GB1195220A - Multi-Stage Tangential Flow Turbines. - Google Patents

Multi-Stage Tangential Flow Turbines.

Info

Publication number
GB1195220A
GB1195220A GB5600867A GB5600867A GB1195220A GB 1195220 A GB1195220 A GB 1195220A GB 5600867 A GB5600867 A GB 5600867A GB 5600867 A GB5600867 A GB 5600867A GB 1195220 A GB1195220 A GB 1195220A
Authority
GB
United Kingdom
Prior art keywords
air
tangential flow
casing
inlet
outlet
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
GB5600867A
Inventor
Ferenc Toth
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 GB5600867A priority Critical patent/GB1195220A/en
Publication of GB1195220A publication Critical patent/GB1195220A/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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • F02C5/04—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

1,195,220. Air heaters. F. TOTH. 8 Dec., 1967, No. 56008/67. Heading F4S. [Also in Division F1] A heat exchanger for preheating combustion air in a gas turbine plant comprises a casing 87 containing tubes 83 through which the air passes from an inlet 29 to an outlet 32. Turbine exhaust gases enter the casing 87 through an inlet 31 and flow over the tubes 83 before leaving through an outlet 84. Non-return valves 85, 86 in the air and exhaust gas lines, respectively, prevent backflow.
GB5600867A 1967-12-08 1967-12-08 Multi-Stage Tangential Flow Turbines. Expired GB1195220A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB5600867A GB1195220A (en) 1967-12-08 1967-12-08 Multi-Stage Tangential Flow Turbines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5600867A GB1195220A (en) 1967-12-08 1967-12-08 Multi-Stage Tangential Flow Turbines.

Publications (1)

Publication Number Publication Date
GB1195220A true GB1195220A (en) 1970-06-17

Family

ID=10475502

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5600867A Expired GB1195220A (en) 1967-12-08 1967-12-08 Multi-Stage Tangential Flow Turbines.

Country Status (1)

Country Link
GB (1) GB1195220A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2350404A (en) * 1999-05-25 2000-11-29 David Johnathan Harris Rotary engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2350404A (en) * 1999-05-25 2000-11-29 David Johnathan Harris Rotary engine
GB2350404B (en) * 1999-05-25 2001-10-17 David Johnathan Harris Rotary engines

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Legal Events

Date Code Title Description
PS Patent sealed
435 Patent endorsed 'licences of right' on the date specified (sect. 35/1949)
PCNP Patent ceased through non-payment of renewal fee