GB613187A - Thermal power plant - Google Patents

Thermal power plant

Info

Publication number
GB613187A
GB613187A GB17950/46A GB1795046A GB613187A GB 613187 A GB613187 A GB 613187A GB 17950/46 A GB17950/46 A GB 17950/46A GB 1795046 A GB1795046 A GB 1795046A GB 613187 A GB613187 A GB 613187A
Authority
GB
United Kingdom
Prior art keywords
exchanger
heat
june
compressor
turbine
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
GB17950/46A
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.)
Aktiengesellschaft fuer Technische Studien
Original Assignee
Aktiengesellschaft fuer Technische Studien
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 Aktiengesellschaft fuer Technische Studien filed Critical Aktiengesellschaft fuer Technische Studien
Publication of GB613187A publication Critical patent/GB613187A/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
    • F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
    • F02C1/10—Closed cycles

Abstract

613,187. Air turbines. AKT.-GES. FUR TECHNISCHE STUDIEN. June 14, 1946, No. 17950. Convention date, June 22, 1945. [Class 110 (iii)] In a turbine plant in which the air or other working medium circulates in a closed circuit, the heat-exchanger 7 is built directly on to the exhaust side of the low-pressure turbine stage 3 and, preferably, the compressor 4 is also, at its inlet side, built directly on to the heatexchanger. The turbine exhaust passage merges without much change of area into a diffusor 6 before the heat-exchanger and the delivery from the heat-exchanger, after passing a cooler 9, is speeded up in a nozzle-like part 71 before the compressor. In a modification the heater may be in two parallel connected parts or may be U-shaped. One bearing for the low-pressure turbine may be in the diffuser 6.
GB17950/46A 1945-06-22 1946-06-14 Thermal power plant Expired GB613187A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH613187X 1945-06-22

Publications (1)

Publication Number Publication Date
GB613187A true GB613187A (en) 1948-11-23

Family

ID=4523537

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17950/46A Expired GB613187A (en) 1945-06-22 1946-06-14 Thermal power plant

Country Status (1)

Country Link
GB (1) GB613187A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2858666A (en) * 1954-01-25 1958-11-04 Cooper Bessemer Corp Turbocharging of two-cycle engines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2858666A (en) * 1954-01-25 1958-11-04 Cooper Bessemer Corp Turbocharging of two-cycle engines

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