GB768969A - Improvements in jet propulsion plant - Google Patents

Improvements in jet propulsion plant

Info

Publication number
GB768969A
GB768969A GB957755A GB957755A GB768969A GB 768969 A GB768969 A GB 768969A GB 957755 A GB957755 A GB 957755A GB 957755 A GB957755 A GB 957755A GB 768969 A GB768969 A GB 768969A
Authority
GB
United Kingdom
Prior art keywords
fuel
distributers
propulsion plant
jet
jet propulsion
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
GB957755A
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.)
Solar Aircraft Co
Original Assignee
Solar Aircraft Co
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
Priority to US260048A priority Critical patent/US2780915A/en
Application filed by Solar Aircraft Co filed Critical Solar Aircraft Co
Priority to GB957755A priority patent/GB768969A/en
Publication of GB768969A publication Critical patent/GB768969A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

768,969. Jet-propulsion plant. SOLAR AIRCRAFT CO. April 1, 1955, No. 9577/55. Class 110 (3). [Also in Group XII] A gas turbine jet-propulsion unit is provided with five fuel distributers 31, 32, 33, 34, 35, which are arranged, as shown, and connected to a pump 42 adapted to supply fuel to the distributers 31-34 or the distributers 32-35 according to the setting of the valve 58. The distributer 32 may be arranged within the stator see Fig. 4 (not shown). Fuel vaporizers or spray-type fuel injectors may be employed. The number of openings in the fuel distributers progressively increases, as shown, whereby fuel is added at a rate proportional to the heat of vaporization in the preceding zone of combustion.
GB957755A 1951-12-05 1955-04-01 Improvements in jet propulsion plant Expired GB768969A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US260048A US2780915A (en) 1951-12-05 1951-12-05 Fuel distribution system for jet engine and afterburner
GB957755A GB768969A (en) 1955-04-01 1955-04-01 Improvements in jet propulsion plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB957755A GB768969A (en) 1955-04-01 1955-04-01 Improvements in jet propulsion plant

Publications (1)

Publication Number Publication Date
GB768969A true GB768969A (en) 1957-02-27

Family

ID=9874681

Family Applications (1)

Application Number Title Priority Date Filing Date
GB957755A Expired GB768969A (en) 1951-12-05 1955-04-01 Improvements in jet propulsion plant

Country Status (1)

Country Link
GB (1) GB768969A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0005425A1 (en) * 1978-04-27 1979-11-14 United Technologies Corporation Control means for an augmentor for a gas turbine engine
GB2275738A (en) * 1987-01-24 1994-09-07 Topexpress Ltd Reducing combustion vibration
FR2732407A1 (en) * 1995-03-29 1996-10-04 Snecma PROCESS FOR AVOIDING COMBUSTION INSTABILITIES IN A TURBO-JET
EP2993405A1 (en) * 2014-09-05 2016-03-09 United Technologies Corporation Variable orifice jet for a turbine engine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0005425A1 (en) * 1978-04-27 1979-11-14 United Technologies Corporation Control means for an augmentor for a gas turbine engine
GB2275738A (en) * 1987-01-24 1994-09-07 Topexpress Ltd Reducing combustion vibration
GB2275738B (en) * 1987-01-24 1995-01-25 Topexpress Ltd Reducing reheat buzz in a gas turbine aeroengine
FR2732407A1 (en) * 1995-03-29 1996-10-04 Snecma PROCESS FOR AVOIDING COMBUSTION INSTABILITIES IN A TURBO-JET
US5699663A (en) * 1995-03-29 1997-12-23 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Method of preventing instabilities produced by combustion in a turbojet engine
EP2993405A1 (en) * 2014-09-05 2016-03-09 United Technologies Corporation Variable orifice jet for a turbine engine
US10041444B2 (en) 2014-09-05 2018-08-07 United Technologies Corporation Variable orifice jet for a turbine engine

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