GB162644A - Arrangement of the explosion chambers in gas turbines - Google Patents

Arrangement of the explosion chambers in gas turbines

Info

Publication number
GB162644A
GB162644A GB867721A GB867721A GB162644A GB 162644 A GB162644 A GB 162644A GB 867721 A GB867721 A GB 867721A GB 867721 A GB867721 A GB 867721A GB 162644 A GB162644 A GB 162644A
Authority
GB
United Kingdom
Prior art keywords
inlet valve
arrangement
chambers
explosion
gas 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
GB867721A
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
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of GB162644A publication Critical patent/GB162644A/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
    • F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

162,644. Holzwarth, H. April 29, 1920, [Convention date]. Mounting and supporting working-fluid supply. -The explosion chambers a of a gas turbine are rigidly connected to the nozzle valve chamber b and to the inlet valve casing c. The inlet valve casing c moves freely in the inlet valve ring f to allow for expansion, and is provided with packing; g, h are air and fuel supply chambers, and d, e the air and fuel inlet valves. Water cooling may be employed for the explosion chamber and for the nozzle and inlet valve casings.
GB867721A 1921-03-21 Arrangement of the explosion chambers in gas turbines Expired GB162644A (en)

Publications (1)

Publication Number Publication Date
GB162644A true GB162644A (en) 1921-07-21

Family

ID=1629437

Family Applications (1)

Application Number Title Priority Date Filing Date
GB867721A Expired GB162644A (en) 1921-03-21 Arrangement of the explosion chambers in gas turbines

Country Status (1)

Country Link
GB (1) GB162644A (en)

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