FR1061753A - Turbo-jet engine control device comprising an exhaust nozzle of variable section - Google Patents

Turbo-jet engine control device comprising an exhaust nozzle of variable section

Info

Publication number
FR1061753A
FR1061753A FR1061753DA FR1061753A FR 1061753 A FR1061753 A FR 1061753A FR 1061753D A FR1061753D A FR 1061753DA FR 1061753 A FR1061753 A FR 1061753A
Authority
FR
France
Prior art keywords
turbo
control device
engine control
jet engine
exhaust 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
Other languages
French (fr)
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Application granted granted Critical
Publication of FR1061753A publication Critical patent/FR1061753A/en
Expired legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P23/00—Arrangements or methods for the control of AC motors characterised by a control method other than vector control
    • H02P23/16—Controlling the angular speed of one shaft

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
FR1061753D 1951-02-24 1952-02-23 Turbo-jet engine control device comprising an exhaust nozzle of variable section Expired FR1061753A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1061753XA 1951-02-24 1951-02-24

Publications (1)

Publication Number Publication Date
FR1061753A true FR1061753A (en) 1954-04-15

Family

ID=22309917

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1061753D Expired FR1061753A (en) 1951-02-24 1952-02-23 Turbo-jet engine control device comprising an exhaust nozzle of variable section

Country Status (1)

Country Link
FR (1) FR1061753A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2955412A (en) * 1957-01-17 1960-10-11 Gen Motors Corp Gas turbine nozzle control
US2972858A (en) * 1956-11-05 1961-02-28 Bendix Corp Exhaust area control for gas turbine engines
US2979889A (en) * 1956-09-18 1961-04-18 Bendix Corp Temperature-modified exhaust nozzle scheduling controller for a gas turbine engine
US2987876A (en) * 1956-02-29 1961-06-13 Bendix Corp Exhaust nozzle control for gas turbine engines
US3007303A (en) * 1955-07-08 1961-11-07 Bendix Corp Compressor pressure modified fuel schedule for an afterburner
US3082599A (en) * 1958-03-21 1963-03-26 United Aircraft Corp Coordinated control of afterburner fuel and exhaust nozzle area

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3007303A (en) * 1955-07-08 1961-11-07 Bendix Corp Compressor pressure modified fuel schedule for an afterburner
US2987876A (en) * 1956-02-29 1961-06-13 Bendix Corp Exhaust nozzle control for gas turbine engines
US2979889A (en) * 1956-09-18 1961-04-18 Bendix Corp Temperature-modified exhaust nozzle scheduling controller for a gas turbine engine
US2972858A (en) * 1956-11-05 1961-02-28 Bendix Corp Exhaust area control for gas turbine engines
US2955412A (en) * 1957-01-17 1960-10-11 Gen Motors Corp Gas turbine nozzle control
US3082599A (en) * 1958-03-21 1963-03-26 United Aircraft Corp Coordinated control of afterburner fuel and exhaust nozzle area

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