GB2009855B - Jetshaft power plant - Google Patents

Jetshaft power plant

Info

Publication number
GB2009855B
GB2009855B GB7844478A GB7844478A GB2009855B GB 2009855 B GB2009855 B GB 2009855B GB 7844478 A GB7844478 A GB 7844478A GB 7844478 A GB7844478 A GB 7844478A GB 2009855 B GB2009855 B GB 2009855B
Authority
GB
United Kingdom
Prior art keywords
jetshaft
power plant
plant
power
jetshaft power
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
GB7844478A
Other versions
GB2009855A (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 GB7844478A priority Critical patent/GB2009855B/en
Publication of GB2009855A publication Critical patent/GB2009855A/en
Application granted granted Critical
Publication of GB2009855B publication Critical patent/GB2009855B/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
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines
    • 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
    • F02C3/165Gas-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)
  • Engine Equipment That Uses Special Cycles (AREA)
GB7844478A 1977-08-16 1978-11-14 Jetshaft power plant Expired GB2009855B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7844478A GB2009855B (en) 1977-08-16 1978-11-14 Jetshaft power plant

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB3426077 1977-08-16
GB7844478A GB2009855B (en) 1977-08-16 1978-11-14 Jetshaft power plant

Publications (2)

Publication Number Publication Date
GB2009855A GB2009855A (en) 1979-06-20
GB2009855B true GB2009855B (en) 1982-02-24

Family

ID=26262217

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7844478A Expired GB2009855B (en) 1977-08-16 1978-11-14 Jetshaft power plant

Country Status (1)

Country Link
GB (1) GB2009855B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2169034A (en) * 1984-12-20 1986-07-02 Taha Khalil Aldoss Jet engine having ramjet driven compressor
FR2680385A1 (en) * 1991-08-12 1993-02-19 Rignault Jean Turbine engine with orthogonal circular reaction
WO2008140433A2 (en) * 2007-05-15 2008-11-20 Ahmet Kaan Onay Turbo cyclic integral impulsion motor
EP2220354A1 (en) * 2007-11-27 2010-08-25 Schneiderbauer-Schwendler, Enno Drive device with compression modification in the form of a thermal rotary engine with internal combustion

Also Published As

Publication number Publication date
GB2009855A (en) 1979-06-20

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Legal Events

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