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FR998179A - Improvements to the sets of rotating machines operated by a fluid - Google Patents

Improvements to the sets of rotating machines operated by a fluid

Info

Publication number
FR998179A
FR998179A FR998179DA FR998179A FR 998179 A FR998179 A FR 998179A FR 998179D A FR998179D A FR 998179DA FR 998179 A FR998179 A FR 998179A
Authority
FR
France
Prior art keywords
fluid
sets
rotating machines
machines operated
operated
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 FR998179A publication Critical patent/FR998179A/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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
FR998179D 1948-10-28 1949-10-25 Improvements to the sets of rotating machines operated by a fluid Expired FR998179A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB998179X 1948-10-28

Publications (1)

Publication Number Publication Date
FR998179A true FR998179A (en) 1952-01-15

Family

ID=10867389

Family Applications (1)

Application Number Title Priority Date Filing Date
FR998179D Expired FR998179A (en) 1948-10-28 1949-10-25 Improvements to the sets of rotating machines operated by a fluid

Country Status (1)

Country Link
FR (1) FR998179A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1052821B (en) * 1955-01-25 1959-03-12 Georges Caillette Device for compensating the gyroscopic moments of gas turbines, especially in aircraft
FR2314362A1 (en) * 1975-06-11 1977-01-07 Mtu Muenchen Gmbh GAS TURBINE ENGINE WITH MODULAR STRUCTURE
US6301889B1 (en) * 2000-09-21 2001-10-16 Caterpillar Inc. Turbocharger with exhaust gas recirculation
EP1213445B1 (en) * 2000-12-07 2005-08-17 Hispano Suiza Reducing gear balancing the forces generated by the fan of a turbo machine
EP3643902A1 (en) * 2018-10-25 2020-04-29 Honeywell International Inc. Inlet flow structure for turboprop engine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1052821B (en) * 1955-01-25 1959-03-12 Georges Caillette Device for compensating the gyroscopic moments of gas turbines, especially in aircraft
FR2314362A1 (en) * 1975-06-11 1977-01-07 Mtu Muenchen Gmbh GAS TURBINE ENGINE WITH MODULAR STRUCTURE
US6301889B1 (en) * 2000-09-21 2001-10-16 Caterpillar Inc. Turbocharger with exhaust gas recirculation
EP1213445B1 (en) * 2000-12-07 2005-08-17 Hispano Suiza Reducing gear balancing the forces generated by the fan of a turbo machine
EP3643902A1 (en) * 2018-10-25 2020-04-29 Honeywell International Inc. Inlet flow structure for turboprop engine
US11072435B2 (en) 2018-10-25 2021-07-27 Honeywell International Inc. Inlet flow structure for turboprop engine

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