R
Roger John Myddelton Sills
Researcher at Rolls-Royce Limited
Publications - 1
Citations - 21
Roger John Myddelton Sills is an academic researcher from Rolls-Royce Limited. The author has contributed to research in topics: Tip clearance. The author has an hindex of 1, co-authored 1 publications receiving 21 citations.
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Gas turbine engines
TL;DR: A gas turbine engine blade tip seal consists of a sealing ring which is controlled by means of two annular control members as discussed by the authors, arranged such that one control member has a relatively rapid thermal response rate and the other control member had a relatively slow response rate, the sealing ring being controlled such that a preferred tip clearance is maintained under varying engine operating conditions.