FR1361269A - Turbine - Google Patents

Turbine

Info

Publication number
FR1361269A
FR1361269A FR940081A FR940081A FR1361269A FR 1361269 A FR1361269 A FR 1361269A FR 940081 A FR940081 A FR 940081A FR 940081 A FR940081 A FR 940081A FR 1361269 A FR1361269 A FR 1361269A
Authority
FR
France
Prior art keywords
turbine
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
FR940081A
Other languages
English (en)
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.)
Garrett Corp
Original Assignee
Garrett 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
Priority claimed from US206840A external-priority patent/US3238721A/en
Application filed by Garrett Corp filed Critical Garrett Corp
Priority to FR940081A priority Critical patent/FR1361269A/fr
Application granted granted Critical
Publication of FR1361269A publication Critical patent/FR1361269A/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275Mechanical drives
    • F02C7/277Mechanical drives the starter being a separate turbine
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27Fluid drives
    • F02C7/272Fluid drives generated by cartridges

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR940081A 1962-07-02 1963-07-02 Turbine Expired FR1361269A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR940081A FR1361269A (fr) 1962-07-02 1963-07-02 Turbine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US206840A US3238721A (en) 1962-07-02 1962-07-02 Engine starter
FR940081A FR1361269A (fr) 1962-07-02 1963-07-02 Turbine

Publications (1)

Publication Number Publication Date
FR1361269A true FR1361269A (fr) 1964-05-15

Family

ID=26202174

Family Applications (1)

Application Number Title Priority Date Filing Date
FR940081A Expired FR1361269A (fr) 1962-07-02 1963-07-02 Turbine

Country Status (1)

Country Link
FR (1) FR1361269A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3010740A1 (fr) * 2013-09-19 2015-03-20 Snecma Systeme et procede de demarrage d'urgence d'une turbomachine d'aeronef

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3010740A1 (fr) * 2013-09-19 2015-03-20 Snecma Systeme et procede de demarrage d'urgence d'une turbomachine d'aeronef
WO2015040310A1 (fr) * 2013-09-19 2015-03-26 Snecma Système et procédé de démarrage d'urgence d'une turbomachine d'aéronef
US9951694B2 (en) 2013-09-19 2018-04-24 Safran Aircraft Engines System and method for emergency starting of an aircraft turbomachine

Similar Documents

Publication Publication Date Title
CH397148A (fr) Trachéotome
FR1361973A (fr) Combiné hélicoptère-avion
AT237955B (de) Heuwerbegerät
CH396068A (fr) Vibro-finisseur
FR1326037A (fr) Turbine
CH394992A (fr) Haveuse
AT241188B (de) Heuwerbemaschine
AT245462B (de) Barrenholm
AT243202B (de) Pelton-Turbine
FR1361269A (fr) Turbine
CH401870A (it) Sportjacke
FR1382058A (fr) Turbine
BE675043Q (fr) Sieraad
BE637189R (fr) Telecommunicatiesysteem
DE1491504B2 (de) Reflexklystron
CH412008A (de) Parametron
BE633541A (fr) Diazabicyclo-octanes
FR1341331A (fr) Turbo-réacteur
FI41053C (fi) Tvättmedelsblandning i fast form innehållande en tertiär aminoxid
FR1326107A (fr) Turbine centripète
ES92024Y (es) Mueble-mesa combinado
ES93940Y (es) Silla-escalera
ES92786Y (es) Goma-juguete
ES92149Y (es) Palomilla cuelga-pantalones
ES92312Y (es) Cierre-resbalón