Blade tip seal insert

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between blade edge and static part

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Details

415200, F01D 1112

Patent

active

056224745

ABSTRACT:
Run-on linings for turbo-engines are arranged between the free ends of moving blades and a housing of a compressor or a turbine of a turbo-engine. The run-on linings are formed of a carrier and fiber bundles and are fastened on the circumference of the housing.

REFERENCES:
patent: 3808087 (1974-04-01), Milewski et al.
patent: 4273824 (1981-06-01), McComas et al.
patent: 4289447 (1981-09-01), Sterman et al.
patent: 5520508 (1996-05-01), Khalid

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