Patent ID: 11952909
Assignee: SAFRAN AIRCRAFT ENGINES
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  B | IPC B  F

Claim 2:
3. The installation for pre-assembling the turbine stators of a turbine according to claim 2, wherein the one of the at least one sector of the set of sectors comprises an inner platform, an outer platform, vanes each comprising a trailing edge and being attached between said inner platform and said outer platform, and a block of abradable honeycomb material extending inwardly of the inner platform between the side faces, and wherein the system for controlling the quality of the sector is configured to control the quality:
of the slots provided in the side faces of the one of the at least one sector of the set of sectors;
of the trailing edges and the surfaces of the vanes; and
of the block of abradable honeycomb material.