FR971304A - Improvements relating to gas turbo-engine units for aircraft - Google Patents

Improvements relating to gas turbo-engine units for aircraft

Info

Publication number
FR971304A
FR971304A FR971304DA FR971304A FR 971304 A FR971304 A FR 971304A FR 971304D A FR971304D A FR 971304DA FR 971304 A FR971304 A FR 971304A
Authority
FR
France
Prior art keywords
aircraft
improvements relating
gas turbo
engine units
engine
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.)
Rotol Ltd
Original Assignee
Rotol Ltd
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 Rotol Ltd filed Critical Rotol Ltd
Application granted granted Critical
Publication of FR971304A publication Critical patent/FR971304A/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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR971304D 1947-08-18 1948-08-17 Improvements relating to gas turbo-engine units for aircraft Expired FR971304A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB971304X 1947-08-18

Publications (1)

Publication Number Publication Date
FR971304A true FR971304A (en) 1951-01-16

Family

ID=10814645

Family Applications (1)

Application Number Title Priority Date Filing Date
FR971304D Expired FR971304A (en) 1947-08-18 1948-08-17 Improvements relating to gas turbo-engine units for aircraft

Country Status (1)

Country Link
FR (1) FR971304A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2635824A1 (en) * 1988-08-25 1990-03-02 Mtu Muenchen Gmbh GAS TURBOMOTEUR TURBOMOTOR DRIVEN BY A ROTORS REDUCER WITH PROPELLERS OR BLOWER ROTORS
DE102010010130A1 (en) * 2010-03-04 2011-09-08 Rolls-Royce Deutschland Ltd & Co Kg Aircraft gas turbine drive has core plant and two counter-rotating pusher propellers, where bleed air is removed from low-pressure compressor and is introduced in inner chamber of propeller hubs
EP3812553A1 (en) * 2019-10-25 2021-04-28 Pratt & Whitney Canada Corp. Fan blade anti-icing concept

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2635824A1 (en) * 1988-08-25 1990-03-02 Mtu Muenchen Gmbh GAS TURBOMOTEUR TURBOMOTOR DRIVEN BY A ROTORS REDUCER WITH PROPELLERS OR BLOWER ROTORS
DE102010010130A1 (en) * 2010-03-04 2011-09-08 Rolls-Royce Deutschland Ltd & Co Kg Aircraft gas turbine drive has core plant and two counter-rotating pusher propellers, where bleed air is removed from low-pressure compressor and is introduced in inner chamber of propeller hubs
DE102010010130B4 (en) 2010-03-04 2020-06-04 Rolls-Royce Deutschland Ltd & Co Kg Aircraft turbine engine with de-icing
EP3812553A1 (en) * 2019-10-25 2021-04-28 Pratt & Whitney Canada Corp. Fan blade anti-icing concept
US11073082B2 (en) 2019-10-25 2021-07-27 Pratt & Whitney Canada Corp. Fan blade anti-icing concept
US11391208B2 (en) 2019-10-25 2022-07-19 Pratt & Whitney Canada Corp. Fan blade anti-icing concept

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