FR1164542A - Starting process for gas turbine engine mechanisms, and installation for implementing said process - Google Patents

Starting process for gas turbine engine mechanisms, and installation for implementing said process

Info

Publication number
FR1164542A
FR1164542A FR1164542DA FR1164542A FR 1164542 A FR1164542 A FR 1164542A FR 1164542D A FR1164542D A FR 1164542DA FR 1164542 A FR1164542 A FR 1164542A
Authority
FR
France
Prior art keywords
implementing
installation
gas turbine
turbine engine
engine mechanisms
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.)
B M W STUDIENGESELLSCHAFT fur
Original Assignee
B M W STUDIENGESELLSCHAFT fur
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 B M W STUDIENGESELLSCHAFT fur filed Critical B M W STUDIENGESELLSCHAFT fur
Application granted granted Critical
Publication of FR1164542A publication Critical patent/FR1164542A/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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27—Fluid drives

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1164542D 1955-07-15 1956-07-13 Starting process for gas turbine engine mechanisms, and installation for implementing said process Expired FR1164542A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1164542X 1955-07-15

Publications (1)

Publication Number Publication Date
FR1164542A true FR1164542A (en) 1958-10-10

Family

ID=7728758

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1164542D Expired FR1164542A (en) 1955-07-15 1956-07-13 Starting process for gas turbine engine mechanisms, and installation for implementing said process

Country Status (1)

Country Link
FR (1) FR1164542A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1989012736A1 (en) * 1988-06-23 1989-12-28 Sundstrand Corporation Pulse accelerating turbine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1989012736A1 (en) * 1988-06-23 1989-12-28 Sundstrand Corporation Pulse accelerating turbine
US4947641A (en) * 1988-06-23 1990-08-14 Sundstrand Corporation Pulse accelerating turbine

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