GB782654A - Improvements in or relating to gas turbine engines - Google Patents

Improvements in or relating to gas turbine engines

Info

Publication number
GB782654A
GB782654A GB1701756A GB1701756A GB782654A GB 782654 A GB782654 A GB 782654A GB 1701756 A GB1701756 A GB 1701756A GB 1701756 A GB1701756 A GB 1701756A GB 782654 A GB782654 A GB 782654A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
control means
fuel
reheat
flow
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
GB1701756A
Inventor
David Omri Davies
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 GB1701756A priority Critical patent/GB782654A/en
Publication of GB782654A publication Critical patent/GB782654A/en
Expired legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/15Control or regulation
    • F02K1/16Control or regulation conjointly with another control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

782,654. Gas turbine jet-propulsion plant. ROLLS-ROYCE, Ltd. July 30,1954 [Sept. 14, 1953], No. 17017/56. Divided out of 782,653. Drawings to Specification. Class 110 (3). A gas turbine engine comprising reheat combustion equipment in which fuel is burnt in the exhaust gases before they pass to atmosphere has basic control means to vary the flow of reheat fuel in accordance with the compressor delivery pressure and trimming control means operative on the basic control means to modify the flow of reheat fuel so as to maintain the static or total head pressure or temperature respectively in the jet pipe in preselected relation to the compressor delivery pressure. The subject-matter of this Specification is identical with that described in Specification 782,653, but the claims differ. Specifications 641,910 and 748,353, [Group XXIX], also are referred to.
GB1701756A 1953-09-14 1953-09-14 Improvements in or relating to gas turbine engines Expired GB782654A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1701756A GB782654A (en) 1953-09-14 1953-09-14 Improvements in or relating to gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1701756A GB782654A (en) 1953-09-14 1953-09-14 Improvements in or relating to gas turbine engines

Publications (1)

Publication Number Publication Date
GB782654A true GB782654A (en) 1957-09-11

Family

ID=10087727

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1701756A Expired GB782654A (en) 1953-09-14 1953-09-14 Improvements in or relating to gas turbine engines

Country Status (1)

Country Link
GB (1) GB782654A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2172056A (en) * 1985-03-04 1986-09-10 Gen Electric Means and method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2172056A (en) * 1985-03-04 1986-09-10 Gen Electric Means and method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine

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