GB141336A - Heat engine of the internal combustion type - Google Patents

Heat engine of the internal combustion type

Info

Publication number
GB141336A
GB141336A GB8770/20A GB877020A GB141336A GB 141336 A GB141336 A GB 141336A GB 8770/20 A GB8770/20 A GB 8770/20A GB 877020 A GB877020 A GB 877020A GB 141336 A GB141336 A GB 141336A
Authority
GB
United Kingdom
Prior art keywords
turbine
internal combustion
heat engine
combustion chamber
combustion type
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
GB8770/20A
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.)
JEAN MARIE PIERRE BERTRAND AUG
Original Assignee
JEAN MARIE PIERRE BERTRAND AUG
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 JEAN MARIE PIERRE BERTRAND AUG filed Critical JEAN MARIE PIERRE BERTRAND AUG
Publication of GB141336A publication Critical patent/GB141336A/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
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

141,336. Le Bidolec, J. M. P. B. A. April 10, 1919, [Convention date]. Void [Published under Sect. 91 of the Act]. Working-fluid supply.-In a turbine system, the combination products are expanded to below atmospheric pressure, and in passing from the turbine 10, 11 to the vacuum pump 15 are cooled in a generator 6, which heats the air supplied by a compressor 2 to the combustion chamber 8. The exhaust gases may be further cooled by a. cooler 13. The turbine comprises initial impulse stages 10 and may include reaction stages 11. The regenerator pipes are ribbed. Fig. 5 shows a form of combustion chamber.
GB8770/20A 1919-04-10 1920-03-25 Heat engine of the internal combustion type Expired GB141336A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR141336X 1919-04-10

Publications (1)

Publication Number Publication Date
GB141336A true GB141336A (en) 1920-11-25

Family

ID=8874689

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8770/20A Expired GB141336A (en) 1919-04-10 1920-03-25 Heat engine of the internal combustion type

Country Status (1)

Country Link
GB (1) GB141336A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2490064A (en) * 1945-01-12 1949-12-06 Kollsman Paul Thermodynamic machine
US2601242A (en) * 1944-08-26 1952-06-24 Claude A Bonvillian Apparatus for the combustion of combustible and vaporizable substances

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2601242A (en) * 1944-08-26 1952-06-24 Claude A Bonvillian Apparatus for the combustion of combustible and vaporizable substances
US2490064A (en) * 1945-01-12 1949-12-06 Kollsman Paul Thermodynamic machine

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