GB382547A - Improvements in turbines for hot driving medium - Google Patents

Improvements in turbines for hot driving medium

Info

Publication number
GB382547A
GB382547A GB10318/32A GB1031832A GB382547A GB 382547 A GB382547 A GB 382547A GB 10318/32 A GB10318/32 A GB 10318/32A GB 1031832 A GB1031832 A GB 1031832A GB 382547 A GB382547 A GB 382547A
Authority
GB
United Kingdom
Prior art keywords
parts
heated
turbine
pipe
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
GB10318/32A
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.)
Milo AB
Original Assignee
Milo AB
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 Milo AB filed Critical Milo AB
Publication of GB382547A publication Critical patent/GB382547A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
    • F01D1/28—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like traversed by the working-fluid substantially radially
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/005—Selecting particular materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/14—Casings modified therefor
    • 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

Abstract

382,547. Gas &c. turbines. AKTIEBOLAGET MILO, 32, Kungsgatan, Stockholm. April 11, 1932, No. 10318. Convention date, Sept. 14, 1931. [Class 110 (iii).] In a gas turbine a portion of the driving medium, which is not heated, is used to cool exposed parts and is then mixed with the other portion for use in the turbine. In Fig. 1 the air supply is divided into two parts the first of which is heated in a pipe 15 by fuel from a pipe 18 and then passes by distributing chambers 11, 12 to a turbine 6 of radial-flow type having oppositely-running rotors. The cooler second part passes by the outer pipe 16 to cooling spaces 19 after which it mixes with the heated air. Blades 25, 26 deflect cooling air upon the bond rings, and holes 28 admit it to the central parts. The arrangement at the centre may be modified. The distributing chambers 11, 12 are movably mounted on bolts 13. Different gases may be used for the two purposes. Certain parts may be made of a siliconchromium-aluminium alloy.
GB10318/32A 1931-09-14 1932-04-11 Improvements in turbines for hot driving medium Expired GB382547A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE382547X 1931-09-14

Publications (1)

Publication Number Publication Date
GB382547A true GB382547A (en) 1932-10-27

Family

ID=6359644

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10318/32A Expired GB382547A (en) 1931-09-14 1932-04-11 Improvements in turbines for hot driving medium

Country Status (4)

Country Link
US (1) US2066788A (en)
FR (1) FR742787A (en)
GB (1) GB382547A (en)
NL (1) NL34915C (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE767491C (en) * 1935-12-09 1952-09-08 Anxionnaz Rene Thermal power plant with gas turbines with constant pressure combustion
US2439473A (en) * 1943-05-11 1948-04-13 United Aireraft Corp Pressurized protective conduit for hot gas power plants
US2458066A (en) * 1944-07-20 1949-01-04 American Locomotive Co Combustion chamber
US2608057A (en) * 1949-12-24 1952-08-26 A V Roe Canada Ltd Gas turbine nozzle box
US2743579A (en) * 1950-11-02 1956-05-01 Gen Motors Corp Gas turbine engine with turbine nozzle cooled by combustion chamber jacket air
US2873909A (en) * 1954-10-26 1959-02-17 Svenska Rotor Maskiner Ab Rotary devices and casing structures therefor
LU91970B1 (en) 2012-04-03 2013-10-04 Equitherm S A R L Turbine

Also Published As

Publication number Publication date
NL34915C (en)
US2066788A (en) 1937-01-05
FR742787A (en) 1933-03-15

Similar Documents

Publication Publication Date Title
GB585334A (en) Improvements in or relating to internal-combustion turbines
GB554112A (en) Method and device for cooling combustion chambers, particularly for gas turbines or the like
GB811393A (en) Improvements in and relating to gas turbine plants
GB382547A (en) Improvements in turbines for hot driving medium
GB196452A (en) Improvements in or relating to internal combustion turbine engines
GB452412A (en) Improvements relating to apparatus for cooling the rotors of turbines
GB569158A (en) Improvements in or relating to gas-turbine plants
US2109997A (en) Gas turbine driven supercharger
GB368318A (en) Improvements in or relating to turbines
GB439773A (en) Improvements in steam and gas turbines
GB586552A (en) Improvements in or relating to internal combustion turbine plant
GB432652A (en) Improved constant pressure gas turbine plant
GB546275A (en) Heat power plant for gaseous working media
GB502727A (en) Improvements in and relating to the charging of internal combustion engines
GB1066678A (en) A rotor for use in a gas turbine engine
GB765225A (en) Improvements in and relating to the cooling of gas turbine blades and rotors
GB372377A (en) Improvements in or relating to turbines
GB678736A (en) Improvements in or relating to storage apparatus for hot gas
GB698907A (en) An improved gas turbine with liquid-cooled rotor blades
GB375643A (en) Improvements in and relating to combustion turbines
GB586602A (en) Improvements in regenerative gas turbine plants
GB469311A (en) Improvements in and relating to gas turbine plant
GB791917A (en) Improvements in and relating to gas turbine plants
GB811434A (en) Improvements in or relating to regenerative heat exchangers
GB524694A (en) Improvements in and relating to the operation of metal air heaters and similar heat exchangers