GB1257072A - - Google Patents

Info

Publication number
GB1257072A
GB1257072A GB1257072DA GB1257072A GB 1257072 A GB1257072 A GB 1257072A GB 1257072D A GB1257072D A GB 1257072DA GB 1257072 A GB1257072 A GB 1257072A
Authority
GB
United Kingdom
Prior art keywords
converter
compressor
line
valve
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
Other languages
English (en)
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 filed Critical
Publication of GB1257072A publication Critical patent/GB1257072A/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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Jet Pumps And Other Pumps (AREA)
GB1257072D 1968-01-26 1969-01-22 Expired GB1257072A (forum.php)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US70094268A 1968-01-26 1968-01-26

Publications (1)

Publication Number Publication Date
GB1257072A true GB1257072A (forum.php) 1971-12-15

Family

ID=24815448

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1257072D Expired GB1257072A (forum.php) 1968-01-26 1969-01-22

Country Status (4)

Country Link
US (1) US3500637A (forum.php)
DE (1) DE1903512A1 (forum.php)
FR (1) FR2000834A1 (forum.php)
GB (1) GB1257072A (forum.php)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1591645A1 (fr) * 2004-04-28 2005-11-02 Eurocopter Dispositif et procédé de régulation du débit carburant d'un turbomoteur

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3657881A (en) * 1969-09-02 1972-04-25 Gen Motors Corp Gas turbine control with prewhirl of air entering the compressor
US3651640A (en) * 1970-09-25 1972-03-28 Power Technology Corp Gas turbine engine with aerodynamic torque converter drive
US3677003A (en) * 1971-02-01 1972-07-18 Twin Disc Inc Aerodynamic torque converter
US3753347A (en) * 1971-12-29 1973-08-21 Power Technology Corp Rankine cycle power plant with compressible fluid torque converter
US8056540B2 (en) * 2010-05-28 2011-11-15 Ford Global Technologies, Llc Method and system for fuel vapor control
CN113266474B (zh) * 2021-06-01 2022-07-15 中国航空工业集团公司沈阳飞机设计研究所 一种加载条件下的航空发动机起动阻力矩测量方法

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3314232A (en) * 1965-06-23 1967-04-18 Charles C Hill Gas turbine engine with aerodynamic torque converter drive

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1591645A1 (fr) * 2004-04-28 2005-11-02 Eurocopter Dispositif et procédé de régulation du débit carburant d'un turbomoteur
FR2869642A1 (fr) * 2004-04-28 2005-11-04 Eurocopter France Dispositif et procede de regulation en acceleration ou en deceleration du debit carburant d'un turbomoteur
US7992392B2 (en) 2004-04-28 2011-08-09 Eurocopter Method for regulating the flow rate of fuel to a turboshaft engine in acceleration or in deceleration

Also Published As

Publication number Publication date
DE1903512A1 (de) 1969-08-28
US3500637A (en) 1970-03-17
FR2000834A1 (forum.php) 1969-09-12

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees