GB595973A - Improvements in or relating to internal-combustion engines combined with exhaust-actuated turbines and jet propulsion units - Google Patents

Improvements in or relating to internal-combustion engines combined with exhaust-actuated turbines and jet propulsion units

Info

Publication number
GB595973A
GB595973A GB17787/45A GB1778745A GB595973A GB 595973 A GB595973 A GB 595973A GB 17787/45 A GB17787/45 A GB 17787/45A GB 1778745 A GB1778745 A GB 1778745A GB 595973 A GB595973 A GB 595973A
Authority
GB
United Kingdom
Prior art keywords
exhaust
valves
internal
pipes
fed
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
GB17787/45A
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
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of GB595973A publication Critical patent/GB595973A/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
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02—Engines with prolonged expansion
    • F02B41/10—Engines with prolonged expansion in exhaust turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/08—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by the fuel being carried by compressed air into main stream of combustion-air
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Gas After Treatment (AREA)

Abstract

595,973. Gas turbines ; motor power plant. RINGHAM, A. July 12, 1945, No. 17787. [Class 110 (iii)] [Also in Group XXVII] An exhaust-actuated turbine x is mounted on an internal-combustion engine shaft driving directly a fan supplying charge to a jetpropulsion unit 7. Air passing through cones b in a propeller is fed by passages c to a chamber i in the hub from which it passes by a pipe 19, controlled by a valve e operated hydraulically, to cylinder ports o. Exhaust valve springs t are tensioned so that the valves open on firing, and high-pressure exhaust passes by pipes w to the turbine. The valves 1 are held open by arms 17 which are spring-pressed under heads u until they are moved back by the. engagement of push-rods 14 on their sloping heads: Fuel is fed by nozzles 12 on to an annular baffle 10 heated by exhaust flowing through pipes 11 and it is mixed with air supplied by the fan 1 and controlled by flap valves 6, the mixture being ignited by sparking-plugs 8.
GB17787/45A 1945-07-12 Improvements in or relating to internal-combustion engines combined with exhaust-actuated turbines and jet propulsion units Expired GB595973A (en)

Publications (1)

Publication Number Publication Date
GB595973A true GB595973A (en) 1947-12-23

Family

ID=1733404

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17787/45A Expired GB595973A (en) 1945-07-12 Improvements in or relating to internal-combustion engines combined with exhaust-actuated turbines and jet propulsion units

Country Status (1)

Country Link
GB (1) GB595973A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2799137A (en) * 1952-02-26 1957-07-16 Tenney Method of and apparatus for feeding fuel to a resonant pulse jet engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2799137A (en) * 1952-02-26 1957-07-16 Tenney Method of and apparatus for feeding fuel to a resonant pulse jet engine

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