GB2216956B - An arrangement comprising a rotary motor,an air compressor,and a gas turbine - Google Patents

An arrangement comprising a rotary motor,an air compressor,and a gas turbine

Info

Publication number
GB2216956B
GB2216956B GB8906061A GB8906061A GB2216956B GB 2216956 B GB2216956 B GB 2216956B GB 8906061 A GB8906061 A GB 8906061A GB 8906061 A GB8906061 A GB 8906061A GB 2216956 B GB2216956 B GB 2216956B
Authority
GB
United Kingdom
Prior art keywords
arrangement
gas turbine
air compressor
rotary motor
rotary
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 - Lifetime
Application number
GB8906061A
Other versions
GB8906061D0 (en
GB2216956A (en
Inventor
Johs Ellingsen
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
Publication of GB8906061D0 publication Critical patent/GB8906061D0/en
Publication of GB2216956A publication Critical patent/GB2216956A/en
Application granted granted Critical
Publication of GB2216956B publication Critical patent/GB2216956B/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
GB8906061A 1988-03-17 1989-03-16 An arrangement comprising a rotary motor,an air compressor,and a gas turbine Expired - Lifetime GB2216956B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NO881173A NO170645C (en) 1988-03-17 1988-03-17 ENGINE ARRANGEMENT INCLUDING A COMPRESSOR AIR COMPRESSOR, A COMBUSTION ENGINE AND A GAS TURBINE

Publications (3)

Publication Number Publication Date
GB8906061D0 GB8906061D0 (en) 1989-04-26
GB2216956A GB2216956A (en) 1989-10-18
GB2216956B true GB2216956B (en) 1992-08-26

Family

ID=19890742

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8906061A Expired - Lifetime GB2216956B (en) 1988-03-17 1989-03-16 An arrangement comprising a rotary motor,an air compressor,and a gas turbine

Country Status (2)

Country Link
GB (1) GB2216956B (en)
NO (1) NO170645C (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2393363C1 (en) * 2009-03-03 2010-06-27 Николай Петрович Генералов Gas turbine engine
RU2463464C1 (en) * 2011-03-24 2012-10-10 Колобанова Галина Николаевна Gas turbine engine
CN114307259B (en) * 2021-12-30 2023-05-30 中国航空工业集团公司金城南京机电液压工程研究中心 Pump type oil-gas separator of hydraulic combined transmission generator

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB496342A (en) * 1937-01-27 1938-11-29 Dimitri Sensaud De Lavaud Improvements in rotary motors and compressors

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB496342A (en) * 1937-01-27 1938-11-29 Dimitri Sensaud De Lavaud Improvements in rotary motors and compressors

Also Published As

Publication number Publication date
NO881173D0 (en) 1988-03-17
NO170645C (en) 1992-11-11
NO881173L (en) 1989-09-18
GB8906061D0 (en) 1989-04-26
GB2216956A (en) 1989-10-18
NO170645B (en) 1992-08-03

Similar Documents

Publication Publication Date Title
EP0468782A3 (en) Gas turbine rotor and operation thereof
GB2220711B (en) Stator assembly for a gas turbine engine
EP0348936A3 (en) A scroll gas compressor
GB2218741B (en) Gas turbine engine
GB2233394B (en) A gas turbine engine rotor assembly
AU4864290A (en) Gas turbine with air-cooled vanes
AU4236689A (en) Gas compressor having dry gas seals
GB9405473D0 (en) A gas turbine engine fan blade assembly
GB9126187D0 (en) Air cooled gas turbine engine aerofoil
GB2226854B (en) Jet engine fan and compressor bearing support
GB9412963D0 (en) Gas turbine engine fan blade assembly
GB9615826D0 (en) Gas turbine engine fan blade retention
GB8914825D0 (en) Gas turbine engine power unit
GB8917938D0 (en) Gas compressor
GB2216956B (en) An arrangement comprising a rotary motor,an air compressor,and a gas turbine
GB8830151D0 (en) Gas turbine engine
GB2176539B (en) Turbine engine including a centrifugal compressor diffuser structure
GB9206404D0 (en) Bladed rotor for a gas turbine engine
GB9405851D0 (en) Gas turbine engine fan blade retention
GB8806739D0 (en) Air turbine
GB2257751B (en) Rotary vane gas compressors
GB8904478D0 (en) Gas turbine engine air intake
GB8907885D0 (en) A gas turbine engine rotor assembly and a gas turbine engine rotor blade
GB9207110D0 (en) A rotor and a rotor blade for a gas turbine engine
AU105173S (en) Three bladed air rotor

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19960316