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Expired Canadian patentCanada

Active clearance control system for a turbomachine

CA 1159660 A · Owner: General Electric Company · Inventors: Knapp, Malcolm H.; Coulson, Charles E.; Johnston, Richard P.

CIPO record

Overview

Drawings and full text

Its claims, description and drawings are in the Canadian Patents Database.

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Abstract From the Canadian patent

An axial compressor is provided with a cooling air manifold surrounding a portion of the shroud and means, for bleeding air from the compressor to the manifold for selectively flowing it in a modulating manner axially along the outer side of the stator/shroud to cool and shrink it during steady-state operating conditions so as to obtain minimum shroud/rotor clearance conditions. Provision is also made to selectively divert the flow of cooling air from the manifold during transient periods of operation so as to alter the thermal growth or shrink rate of the stator/shroud and result in adequate clearance with the compressor rotor.

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Listed from its CIPO record in Patent Yard's archive of Canadian patents past their term. Its claims, description and drawings are in the CIPO record and on Google Patents, and the Claude kit works from them.

Why it's free to use

  • Granted January 3, 1984. A Canadian patent filed before October 1, 1989 lasted 17 years from grant, so its term ended January 3, 2001.
  • We check Canadian rights only. A patent in its family in another country could still be in force: check its family on Google Patents.
FiledJuly 18, 1980
GrantedJanuary 3, 1984
Term endedJanuary 3, 2001
Patent numberCA 1159660 A
Classification (IPC)F02K99/00 +2 more

Timeline

Timeline From CIPO dates

1981198419871990199319961999Application filedJuly 18, 1980Patent grantedJan 3, 1984Term endedJan 3, 2001

Sources & verification

Everything on this page comes from the CIPO record linked above. Contains information licensed under the Open Government Licence – Canada.