GB541349A - Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft - Google Patents

Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft

Info

Publication number
GB541349A
GB541349A GB1189940A GB1189940A GB541349A GB 541349 A GB541349 A GB 541349A GB 1189940 A GB1189940 A GB 1189940A GB 1189940 A GB1189940 A GB 1189940A GB 541349 A GB541349 A GB 541349A
Authority
GB
United Kingdom
Prior art keywords
propulsion
aircraft
relating
gas turbines
prime movers
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
GB1189940A
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 GB1189940A priority Critical patent/GB541349A/en
Publication of GB541349A publication Critical patent/GB541349A/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)
  • Discharge Lamp (AREA)

Abstract

541,349. Propelling ships. HEWSON, B. T., and LOCAN, A. July 19, 1940, No. 11899. [Class 114] [Also in Group XXVI] A combustion chamber 101 delivers gas to a central jet tube 100 and other ignition apparatuses 104 deliver gas through orifices 105 into the jet tube. The chamber 101 may be replaced by a funnel-shaped opening having a spring-pressed valve opening inwards with the air pressure.
GB1189940A 1940-07-19 1940-07-19 Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft Expired GB541349A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1189940A GB541349A (en) 1940-07-19 1940-07-19 Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1189940A GB541349A (en) 1940-07-19 1940-07-19 Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft

Publications (1)

Publication Number Publication Date
GB541349A true GB541349A (en) 1941-11-24

Family

ID=9994693

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1189940A Expired GB541349A (en) 1940-07-19 1940-07-19 Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft

Country Status (1)

Country Link
GB (1) GB541349A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2435138A (en) * 1943-01-15 1948-01-27 Armstrong Siddeley Motors Ltd Compound internal-combustion turbine plant
US2454738A (en) * 1944-01-31 1948-11-23 Power Jets Res And Development Internal-combustion turbine power plant
US2477798A (en) * 1941-04-08 1949-08-02 Rolls Royce Contrarotating axial flow high and low pressure turbine and compressor with bladed duct with turbine cooling
US2479573A (en) * 1943-10-20 1949-08-23 Gen Electric Gas turbine power plant
US2518498A (en) * 1946-03-25 1950-08-15 Schulte Rudolph Carl Propulsion system for aircraft
US2531761A (en) * 1944-12-02 1950-11-28 Aerojet Engineering Corp Thermal jet and rocket motor propulsion system
US2593541A (en) * 1947-04-03 1952-04-22 Napier & Son Ltd Cooling apparatus for use with aero or other engines
US3410093A (en) * 1967-05-26 1968-11-12 Ghougasian John Nazareth Reaction thrust engine with fluid operated compressor

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2477798A (en) * 1941-04-08 1949-08-02 Rolls Royce Contrarotating axial flow high and low pressure turbine and compressor with bladed duct with turbine cooling
US2435138A (en) * 1943-01-15 1948-01-27 Armstrong Siddeley Motors Ltd Compound internal-combustion turbine plant
US2479573A (en) * 1943-10-20 1949-08-23 Gen Electric Gas turbine power plant
US2454738A (en) * 1944-01-31 1948-11-23 Power Jets Res And Development Internal-combustion turbine power plant
US2531761A (en) * 1944-12-02 1950-11-28 Aerojet Engineering Corp Thermal jet and rocket motor propulsion system
US2518498A (en) * 1946-03-25 1950-08-15 Schulte Rudolph Carl Propulsion system for aircraft
US2593541A (en) * 1947-04-03 1952-04-22 Napier & Son Ltd Cooling apparatus for use with aero or other engines
US3410093A (en) * 1967-05-26 1968-11-12 Ghougasian John Nazareth Reaction thrust engine with fluid operated compressor

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