GB1127653A - Improvements in and relating to a continuous fuel splash plate arrangement for a gas turbine jet propulsion engine afterburner - Google Patents

Improvements in and relating to a continuous fuel splash plate arrangement for a gas turbine jet propulsion engine afterburner

Info

Publication number
GB1127653A
GB1127653A GB18601/66A GB1860166A GB1127653A GB 1127653 A GB1127653 A GB 1127653A GB 18601/66 A GB18601/66 A GB 18601/66A GB 1860166 A GB1860166 A GB 1860166A GB 1127653 A GB1127653 A GB 1127653A
Authority
GB
United Kingdom
Prior art keywords
relating
gas turbine
splash plate
jet propulsion
propulsion engine
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
GB18601/66A
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft 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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB1127653A publication Critical patent/GB1127653A/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)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

1,127,653. Reheat combustion equipment. UNITED AIRCRAFT CORP. April 28, 1966 [April 29, 1965], No. 18601/66. Heading F1L. The subject matter of this Specification is the same as that described in Specifications 1,127, 651 and 1,127,652 but the claims relate to the arrangement of the fuel dispensing ring and its splash plate in the engine reheat equipment.
GB18601/66A 1965-04-29 1966-04-28 Improvements in and relating to a continuous fuel splash plate arrangement for a gas turbine jet propulsion engine afterburner Expired GB1127653A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US451860A US3269115A (en) 1965-04-29 1965-04-29 Jet engine afterburner continuous splash plate

Publications (1)

Publication Number Publication Date
GB1127653A true GB1127653A (en) 1968-09-18

Family

ID=23794007

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18601/66A Expired GB1127653A (en) 1965-04-29 1966-04-28 Improvements in and relating to a continuous fuel splash plate arrangement for a gas turbine jet propulsion engine afterburner

Country Status (2)

Country Link
US (1) US3269115A (en)
GB (1) GB1127653A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3485045A (en) * 1968-07-23 1969-12-23 United Aircraft Corp Afterburner for bypass turbine engine
US3574507A (en) * 1969-07-31 1971-04-13 Gen Electric Air/fuel mixing and flame-stabilizing device for fluid fuel burners
US4594851A (en) * 1983-12-16 1986-06-17 The United States Of America As Represented By The Secretary Of The Air Force Flameholder with removable flameholder attachments
US5179832A (en) * 1991-07-26 1993-01-19 United Technologies Corporation Augmenter flame holder construction
US10563868B2 (en) * 2017-05-08 2020-02-18 General Electric Company Coupling method and structure for a propulsion system hot section

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2793495A (en) * 1951-05-01 1957-05-28 Gen Motors Corp Jet propulsion combustion apparatus with expansibly mounted fuel manifold
US2728191A (en) * 1954-03-25 1955-12-27 Casey Hilton Wayne Steam generation and auxiliary engines for ram jet engines

Also Published As

Publication number Publication date
US3269115A (en) 1966-08-30

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