Rotary kinetic fluid motors or pumps – With diversely oriented inlet or additional inlet for...
Patent
1980-02-22
1982-03-02
Hart, Douglas
Rotary kinetic fluid motors or pumps
With diversely oriented inlet or additional inlet for...
415117, 415134, 415172A, 415178, F01D 1108
Patent
active
043176461
ABSTRACT:
A device for controlling the clearance between the blade tips of a gas turbine engine turbine rotor and associated segmented shrouds comprises a control ring which is secured to the engine casing by a plurality of dowels. The control ring is supplied with cooling fluid to its hollow interior and is covered with a thermally insulating layer, whereby the rate of movement of the shroud segments can be maintained substantially equal to that of the adjacent turbine rotor.
REFERENCES:
patent: 2863634 (1958-12-01), Chamberlain
patent: 3583824 (1971-06-01), Smuland
patent: 3825364 (1974-07-01), Halila
patent: 3864056 (1975-02-01), Gabriel
patent: 4251185 (1981-02-01), Karstensen
Hooke Noel H.
Pask George
Steel Thomas
Hart Douglas
Rolls-Royce Limited
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