GB729272A - Fuel control system for gas turbines - Google Patents

Fuel control system for gas turbines

Info

Publication number
GB729272A
GB729272A GB18713/53A GB1871353A GB729272A GB 729272 A GB729272 A GB 729272A GB 18713/53 A GB18713/53 A GB 18713/53A GB 1871353 A GB1871353 A GB 1871353A GB 729272 A GB729272 A GB 729272A
Authority
GB
United Kingdom
Prior art keywords
control system
fuel control
gas turbines
gas turbine
throttle valve
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
GB18713/53A
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB729272A publication Critical patent/GB729272A/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
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16Control of working fluid flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

729,272. Gas turbine plant. BENDIX AVIATION CORPORATION. July 14, 1949 [Aug. 10, 1948], No. 18713/53. Divided out of 729,201. Drawings to Specification. Class 110(3). [Also in Group XXIX] A fuel system for a gas turbine plant consisting of a fuel pump discharging to the combustion chamber through a main conduit having a throttle valve and a regulator valve for varying the head across the throttle valve located therein has the regulator valve controlled by means responsive to the turbine inlet temperature to maintain a preselected limit on the fuel flow. The subject-matter of this Specification is substantially the same as that described in Specification 729,201, but the claims differ. Specification 729,300 also is referred to.
GB18713/53A 1948-08-10 1949-07-14 Fuel control system for gas turbines Expired GB729272A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US729272XA 1948-08-10 1948-08-10

Publications (1)

Publication Number Publication Date
GB729272A true GB729272A (en) 1955-05-04

Family

ID=22110596

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18713/53A Expired GB729272A (en) 1948-08-10 1949-07-14 Fuel control system for gas turbines

Country Status (1)

Country Link
GB (1) GB729272A (en)

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