GB585334A - Improvements in or relating to internal-combustion turbines - Google Patents

Improvements in or relating to internal-combustion turbines

Info

Publication number
GB585334A
GB585334A GB6209/41A GB620941A GB585334A GB 585334 A GB585334 A GB 585334A GB 6209/41 A GB6209/41 A GB 6209/41A GB 620941 A GB620941 A GB 620941A GB 585334 A GB585334 A GB 585334A
Authority
GB
United Kingdom
Prior art keywords
air
exchanger
fuel oil
heat
ports
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
GB6209/41A
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 GB6209/41A priority Critical patent/GB585334A/en
Priority to US505392A priority patent/US2413225A/en
Publication of GB585334A publication Critical patent/GB585334A/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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185—Cooling means for reducing the temperature of the cooling air or gas

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

585,334. Gas turbines. GRIFFITH, A. A. May 14, 1941, No. 6209. [Class 110 (iii)] In a gas turbine, air, which is taken from the delivery of the air-compressor for supplying to end-thrust balancing devices and, for use as a cooling medium, to bearings &c. is cooled by heat interchange with the fuel oil. A heatexchanger is located in the space between the diaphragm 28 and a cover 27. Air from the compressor delivery enters by ports 30 and after traversing the heat-exchanger passes into the hollow shaft 10 for distribution. Fuel oil passes along a pipe 24 within the hollow shaft and enters the exchanger through ports 32, leaving it by passages 33 on its way to the burner. The heat-exchanger is made up of a number of nested cylinders and, in an alternative, of a number of associated discs. As the fuel oil and the circulating air are at the same pressure, light constructions may be used. Specifications 585,330 and 585,332 are referred to.
GB6209/41A 1941-05-14 1941-05-14 Improvements in or relating to internal-combustion turbines Expired GB585334A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB6209/41A GB585334A (en) 1941-05-14 1941-05-14 Improvements in or relating to internal-combustion turbines
US505392A US2413225A (en) 1941-05-14 1943-10-07 Internal-combustion turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB6209/41A GB585334A (en) 1941-05-14 1941-05-14 Improvements in or relating to internal-combustion turbines

Publications (1)

Publication Number Publication Date
GB585334A true GB585334A (en) 1947-02-05

Family

ID=9810405

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6209/41A Expired GB585334A (en) 1941-05-14 1941-05-14 Improvements in or relating to internal-combustion turbines

Country Status (2)

Country Link
US (1) US2413225A (en)
GB (1) GB585334A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1085718B (en) * 1958-11-26 1960-07-21 Daimler Benz Ag Gas turbine engine
DE1214053B (en) * 1960-09-14 1966-04-07 Snecma Turbine jet engine
DE3218927A1 (en) * 1982-05-19 1983-11-24 Klöckner-Humboldt-Deutz AG, 5000 Köln GAS TURBINE ENGINE FOR AN AIRCRAFT

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR957061A (en) * 1944-09-23 1950-02-14
US2463851A (en) * 1944-11-30 1949-03-08 Wright Aeronautical Corp Turbine cooling system
US2589239A (en) * 1945-05-16 1952-03-18 Malcolm Mitchell Turbine-compressor unit
US2602289A (en) * 1945-05-25 1952-07-08 Rateau Soc Method and means for propelling a vehicle using normally gaseous fuel as a liquid
US2611241A (en) * 1946-03-19 1952-09-23 Packard Motor Car Co Power plant comprising a toroidal combustion chamber and an axial flow gas turbine with blade cooling passages therein forming a centrifugal air compressor
US2631430A (en) * 1946-12-12 1953-03-17 Chrysler Corp Gas turbine power plant having coaxially arranged combustors and regenerator
US2639583A (en) * 1947-06-25 1953-05-26 Harry C Steele Contrarotating gas turbine having a power turbine and a plurality of compressor-turbines in series
US2541108A (en) * 1947-08-06 1951-02-13 Westinghouse Electric Corp Cooling of annular combustion chamber fuel manifolds
US2668413A (en) * 1948-03-15 1954-02-09 James V Giliberty Gas turbine power plant with duplexed blading
US2648519A (en) * 1948-04-22 1953-08-11 Campini Secondo Cooling combustion turbines
US2721445A (en) * 1949-12-22 1955-10-25 James V Giliberty Aircraft propulsion plant of the propeller-jet turbine type
US2783613A (en) * 1951-01-18 1957-03-05 Helmut P G A R Von Zborowski Cooling system employing fuel for cooling the blades of gas turbine engines
US2942413A (en) * 1954-10-28 1960-06-28 Thompson Ramo Wooldridge Inc Turbine cooling system
US3294161A (en) * 1961-07-03 1966-12-27 Continental Aviat & Eng Corp Heat exchangers
US3272429A (en) * 1964-10-16 1966-09-13 Westinghouse Electric Corp Rotors of centrifugal fans
US3847298A (en) * 1972-03-20 1974-11-12 Garrett Corp Fuel tank inerting system
US4949544A (en) * 1988-12-06 1990-08-21 General Electric Company Series intercooler
GB201902095D0 (en) 2019-02-15 2019-04-03 Rolls Royce Plc Electric turbomachine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1085718B (en) * 1958-11-26 1960-07-21 Daimler Benz Ag Gas turbine engine
DE1214053B (en) * 1960-09-14 1966-04-07 Snecma Turbine jet engine
DE3218927A1 (en) * 1982-05-19 1983-11-24 Klöckner-Humboldt-Deutz AG, 5000 Köln GAS TURBINE ENGINE FOR AN AIRCRAFT
FR2527266A1 (en) * 1982-05-19 1983-11-25 Kloeckner Humboldt Deutz Ag GAS TURBINE PROPELLER FOR MISSILE

Also Published As

Publication number Publication date
US2413225A (en) 1946-12-24

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