GB654200A - Improvements relating to burner ignition means - Google Patents

Improvements relating to burner ignition means

Info

Publication number
GB654200A
GB654200A GB23477/48A GB2347748A GB654200A GB 654200 A GB654200 A GB 654200A GB 23477/48 A GB23477/48 A GB 23477/48A GB 2347748 A GB2347748 A GB 2347748A GB 654200 A GB654200 A GB 654200A
Authority
GB
United Kingdom
Prior art keywords
fuel
burner
igniter
ignited
cone
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
GB23477/48A
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.)
GEORGE DAVID SMITH
Original Assignee
GEORGE DAVID SMITH
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 GEORGE DAVID SMITH filed Critical GEORGE DAVID SMITH
Publication of GB654200A publication Critical patent/GB654200A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/18Visual or acoustic landing aids
    • B64F1/20Arrangement of optical beacons
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/80Energy efficient operational measures, e.g. ground operations or mission management

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Spray-Type Burners (AREA)

Abstract

654,200. Lighting burners. SMITH, G. D. Sept. 7, 1948, No. 23477. Convention date, Sept. 8,1947. [Class 75(iii)] A burner from which fuel normally flows in a cone of a predetermined angle, but initially on starting up flows momentarily in a cone of a wider angle, is combined with an igniter having a cavity or recess therein disposed with its open end in proximity to and directed toward the burner, and within said wider angle but outside of said predetermined angle, a fuel igniter element being disposed in said cavity, and when the burner is started fuel is projected into the said cavity or recess to be ignited by the igniter element, the ignited fuel then flashing back to ignite the fuel stream flowing from the burner, and, after ignition the burning fuel normally will flow out of contact with the igniter. A burner 15 for use in fog dispersal is ignited by an electric heating element 12 disposed in a recess 55 beneath a protecting cover 21 at the top of a hollow column 13 through which passes electric supply leads 60, 61. The burner 15 is adapted to discharge dispersed liquid or gaseous fuel initially in a cone 40 of wide angle to be ignited by the heating element 12. and, after ignition and when the inertia of the fuel has been overcome, to discharge said fuel in a cone 50 of smaller angle so that the flame does not contact the igniter element 12.
GB23477/48A 1947-09-08 1948-09-07 Improvements relating to burner ignition means Expired GB654200A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US654200XA 1947-09-08 1947-09-08

Publications (1)

Publication Number Publication Date
GB654200A true GB654200A (en) 1951-06-13

Family

ID=22062589

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23477/48A Expired GB654200A (en) 1947-09-08 1948-09-07 Improvements relating to burner ignition means

Country Status (1)

Country Link
GB (1) GB654200A (en)

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