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GB2003553B - Gas reaction engine having a torque rotor driven fan or fans - Google Patents

Gas reaction engine having a torque rotor driven fan or fans

Info

Publication number
GB2003553B
GB2003553B GB7833039A GB7833039A GB2003553B GB 2003553 B GB2003553 B GB 2003553B GB 7833039 A GB7833039 A GB 7833039A GB 7833039 A GB7833039 A GB 7833039A GB 2003553 B GB2003553 B GB 2003553B
Authority
GB
United Kingdom
Prior art keywords
fans
gas reaction
driven fan
rotor driven
torque rotor
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
GB7833039A
Other versions
GB2003553A (en
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 GB7833039A priority Critical patent/GB2003553B/en
Publication of GB2003553A publication Critical patent/GB2003553A/en
Application granted granted Critical
Publication of GB2003553B publication Critical patent/GB2003553B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16Gas-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/005Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the engine comprising a rotor rotating under the actions of jets issuing from this rotor

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)
GB7833039A 1977-05-27 1978-08-11 Gas reaction engine having a torque rotor driven fan or fans Expired GB2003553B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7833039A GB2003553B (en) 1977-05-27 1978-08-11 Gas reaction engine having a torque rotor driven fan or fans

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB2244277 1977-05-27
GB7833039A GB2003553B (en) 1977-05-27 1978-08-11 Gas reaction engine having a torque rotor driven fan or fans

Publications (2)

Publication Number Publication Date
GB2003553A GB2003553A (en) 1979-03-14
GB2003553B true GB2003553B (en) 1982-04-07

Family

ID=26255920

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7833039A Expired GB2003553B (en) 1977-05-27 1978-08-11 Gas reaction engine having a torque rotor driven fan or fans

Country Status (1)

Country Link
GB (1) GB2003553B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102316629B1 (en) * 2020-06-23 2021-10-25 두산중공업 주식회사 Turbine blade tip clearance control apparatus and gas turbine comprising the same

Also Published As

Publication number Publication date
GB2003553A (en) 1979-03-14

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Legal Events

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