GB288929A - Improvements in and relating to gas turbines - Google Patents

Improvements in and relating to gas turbines

Info

Publication number
GB288929A
GB288929A GB3147527A GB3147527A GB288929A GB 288929 A GB288929 A GB 288929A GB 3147527 A GB3147527 A GB 3147527A GB 3147527 A GB3147527 A GB 3147527A GB 288929 A GB288929 A GB 288929A
Authority
GB
United Kingdom
Prior art keywords
rotor
chamber
perress
pockets
casing
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
GB3147527A
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.)
THOMAS EDWARD LAMB PERRESS
Original Assignee
THOMAS EDWARD LAMB PERRESS
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 THOMAS EDWARD LAMB PERRESS filed Critical THOMAS EDWARD LAMB PERRESS
Priority to GB3147527A priority Critical patent/GB288929A/en
Publication of GB288929A publication Critical patent/GB288929A/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

288,929. Perress, J. H. L., and Perress, T. E. L. Nov. 23, 1927. Working-fluid supply.-A gas turbine comprises a rotor 2 having blades 3 to the pockets between which gas is supplied under pressure from a chamber 11. The charges are exploded by a sparking plug 17, and react on fixed blades 13, and then pass to an exhaust 15. A vacuum chamber 16 is provided to draw any exhaust gases &c. carried round by the rotor. 'The pressure in the supply chamber 11, and the vacuum in the chamber 16 may be established by fans on the rotor shaft. According to the Provisional Specification, the rotor may be provided with pockets from which the remaining exhaust gases may be removed by a spring-controlled plate. Cooling parts.-The bottom of the casing 5 is formed as a sump containing cooling water or other liquid through which the rotor passes The water is circulated through a radiator, and the stationary vanes and casing may be jacketed or finned. Leakage-preventing devices.-The rim of the rotor 2 is formed with grooves 8 co-operating with ribs of anti-friction metal or asbestos on the fixed segmental part 6, and packing pieces 10 of part-circle shape are arranged on each side of the chambers 11, 16.
GB3147527A 1927-11-23 1927-11-23 Improvements in and relating to gas turbines Expired GB288929A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3147527A GB288929A (en) 1927-11-23 1927-11-23 Improvements in and relating to gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3147527A GB288929A (en) 1927-11-23 1927-11-23 Improvements in and relating to gas turbines

Publications (1)

Publication Number Publication Date
GB288929A true GB288929A (en) 1928-04-19

Family

ID=10323633

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3147527A Expired GB288929A (en) 1927-11-23 1927-11-23 Improvements in and relating to gas turbines

Country Status (1)

Country Link
GB (1) GB288929A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2444213A (en) * 1944-10-17 1948-06-29 Harvey B Weeks Rotary turbine
GB2305471A (en) * 1995-09-23 1997-04-09 James Linton Intermittant-combustion turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2444213A (en) * 1944-10-17 1948-06-29 Harvey B Weeks Rotary turbine
GB2305471A (en) * 1995-09-23 1997-04-09 James Linton Intermittant-combustion turbine engine

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