GB711788A - Improvements in or relating to gas-turbine power plants - Google Patents

Improvements in or relating to gas-turbine power plants

Info

Publication number
GB711788A
GB711788A GB14251A GB14251A GB711788A GB 711788 A GB711788 A GB 711788A GB 14251 A GB14251 A GB 14251A GB 14251 A GB14251 A GB 14251A GB 711788 A GB711788 A GB 711788A
Authority
GB
United Kingdom
Prior art keywords
clutch
oil
passages
fed
friction
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
GB14251A
Inventor
Lionel Haworth
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
Priority to GB14251A priority Critical patent/GB711788A/en
Publication of GB711788A publication Critical patent/GB711788A/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
    • F02C7/36Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/40Transmission of power
    • F05D2260/402Transmission of power through friction drives
    • F05D2260/4023Transmission of power through friction drives through a friction clutch
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/40Transmission of power
    • F05D2260/406Transmission of power through hydraulic systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (AREA)

Abstract

711,788. Friction clutches. ROLLS-ROYCE, Ltd. April 1, 1952 [Jan. 2, 1951], No. 142/51. Class 80 (2) [Also in Groups XXVI, XXIX and XXXIII] A clutch .24, Fig. 2, comprises a hydraulic clutch and a friction clutch having a common casing 25 which is splined to the driving shaft 10a of a gas turbine engine. The hydraulic clutch is fed with oil through passages 30, 31 as shown and is drained through a restricted orifice 32. The friction clutch comprises plates 34, 35 which are urged together, against the action of springs 36, by pistons 37 sliding in cylinders 38. The cylinders are supplied with oil through passages 39, 40 and exhausted through ports 41 which are controlled by valves 42. The valves are opened against the action of springs 43 by solenoids 44. If desired the actuation of the hydraulic and friction clutches may be effected in response to the speed of the driving shaft 10a and the driven shaft 22 respectively. In a modification, Fig. 4, the hydraulic clutch is fed with oil through passages 50, 51, 52, 55, 56 and drained through a spring loaded ball valve 57. The plates of the friction clutch are urged together by a piston and cylinder unit comprising a cylinder 58, 59 slidably mounted on the'driven shaft 22 and a piston 60 fixed thereto. The oil fed to the space between the parts 59, 60 is exhausted past the piston rings 61 which are adapted to be urged into contact with the cylinder wall by centrifugal force when the shaft 22 rotates.
GB14251A 1951-01-02 1951-01-02 Improvements in or relating to gas-turbine power plants Expired GB711788A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB14251A GB711788A (en) 1951-01-02 1951-01-02 Improvements in or relating to gas-turbine power plants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB14251A GB711788A (en) 1951-01-02 1951-01-02 Improvements in or relating to gas-turbine power plants

Publications (1)

Publication Number Publication Date
GB711788A true GB711788A (en) 1954-07-14

Family

ID=9699142

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14251A Expired GB711788A (en) 1951-01-02 1951-01-02 Improvements in or relating to gas-turbine power plants

Country Status (1)

Country Link
GB (1) GB711788A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0223364A1 (en) * 1985-11-21 1987-05-27 Avco Corporation Convertible turbo-fan, turbo-shaft aircraft propulsion system
EP1749995A2 (en) * 2005-08-03 2007-02-07 Candent Technologies, Inc. Multi spool gas turbine system
WO2014149121A2 (en) * 2013-03-07 2014-09-25 Bouton Matthew T Clutch coupled to gas turbine engine and method for cooling

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0223364A1 (en) * 1985-11-21 1987-05-27 Avco Corporation Convertible turbo-fan, turbo-shaft aircraft propulsion system
EP1749995A2 (en) * 2005-08-03 2007-02-07 Candent Technologies, Inc. Multi spool gas turbine system
EP1749995A3 (en) * 2005-08-03 2010-04-28 Candent Technologies, Inc. Multi spool gas turbine system
US8220245B1 (en) 2005-08-03 2012-07-17 Candent Technologies, Inc. Multi spool gas turbine system
WO2014149121A2 (en) * 2013-03-07 2014-09-25 Bouton Matthew T Clutch coupled to gas turbine engine and method for cooling
WO2014149121A3 (en) * 2013-03-07 2014-12-11 Bouton Matthew T Clutch coupled to gas turbine engine and method for cooling
US9534640B2 (en) 2013-03-07 2017-01-03 Rolls-Royce Corporation Clutch coupled to gas turbine engine and method for cooling
US10443663B2 (en) * 2013-03-07 2019-10-15 Rolls-Royce Corporation Clutch coupled to gas turbine engine and method for cooling

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