GB879745A - Gas flow control apparatus - Google Patents

Gas flow control apparatus

Info

Publication number
GB879745A
GB879745A GB1504659A GB1504659A GB879745A GB 879745 A GB879745 A GB 879745A GB 1504659 A GB1504659 A GB 1504659A GB 1504659 A GB1504659 A GB 1504659A GB 879745 A GB879745 A GB 879745A
Authority
GB
United Kingdom
Prior art keywords
branch
fuel
duct
valve gate
temperature
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
GB1504659A
Inventor
Frederick William Walto Morley
Donald Maynard Anley
Geoffrey Peter Torrance
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 GB1504659A priority Critical patent/GB879745A/en
Publication of GB879745A publication Critical patent/GB879745A/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
    • F02C7/22Fuel supply systems
    • F02C7/224Heating fuel before feeding to the burner
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D7/00Control of flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

879,745. Valves. ROLLS-ROYCE Ltd. April 25, 1960 [May 1, 1959], No. 15046/59. Class 135. [Also in Group XXVI] Gas flow-control apparatus comprising a duct for the passage of hot gas (e.g. hot air) provided with two branches, has closure means for selectively blocking one or other of the branches and for simultaneously effecting unblocking of the other branch and control means, operative upon the temperature of the gas reaching a predetermined value, for ensuring that a predetermined one of said branches is blocked. The invention is described with reference to a gas-turbine plant in which hot air from the compressor or ram air is heated by being passed over hot surfaces within the engine when being employed for cooling and sealing purposes and then led through a duct 29 to a valve 24 leading through a duct 22 to a heat exchanger for heating the fuel and through a branch 26 to atmosphere. A valve gate 27 is progressively movable between a position in which it blocks the branch 26 to a position in which it blocks the branch 23. With the valve shown the total hot gas flow remains constant. The valve gate 27 is connected by a fusible plug 36 to an arm 37 splined on a shaft 38. The shaft 38 is rotated by an arm 49 connected to a temperature responsive device mounted on the fuel heat-exchanger. In operation the temperature responsive means controls the valve gate 27 so that at a predetermined low-fuel temperature the valve gate blocks the branch 26 so that hot air is supplied to the fuel heat exchanger through the branch 23. If, however, the temperature of the hot air flowing through the duct 29 rises excessively (e.g. because of a seal failure), the fusible plug 36 will melt. The valve gate 27 will then be forced by the spring 48 into the position shown in Fig. 1, in which the branch 23 is blocked. This prevents excessive vaporization of the fuel and the consequent possibility of explosion.
GB1504659A 1959-05-01 1959-05-01 Gas flow control apparatus Expired GB879745A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1504659A GB879745A (en) 1959-05-01 1959-05-01 Gas flow control apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1504659A GB879745A (en) 1959-05-01 1959-05-01 Gas flow control apparatus

Publications (1)

Publication Number Publication Date
GB879745A true GB879745A (en) 1961-10-11

Family

ID=10052090

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1504659A Expired GB879745A (en) 1959-05-01 1959-05-01 Gas flow control apparatus

Country Status (1)

Country Link
GB (1) GB879745A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5255505A (en) * 1992-02-21 1993-10-26 Westinghouse Electric Corp. System for capturing heat transferred from compressed cooling air in a gas turbine
CN106368821A (en) * 2015-07-20 2017-02-01 通用电气公司 Cooling system for a turbine engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5255505A (en) * 1992-02-21 1993-10-26 Westinghouse Electric Corp. System for capturing heat transferred from compressed cooling air in a gas turbine
CN106368821A (en) * 2015-07-20 2017-02-01 通用电气公司 Cooling system for a turbine engine
US9995314B2 (en) 2015-07-20 2018-06-12 General Electric Company Cooling system for a turbine engine

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