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FR1090733A - Improvements to Gas Turbine Power Plant Layouts - Google Patents

Improvements to Gas Turbine Power Plant Layouts

Info

Publication number
FR1090733A
FR1090733A FR1090733DA FR1090733A FR 1090733 A FR1090733 A FR 1090733A FR 1090733D A FR1090733D A FR 1090733DA FR 1090733 A FR1090733 A FR 1090733A
Authority
FR
France
Prior art keywords
gas turbine
power plant
turbine power
plant layouts
layouts
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1090733A publication Critical patent/FR1090733A/en
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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047Heating to prevent icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1090733D 1952-10-10 1953-10-08 Improvements to Gas Turbine Power Plant Layouts Expired FR1090733A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1090733X 1952-10-10

Publications (1)

Publication Number Publication Date
FR1090733A true FR1090733A (en) 1955-04-04

Family

ID=10873349

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1090733D Expired FR1090733A (en) 1952-10-10 1953-10-08 Improvements to Gas Turbine Power Plant Layouts

Country Status (1)

Country Link
FR (1) FR1090733A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2965285A (en) * 1955-10-10 1960-12-20 Holley Carburetor Co Compressor bleed control
US3031132A (en) * 1956-12-19 1962-04-24 Rolls Royce Gas-turbine engine with air tapping means
US3446425A (en) * 1967-04-27 1969-05-27 Mc Donnell Douglas Corp Means and method for minimizing bleed air contamination
FR2898939A1 (en) * 2006-03-22 2007-09-28 Snecma Sa SYSTEM FOR DEFROSTING A TURBOMOTEUR INPUT CONE FOR AN AIRCRAFT

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2965285A (en) * 1955-10-10 1960-12-20 Holley Carburetor Co Compressor bleed control
US3031132A (en) * 1956-12-19 1962-04-24 Rolls Royce Gas-turbine engine with air tapping means
US3446425A (en) * 1967-04-27 1969-05-27 Mc Donnell Douglas Corp Means and method for minimizing bleed air contamination
FR2898939A1 (en) * 2006-03-22 2007-09-28 Snecma Sa SYSTEM FOR DEFROSTING A TURBOMOTEUR INPUT CONE FOR AN AIRCRAFT
EP1840028A1 (en) * 2006-03-22 2007-10-03 Snecma De-icing system for the inlet cone of an aircraft turboengine
US7658077B2 (en) 2006-03-22 2010-02-09 Snecma System for deicing an aircraft turbine engine inlet cone
RU2444638C2 (en) * 2006-03-22 2012-03-10 Снекма Anti-ice system of aircraft gas turbine engine inlet cone

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