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Platform for a swing root turbomachinery bladeA rotor apparatus, comprising a blade having a root adapted to swing laterally within a supporting spindle under impact loading, is provided with a flow path defining platform. The platform comprises an inner shroud extending generally laterally of the blade airfoil portion and adapted to swing laterally. In one embodiment, wherein the blade primarily comprises a laminate of composite filament plies, the inner shroud is bonded to the laminate. An outer shroud, fixed with respect to the supporting spindle, forms a lateral extension of the inner shroud with the blade in its normal operating position. The inner and outer shrouds are provided with a pair of complementary adjacent surfaces contoured to pass in relatively close-fitting relationships to each other when the blade swings under impact loadings.
Document ID
19770025204
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Ravenhall, R.
(GE Cincinnati, United States)
Date Acquired
September 3, 2013
Publication Date
August 30, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: NASA-CASE-LEW-12312-1
Patent Application Number: US-PATENT-APPL-SN-654787
Patent Number: US-PATENT-4,045,149
Accession Number
77N32148
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-12312-1|US-PATENT-4,045,149
Patent Application
US-PATENT-APPL-SN-654787
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