US 4,046,487 AGranted

Turbine blade indexing assembly

AssigneeTeledyne Industries, Inc.

InventorHerman N. Lenz

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Abstract

A turbine blade indexing assembly adapted for variably adjusting the pitch of the turbine blades in a turbine wheel. The indexing assembly includes a housing secured to a turbine hub and an indexing ring contained between the housing and the hub and adapted for limited rotational movement relative to the housing. A plurality of radial bores are formed around the periphery of the housing and each bore is adapted to receive a cylindrical shank of the turbine blade therethrough. A blade retainer ring, having a transverse bore adapted to register with a transverse bore formed through the turbine blade shank, is positioned on each turbine blade shank so that a pin member inserted through the registering bores in the shank and retainer ring rotatably secures the turbine blade to the housing. One end of the pin member is received in an actuator slot formed in the indexing ring so that rotational movement of the indexing ring produces a corresponding axial rotation of the turbine blades. At least one bolt is provided to secure the indexing ring to the housing in order to prevent further rotational movement of the indexing ring relative to the housing after the proper turbine blade pitch is obtained.

A device for testing the characteristics of a turbine assembly with the turbine blades adjusted through a wide range of pitches and with different numbers of turbine blades, said device comprising:

a turbine hub adapted to be rotated,
a housing provided with a plurality of circumferentially spaced radially extending bores, each of said bores having an inwardly extending shoulder portion intermediate the ends of said bores,
a plurality of turbine blades, each being provided with a shank portion adapted to be received within said bores with an end extending beyond said bore, said shank portion having an enlarged abutment surface which seats against said shoulder formed in said bore when said shank portion is inserted radially inwardly into one of said bores,
a retainer ring for each of said turbine blades, each of said retainer rings having an axial bore of substantially the same diameter as the end of said shank portion whereby said retainer ring will fit over the end of said shank portion,
said retainer rings and said ends of said shank portion each having a diametrical bore therethrough and a pin member receivable in said diametrical bores to thereby lock said ring member to said shank portion and thus said turbine blade to said housing,
said pin members each having a spherical head portion,
an indexing ring detachably mounted to said housing and provided with a plurality of actuator slots disposed to receive the head portions of said pin members,
means for selectively rotating said indexing ring to thereby move said head portions of said pin members whereby said turbine blades will be rotated about their axis to change the pitch thereof,
said housing with said turbine blades being detachably mounted to said hub whereby said housing and said turbine blades can be removed as a unit from said hub to permit individual removal of said turbine blades from said housing for replacement or testing purposes or to permit said housing to be replaced by a similar housing having different turbine blade spacings to thereby permit the testing of the effect of different blade spacings on the operation of said turbine assembly.

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Abstract

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