GB407590A - Improvements in or relating to combustion-product engines - Google Patents

Improvements in or relating to combustion-product engines

Info

Publication number
GB407590A
GB407590A GB19638/33A GB1963833A GB407590A GB 407590 A GB407590 A GB 407590A GB 19638/33 A GB19638/33 A GB 19638/33A GB 1963833 A GB1963833 A GB 1963833A GB 407590 A GB407590 A GB 407590A
Authority
GB
United Kingdom
Prior art keywords
combustion
combustion chamber
engine
stages
class
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
GB19638/33A
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 GB19638/33A priority Critical patent/GB407590A/en
Publication of GB407590A publication Critical patent/GB407590A/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
    • F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G3/00—Combustion-product positive-displacement engine plants
    • F02G3/02—Combustion-product positive-displacement engine plants with reciprocating-piston engines
    • 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
    • F02B29/00—Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
    • 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)
  • Chemical Kinetics & Catalysis (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

407,590. Generating combustion products under pressure. KINGSTON, J. R., and POWELL, W. H., Engineer-in-Chief's Department, G.P.O., London. July 11, 1933, No. 19638. [Class 51 (i).] In a combustion-product engine in which a rotary blower 4 is used for the first stage of compression and a reciprocating compressor or compressors 3 for the final stage or stages, with inter-coolers 5 between the stages, the combustion chamber 2 comprises a comparatively long quartz tube 16 of relatively small bore, surrounded by a fireclay or other refractory and opaque covering protected by a layer 17 of a resilient nonconducting material such as asbestos or slag wool enclosed in an outer metal casing 26. The quartz tube 16 preferably has a length of at least ten times its diameter and at least five times the length of the piston stroke of the power cylinder. The fuel pump 6 is actuated by a cam 10 driven from the engine crank-shaft 11. Between the compressor 3 and the combustion chamber, the air may be passed through the tubes of a counterflow recuperator heated by the exhaust from the engine. In a modification, the combustion chamber is in the form of one or more long U-shaped tubes. Specifications 142,051 and 246,692, [both in Class 7 (i)], are referred to.
GB19638/33A 1933-07-11 1933-07-11 Improvements in or relating to combustion-product engines Expired GB407590A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB19638/33A GB407590A (en) 1933-07-11 1933-07-11 Improvements in or relating to combustion-product engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB19638/33A GB407590A (en) 1933-07-11 1933-07-11 Improvements in or relating to combustion-product engines

Publications (1)

Publication Number Publication Date
GB407590A true GB407590A (en) 1934-03-22

Family

ID=10132690

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19638/33A Expired GB407590A (en) 1933-07-11 1933-07-11 Improvements in or relating to combustion-product engines

Country Status (1)

Country Link
GB (1) GB407590A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4603547A (en) * 1980-10-10 1986-08-05 Williams Research Corporation Catalytic relight coating for gas turbine combustion chamber and method of application

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4603547A (en) * 1980-10-10 1986-08-05 Williams Research Corporation Catalytic relight coating for gas turbine combustion chamber and method of application

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