GB659802A - Improvements relating to the burning of mobile fuels in fast moving gas streams - Google Patents

Improvements relating to the burning of mobile fuels in fast moving gas streams

Info

Publication number
GB659802A
GB659802A GB2074846A GB2074846A GB659802A GB 659802 A GB659802 A GB 659802A GB 2074846 A GB2074846 A GB 2074846A GB 2074846 A GB2074846 A GB 2074846A GB 659802 A GB659802 A GB 659802A
Authority
GB
United Kingdom
Prior art keywords
piston
air
fuel
spring
plunger
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
GB2074846A
Inventor
Arthur Rynyon Devereux Robson
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB2074846A priority Critical patent/GB659802A/en
Publication of GB659802A publication Critical patent/GB659802A/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
    • F02C7/26Starting; Ignition
    • F02C7/264Ignition

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

659,802. Igniting burners. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. July 11, 1946, No. 20748. [Class 75(iii)] A liquid fuel pressure operated apparatus for initiating the action of a device for igniting a jet or spray of fuel in a fast moving air stream comprises a spring loaded piston operating in a cylinder, one side of the piston being exposed to the fuel pressure which opposes the spring loading, the cylinder space in the other side of the piston forming or communicating with a chamber in which air is alternately aspirated and compressed by the movements of the piston, the said air being utilized to initiate the action of the ignition device. The inlet 36, Fig. 1, of the cylinder 34 is connected to a branch from the fuel supply line downstream of the fuel cock, and the piston 22 is moved under the pressure of the fuel against the action of a spring 41. Towards the end of the latter movement an extension 24 of the piston 22 actuates a metering pump plunger 25 to deliver a measured quantity of an igniter fluid through a non-return valve 26 and connection 44 to a delivery line teminating at the burner. When the plunger 25 approaches the end of its stroke it uncovers a port 27 through which the air compressed between the piston 22 and the plunger 25 is released into the delivery line to blow the measured quantity of igniter fluid into the combustion region of the burner. At the return stroke of the plunger 25, effected by a spring 43, a fresh charge of igniter fluid is drawn into the pump chamber through the inlet 42 and non-return valve 28 and the space between the plunger 25 and the piston 22 is refilled with air, on the return stroke of the latter, through a non-return valve 29. Suitable igniter fluids are mentioned, in Specification 659,795. Alternatively, the fuel may be ignited by electrical means when the air space in the cylinder 34, Fig. 2 is connected with a chamber 46 containing a diaphragm 30 loaded by a spring 31 and having a stem 47 carrying a contact 48, which bridges the contacts 32 of an igniter circuit when the diaphragm 30 is raised by the pressure of the air compressed by the piston 22. A bleed hole 33 affords a controlled leak which after an appropriate delay, relieves the air pressure sufficiently to allow the spring 31 to return the' diaphragm 30 and contact 48 to the open circuit position. The apparatus shown in Fig. 1 or 2 may be modified to act as a fuel pressure accumulator as described in Specification 588,083, [Group XXVII].
GB2074846A 1946-07-11 1946-07-11 Improvements relating to the burning of mobile fuels in fast moving gas streams Expired GB659802A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2074846A GB659802A (en) 1946-07-11 1946-07-11 Improvements relating to the burning of mobile fuels in fast moving gas streams

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2074846A GB659802A (en) 1946-07-11 1946-07-11 Improvements relating to the burning of mobile fuels in fast moving gas streams

Publications (1)

Publication Number Publication Date
GB659802A true GB659802A (en) 1951-10-31

Family

ID=10151001

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2074846A Expired GB659802A (en) 1946-07-11 1946-07-11 Improvements relating to the burning of mobile fuels in fast moving gas streams

Country Status (1)

Country Link
GB (1) GB659802A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE942549C (en) * 1953-06-02 1956-05-03 Plessey Co Ltd Device for the flow control and ignition of liquid fuel, in particular start-up device for gas turbine combustion chambers
DE952855C (en) * 1952-06-01 1956-11-22 Plessey Co Ltd Control and ignition device for turbine starters operated with liquid fuel
US2913875A (en) * 1957-08-22 1959-11-24 Robert E Meyer Igniter fuel injector device
US3105356A (en) * 1958-04-28 1963-10-01 Thompson Ramo Wooldridge Inc Injector chamber construction
CN112412629A (en) * 2020-11-27 2021-02-26 中国航发四川燃气涡轮研究院 Adjustable telescopic automatic control igniter device

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE952855C (en) * 1952-06-01 1956-11-22 Plessey Co Ltd Control and ignition device for turbine starters operated with liquid fuel
DE942549C (en) * 1953-06-02 1956-05-03 Plessey Co Ltd Device for the flow control and ignition of liquid fuel, in particular start-up device for gas turbine combustion chambers
US2913875A (en) * 1957-08-22 1959-11-24 Robert E Meyer Igniter fuel injector device
US3105356A (en) * 1958-04-28 1963-10-01 Thompson Ramo Wooldridge Inc Injector chamber construction
CN112412629A (en) * 2020-11-27 2021-02-26 中国航发四川燃气涡轮研究院 Adjustable telescopic automatic control igniter device
CN112412629B (en) * 2020-11-27 2022-09-20 中国航发四川燃气涡轮研究院 Adjustable telescopic automatic control igniter device

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