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
GB25078/39A
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.)
British Thomson Houston Co Ltd
Original Assignee
British Thomson Houston Co Ltd
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 British Thomson Houston Co LtdfiledCriticalBritish Thomson Houston Co Ltd
Publication of GB532491ApublicationCriticalpatent/GB532491A/en
532,491. Gas turbines. BRITISH THOMSONHOUSTON CO., Ltd. Sept. 1, 1939, No. 25078. Convention date, Sept. 3, 1938. [Class 110 (iii)] A turbine 15 drives an electric generator 12 and is driven by the exhaust gases of an I.C. aeroplane or other engine which are admittted at 17. The gases are led to a nozzle segment 22 by an open passage 25 to the right of a partition 21 and to the rest 23 of the nozzle annulus by a passage 24 provided with a valve 26. A passage 18 provided with a valve 19 leads to waste. The valves are controlled by a speedgovernor 27 through pressure oil, operating devices 30, 32, a lever 36 pivoted at 37 and a floating lever 38. The latter is biassed by a spring 43 so that on diminished speed the valve 19 is closed before the closing of the valve 26 commences.
GB25078/39A1938-09-031939-09-01Improvements in and relating to governing mechanisms for turbines
ExpiredGB532491A
(en)