FR967835A - Improvements to compressors in gas turbine units - Google Patents

Improvements to compressors in gas turbine units

Info

Publication number
FR967835A
FR967835A FR967835DA FR967835A FR 967835 A FR967835 A FR 967835A FR 967835D A FR967835D A FR 967835DA FR 967835 A FR967835 A FR 967835A
Authority
FR
France
Prior art keywords
compressors
gas turbine
turbine units
units
gas
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 FR967835A publication Critical patent/FR967835A/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)
FR967835D 1947-06-20 1948-06-19 Improvements to compressors in gas turbine units Expired FR967835A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB967835X 1947-06-20

Publications (1)

Publication Number Publication Date
FR967835A true FR967835A (en) 1950-11-13

Family

ID=10805348

Family Applications (1)

Application Number Title Priority Date Filing Date
FR967835D Expired FR967835A (en) 1947-06-20 1948-06-19 Improvements to compressors in gas turbine units

Country Status (1)

Country Link
FR (1) FR967835A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022073889A1 (en) * 2020-10-08 2022-04-14 Safran Nacelles Supersonic air intake of an aircraft propulsion assembly comprising a device for de-icing the support arms and de-icing method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022073889A1 (en) * 2020-10-08 2022-04-14 Safran Nacelles Supersonic air intake of an aircraft propulsion assembly comprising a device for de-icing the support arms and de-icing method
FR3115070A1 (en) * 2020-10-08 2022-04-15 Safran Nacelles Supersonic air intake of an aircraft propulsion system comprising a device for de-icing the support arms and method for de-icing
US12037940B2 (en) 2020-10-08 2024-07-16 Safran Nacelles Supersonic air inlet of an aircraft propelling assembly comprising a support arm de-icing device and de-icing method

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