Title:
FASTENING ELEMENT FOR A GUIDE BLADE RING OF A TURBOMACHINE
Document Type and Number:
WIPO Patent Application WO/2011/018072
Kind Code:
A3
Abstract:
The invention relates to a turbomachine (10), in particular a gas turbine, comprising a housing (22) and a guide blade ring (12), the outer shroud (16) of which is divided into segments (14) by joints, characterized in that the outer shroud (16) is fastened to the housing (22) by means of a first fastening element (30) for absorbing axial force and a second fastening element (24) independent of the first fastening element (30) for absorbing circumferential force, the first and the second fastening elements (24, 30) enabling play in the radial direction for the segments (14) of the outer shroud (16).
Inventors:
WEIDMANN WILFRIED (DE)
Application Number:
PCT/DE2010/000927
Publication Date:
September 15, 2011
Filing Date:
August 05, 2010
Export Citation:
Assignee:
MTU AERO ENGINES GMBH (DE)
WEIDMANN WILFRIED (DE)
WEIDMANN WILFRIED (DE)
International Classes:
F01D9/04; F01D25/24
Foreign References:
| US4492517A | 1985-01-08 | |||
| US2903237A | 1959-09-08 | |||
| FR1547844A | 1968-11-29 | |||
| EP0616111A1 | 1994-09-21 | |||
| EP0937864A2 | 1999-08-25 | |||
| EP1939404A2 | 2008-07-02 |
Download PDF:
Previous Patent: CONVEYED-GOODS DISTRIBUTOR
Next Patent: VALVE TRAIN FOR INTERNAL COMBUSTION ENGINES FOR ACTUATING GAS EXCHANGE VALVES
Next Patent: VALVE TRAIN FOR INTERNAL COMBUSTION ENGINES FOR ACTUATING GAS EXCHANGE VALVES