GB190915565A - Improvements in Gas Turbines. - Google Patents

Improvements in Gas Turbines.

Info

Publication number
GB190915565A
GB190915565A GB190915565DA GB190915565A GB 190915565 A GB190915565 A GB 190915565A GB 190915565D A GB190915565D A GB 190915565DA GB 190915565 A GB190915565 A GB 190915565A
Authority
GB
United Kingdom
Prior art keywords
valves
air
cooling
turbine
gas
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
Inventor
Hans Holzwarth
Erhard Junghans
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
Application granted granted Critical
Publication of GB190915565A publication Critical patent/GB190915565A/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)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

15,565. Holzwarth, H., and Junghans, E. July 3. Working-fluid supply; cooling and heating parts; nozzles. - A gas turbine comprises two main parts, a base-portion I containing the air, gas, and combustion chambers, the valves, and the lower bearing, and an upper portion II containing the turbine proper. A series of combustion chambers 8, are supplied through suitable valves (not shown) with gas and air from channels 13, 12 respectively. Valves 10, with water - jacketed casings 3, control the admission of combustion products to nozzles 9, situated in a removable ring 11. These valves, together with their casings, are easily removable for inspection. The turbine is arranged on a vertical shaft and is enclosed in a waterjacketed casing 7, the lower part of the casing forming a part of the base portion II. When the temperature of the exhaust exceeds a predetermined limit, a thermostat 34 excites solenoids 56, which operate armatures 57 attached to valves 31, whereby air is admitted direct from the air chamber 12 to the turbine blades for cooling. The form of thermostat may he varied, and it may be operated by the temperature of the cooling-water. The interior of the base-portion may be packed with heatinsulating material 6.
GB190915565D 1909-07-03 1909-07-03 Improvements in Gas Turbines. Expired GB190915565A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190915565T 1909-07-03

Publications (1)

Publication Number Publication Date
GB190915565A true GB190915565A (en) 1910-07-04

Family

ID=32556530

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190915565D Expired GB190915565A (en) 1909-07-03 1909-07-03 Improvements in Gas Turbines.

Country Status (1)

Country Link
GB (1) GB190915565A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2940257A (en) * 1953-03-27 1960-06-14 Daimler Benz Ag Cooling arrangement for a combustion turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2940257A (en) * 1953-03-27 1960-06-14 Daimler Benz Ag Cooling arrangement for a combustion turbine

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