Title:
GAS TURBINE INCLUDING BLADE TIP GAP ADJUSTING MEANS AND CONTROL METHOD THEREFOR
Document Type and Number:
WIPO Patent Application WO/2015/108340
Kind Code:
A1
Abstract:
The present invention relates to: a gas turbine having a rotor shaft, which is movable in the direction of a rotation shaft, for adjusting a turbine blade front end gap, and having a blade vane carrier, which is movable in the direction of the rotation shaft, for adjusting a compressor blade front end gap when the rotor shaft moves, thereby enabling the active adjustment of the compressor blade front end gap; and a control method therefor.
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Inventors:
KIM HYUNG YOON (KR)
Application Number:
PCT/KR2015/000398
Publication Date:
July 23, 2015
Filing Date:
January 14, 2015
Export Citation:
Assignee:
DOOSAN HEAVY IND CONSTR CO LTD (KR)
International Classes:
F02C9/22; F01D17/16
Foreign References:
JP2003314209A | 2003-11-06 | |||
JP2006189048A | 2006-07-20 | |||
JP2736345B2 | 1998-04-02 | |||
US5263816A | 1993-11-23 |
Attorney, Agent or Firm:
HONESTY & JR PARTNERS INTELLECTUAL PROPERTY LAW GROUP (KR)
특허법인 정안 (KR)
특허법인 정안 (KR)
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