Rotor blade having a tip cap end closure

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

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416232, 291568H, 291568B, F01D 518

Patent

active

045898243

ABSTRACT:
An airfoil structure for use in an axial flow turbomachine is disclosed. Various construction details which improve the durability, integrity and the cooling effectiveness of the structure are shown and a method for fabricating the structure is developed. The tip of the structure is closed by a tip cap, and in one embodiment, a ductile material is deposited between the tip of the structure and the tip cap to prevent the leakage of cooling medium.

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patent: 4010531 (1977-03-01), Anderson et al.
patent: 4048682 (1977-09-01), Smith
patent: 4073599 (1978-02-01), Allen et al.

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