GB293594A - Improvements in or relating to apparatus for burning liquid or gaseous fuel and in the application thereof to internal combustion turbines, turbo-airscrews, projectiles, rockets and the like - Google Patents

Improvements in or relating to apparatus for burning liquid or gaseous fuel and in the application thereof to internal combustion turbines, turbo-airscrews, projectiles, rockets and the like

Info

Publication number
GB293594A
GB293594A GB3214125A GB3214125A GB293594A GB 293594 A GB293594 A GB 293594A GB 3214125 A GB3214125 A GB 3214125A GB 3214125 A GB3214125 A GB 3214125A GB 293594 A GB293594 A GB 293594A
Authority
GB
United Kingdom
Prior art keywords
fuel
pellet
airscrews
rockets
projectiles
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
GB3214125A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB3214125A priority Critical patent/GB293594A/en
Publication of GB293594A publication Critical patent/GB293594A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/005—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the engine comprising a rotor rotating under the actions of jets issuing from this rotor

Abstract

293,594. Carter, B. C. Dec. 19, 1925. Lighting burners by fulminating- pellet and like devices.-In a hollow projectile in which fuel contained under pressure in an annular chamber 9 issues through an orifice 11 on the operation of a valve 21 by a driver plate 26, the operation of the valve 21 actuates the firing bolt 29 of a percussion ignition device 12. Fig. 5 shows the use of a striker 30 operated by the explosion of the propellant charge to explode a percussion cap 32 adjacent a " thermit " or similar pellet 33. The heat generated at the pellet 33 fuses or releases a sealing disc 34 thereby opening the fuel conduit 35 and igniting the escaping fuel. Alternatively the fuel may be ignited by the explosion of the propellant charge acting through leak holes. Specifications 26197/12, 26281/12, [both in Class 51 (i), Furnaces and kilns, Combustion apparatus of], 227,151, and 287,701, [both in Class 110 (iii), Turbines &c.], are referred to.
GB3214125A 1925-12-19 1925-12-19 Improvements in or relating to apparatus for burning liquid or gaseous fuel and in the application thereof to internal combustion turbines, turbo-airscrews, projectiles, rockets and the like Expired GB293594A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3214125A GB293594A (en) 1925-12-19 1925-12-19 Improvements in or relating to apparatus for burning liquid or gaseous fuel and in the application thereof to internal combustion turbines, turbo-airscrews, projectiles, rockets and the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3214125A GB293594A (en) 1925-12-19 1925-12-19 Improvements in or relating to apparatus for burning liquid or gaseous fuel and in the application thereof to internal combustion turbines, turbo-airscrews, projectiles, rockets and the like

Publications (1)

Publication Number Publication Date
GB293594A true GB293594A (en) 1928-08-16

Family

ID=10333924

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3214125A Expired GB293594A (en) 1925-12-19 1925-12-19 Improvements in or relating to apparatus for burning liquid or gaseous fuel and in the application thereof to internal combustion turbines, turbo-airscrews, projectiles, rockets and the like

Country Status (1)

Country Link
GB (1) GB293594A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2601258A (en) * 1945-11-28 1952-06-24 Stefan Czarnecki Helicopter with jet-operated rotor
US2634577A (en) * 1949-01-03 1953-04-14 Havilland Engine Co Ltd Compact container arrangement for propellant feeding means of rockets
US2639580A (en) * 1945-03-21 1953-05-26 James L Stuart Valveless pulse jet engine
US2648196A (en) * 1947-03-18 1953-08-11 Experiment Inc Ram jet burner with aqueous injection to promote smooth burning
US2673696A (en) * 1946-05-24 1954-03-30 Autogiro Co Of America Helicopter having a jet-driven rotor system
US2684629A (en) * 1949-06-16 1954-07-27 Bofors Ab Reaction-motor missile
US2892410A (en) * 1946-04-03 1959-06-30 David H Sloan Ram jet projectile
US8117847B2 (en) 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2639580A (en) * 1945-03-21 1953-05-26 James L Stuart Valveless pulse jet engine
US2601258A (en) * 1945-11-28 1952-06-24 Stefan Czarnecki Helicopter with jet-operated rotor
US2892410A (en) * 1946-04-03 1959-06-30 David H Sloan Ram jet projectile
US2673696A (en) * 1946-05-24 1954-03-30 Autogiro Co Of America Helicopter having a jet-driven rotor system
US2648196A (en) * 1947-03-18 1953-08-11 Experiment Inc Ram jet burner with aqueous injection to promote smooth burning
US2634577A (en) * 1949-01-03 1953-04-14 Havilland Engine Co Ltd Compact container arrangement for propellant feeding means of rockets
US2684629A (en) * 1949-06-16 1954-07-27 Bofors Ab Reaction-motor missile
US8117847B2 (en) 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid

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