 1963-10-23 Post-combustion charge limiter Expired FR1382214A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR951560A FR1382214A (en) 1963-10-23 1963-10-23 Post-combustion charge limiter
GB4305964A GB1084957A (en) 1963-10-23 1964-10-22 Improvements in or relating to turbojets with afterburner and variable area nozzle means
DE1964S0093840 DE1289680B (en) 1963-10-23 1964-10-22 Gas turbine jet engine with afterburner and adjustable thrust nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR951560A FR1382214A (en) 1963-10-23 1963-10-23 Post-combustion charge limiter

Publications (1)

Publication Number Publication Date
FR1382214A true FR1382214A (en) 1964-12-18

Family

ID=8815024

Family Applications (1)

Application Number Title Priority Date Filing Date
FR951560A Expired FR1382214A (en) 1963-10-23 1963-10-23 Post-combustion charge limiter

Country Status (3)

Country Link
DE (1) DE1289680B (en)
FR (1) FR1382214A (en)
GB (1) GB1084957A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1301933B (en) * 1965-03-10 1969-08-28 Snecma Afterburn control device for gas turbine jet engines with adjustable thrust nozzle
US4467600A (en) * 1979-07-31 1984-08-28 Messerschmitt-Boelkow-Blohm Gmbh System for controlling the thrust nozzle adjustment of dual cycle gas turbine jet propulsion engines

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2834339B1 (en) * 2001-12-31 2004-02-27 Bosch Gmbh Robert PNEUMATIC CYLINDER FOR THE TESTING OF A SERVOMOTOR

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969640A (en) * 1953-08-25 1961-01-31 Solar Aircraft Co Pressure ratio sensing, indicating, and controlling apparatus
US2944387A (en) * 1954-09-24 1960-07-12 Curtiss Wright Corp Jet engine speed and nozzle controls
GB826125A (en) * 1955-04-06 1959-12-31 Rolls Royce Improvements in or relating to gas-turbine engine fuel systems
DE1020493B (en) * 1955-04-26 1957-12-05 Gen Electric Electrical control device to prevent excess temperatures in back pressure internal combustion engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1301933B (en) * 1965-03-10 1969-08-28 Snecma Afterburn control device for gas turbine jet engines with adjustable thrust nozzle
US4467600A (en) * 1979-07-31 1984-08-28 Messerschmitt-Boelkow-Blohm Gmbh System for controlling the thrust nozzle adjustment of dual cycle gas turbine jet propulsion engines

Also Published As

Publication number Publication date
GB1084957A (en) 1967-09-27
DE1289680B (en) 1969-02-20

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