TW221476B - Heat-recovering-thrust-turbine with rotational flow path - Google Patents

Heat-recovering-thrust-turbine with rotational flow path

Info

Publication number
TW221476B
TW221476B TW081103263A TW81103263A TW221476B TW 221476 B TW221476 B TW 221476B TW 081103263 A TW081103263 A TW 081103263A TW 81103263 A TW81103263 A TW 81103263A TW 221476 B TW221476 B TW 221476B
Authority
TW
Taiwan
Prior art keywords
turbine
thrust
flow path
recovering
heat
Prior art date
Application number
TW081103263A
Other languages
Chinese (zh)
Inventor
Dae-Sung Lee
Ho-Keun Shin
Original Assignee
Dae-Sung Lee
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 Dae-Sung Lee filed Critical Dae-Sung Lee
Application granted granted Critical
Publication of TW221476B publication Critical patent/TW221476B/en

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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module

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

A heat-recovering-thrust-turbine including the rotational flow path has been invented in present work. This thrust turbine consists of a rotating disc having unique shape and functions of compressor and turbine together, a combustion chamber, manifolds for heat recovering and a divergent nozzle having the curved flow path in a different way of conventional gas turbine engines utilizing a straight discharging mechanism of the exhaust gases. Thus, this invented thrust turbine is able to perform the combined function such as compression of air, cooling of the hot section, recovery of the wasted heats and generation of the thrust and the turbine power being used for the air compression, simultaneously.
TW081103263A 1990-10-27 1992-04-25 Heat-recovering-thrust-turbine with rotational flow path TW221476B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019900017297A KR960000484B1 (en) 1990-10-27 1990-10-27 Heat-recovering-thrust-turbine having rotational flow path

Publications (1)

Publication Number Publication Date
TW221476B true TW221476B (en) 1994-03-01

Family

ID=19305272

Family Applications (1)

Application Number Title Priority Date Filing Date
TW081103263A TW221476B (en) 1990-10-27 1992-04-25 Heat-recovering-thrust-turbine with rotational flow path

Country Status (2)

Country Link
KR (1) KR960000484B1 (en)
TW (1) TW221476B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100276916B1 (en) * 1995-12-07 2001-01-15 정몽규 Semi-automatic clutch for car

Also Published As

Publication number Publication date
KR920008329A (en) 1992-05-27
KR960000484B1 (en) 1996-01-08

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