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
GB11959/32A
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.)
Milo AB
Original Assignee
Milo AB
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 Milo ABfiledCriticalMilo AB
Publication of GB372407ApublicationCriticalpatent/GB372407A/en
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
F02C3/36—Open cycles
Abstract
372,407. Gas turbine plant. AKTIEBOLAGET MILO, 17, Vastra Tradgardsgatan, Stockholm. Nov. 4, 1930, No. 11959/32. Convention date, March 24,1930. Divided on 372,377. Drawings to Specification. [Class 110 (iii).] A gas turbine plant comprises air compressors, means for heating the, compressed air at constant pressure to a temperature above 800‹ C., and one cr more turbines having a thermo-dynamic efficiency of. not less than 80 per cent. The apparatus illustrated is that described in Specifications 368,317, 368,318 and 368,702.
GB11959/32A1930-03-241930-11-04Improvements in or relating to turbines
ExpiredGB372407A
(en)
Arrangement for starting up thermal power plants in which a gaseous working medium continuously describes a closed cycle under a pressure above atmospheric