GB111381A - Improvements in Hot Air Turbines. - Google Patents

Improvements in Hot Air Turbines.

Info

Publication number
GB111381A
GB111381A GB69917A GB69917A GB111381A GB 111381 A GB111381 A GB 111381A GB 69917 A GB69917 A GB 69917A GB 69917 A GB69917 A GB 69917A GB 111381 A GB111381 A GB 111381A
Authority
GB
United Kingdom
Prior art keywords
water
holes
hot air
air turbines
turbines
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
GB69917A
Inventor
William John Rodgerson
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 GB69917A priority Critical patent/GB111381A/en
Publication of GB111381A publication Critical patent/GB111381A/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
    • F02C3/34—Gas-turbine plants characterised by the use of combustion products as the working fluid with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle
    • 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
    • F02C3/32—Inducing air flow by fluid jet, e.g. ejector action

Abstract

111,381. Rodgerson, W. J. Jan. 15, 1917. Density separators.-In a multi-stage centrifugal compressor for compressing gases isothermally, water jets are supplied to the gases during compression through holes 15 in the impellers; the last impeller has no holes, but is surrounded, outside the usual air volute, by a passage 17 into which surplus water is projected by centrifugal force, the water being drained by a pipe 18 and a trap. Specifications 2565/95, 18049/13 and 100,072 [Class 110 (iii), Turbines &c.], are referred to.
GB69917A 1917-01-15 1917-01-15 Improvements in Hot Air Turbines. Expired GB111381A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB69917A GB111381A (en) 1917-01-15 1917-01-15 Improvements in Hot Air Turbines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB69917A GB111381A (en) 1917-01-15 1917-01-15 Improvements in Hot Air Turbines.

Publications (1)

Publication Number Publication Date
GB111381A true GB111381A (en) 1917-11-29

Family

ID=32481147

Family Applications (1)

Application Number Title Priority Date Filing Date
GB69917A Expired GB111381A (en) 1917-01-15 1917-01-15 Improvements in Hot Air Turbines.

Country Status (1)

Country Link
GB (1) GB111381A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2499772A (en) * 1944-06-24 1950-03-07 Eugene F Osborne Liquid air turbine
US2504320A (en) * 1945-02-26 1950-04-18 Lindberg Eng Co Method of and apparatus for forced convection heating
US2583430A (en) * 1945-05-17 1952-01-22 Nina K Guercken Power plant, including a combustion chamber and an impulse turbine driven by exhaustgases from the chamber
US2612022A (en) * 1945-12-07 1952-09-30 Joseph F Keys Internal-combustion engine with rotary constant volume combustion chamber
US2686631A (en) * 1948-05-08 1954-08-17 United Aircraft Corp Coolant injection system for gas turbines

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2499772A (en) * 1944-06-24 1950-03-07 Eugene F Osborne Liquid air turbine
US2504320A (en) * 1945-02-26 1950-04-18 Lindberg Eng Co Method of and apparatus for forced convection heating
US2583430A (en) * 1945-05-17 1952-01-22 Nina K Guercken Power plant, including a combustion chamber and an impulse turbine driven by exhaustgases from the chamber
US2612022A (en) * 1945-12-07 1952-09-30 Joseph F Keys Internal-combustion engine with rotary constant volume combustion chamber
US2686631A (en) * 1948-05-08 1954-08-17 United Aircraft Corp Coolant injection system for gas turbines

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