GB562117A - Improvements in gas turbines - Google Patents

Improvements in gas turbines

Info

Publication number
GB562117A
GB562117A GB376843A GB376843A GB562117A GB 562117 A GB562117 A GB 562117A GB 376843 A GB376843 A GB 376843A GB 376843 A GB376843 A GB 376843A GB 562117 A GB562117 A GB 562117A
Authority
GB
United Kingdom
Prior art keywords
port
serrations
vanes
pocket
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
GB376843A
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 GB376843A priority Critical patent/GB562117A/en
Publication of GB562117A publication Critical patent/GB562117A/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
    • F02C5/06—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output

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

562,117. Turbines. CARTWRIGHT, W. March 9, 1943, No. 3768. [Classes 110 (ii) and 110 (iii)] The turbine rotor has two or more parallel sets of pockets F on its periphery and serrations I around the stator. Behind each pocket are two vanes C with a scavenging port B between them, the vanes being projected radially by centrifugal force. Working fluid is admitted through a port E and compressed through a crescent-shaped space D into a pocket F, fixed by a plug H and expanded until an exhaust port N is reached. The port B scavenges the serrations. It is sealed off while passing over the inlet E by a core A.
GB376843A 1943-03-09 1943-03-09 Improvements in gas turbines Expired GB562117A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB376843A GB562117A (en) 1943-03-09 1943-03-09 Improvements in gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB376843A GB562117A (en) 1943-03-09 1943-03-09 Improvements in gas turbines

Publications (1)

Publication Number Publication Date
GB562117A true GB562117A (en) 1944-06-19

Family

ID=9764568

Family Applications (1)

Application Number Title Priority Date Filing Date
GB376843A Expired GB562117A (en) 1943-03-09 1943-03-09 Improvements in gas turbines

Country Status (1)

Country Link
GB (1) GB562117A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2519700A1 (en) * 1981-10-21 1983-07-18 Lippis Mario Variable output turbine engine - has rotor defining triangular combustion chambers with inlet and exhaust orifices
GB2278646A (en) * 1993-03-01 1994-12-07 Howard Bidwell Turbine using i.c. engine exhaust gas

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2519700A1 (en) * 1981-10-21 1983-07-18 Lippis Mario Variable output turbine engine - has rotor defining triangular combustion chambers with inlet and exhaust orifices
GB2278646A (en) * 1993-03-01 1994-12-07 Howard Bidwell Turbine using i.c. engine exhaust gas

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