Spacing arrangement

Rotary kinetic fluid motors or pumps – Runner or blade selectively adjustable relative to casing – Axially adjusted

Reexamination Certificate

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C415S174100, C415S173200

Reexamination Certificate

active

11106621

ABSTRACT:
A spacing arrangement for a gas turbine engine10.The spacing arrangement being arranged such that as a rotor blade26of a compressor13rotates, the rotor disc28will move outwards and forwards to maintain a substantially constant gap36between the rotor blade26and an inclined casing20.

REFERENCES:
patent: 6607350 (2003-08-01), Dodd
patent: 6676372 (2004-01-01), Scholz et al.
patent: 2002/0150469 (2002-10-01), Bolms
patent: 2 129 880 (1984-05-01), None
patent: 2 371 093 (2002-07-01), None
patent: 57195803 (1982-12-01), None
patent: WO 99/28598 (1999-06-01), None

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