Invention Application
US20160363004A1 INNER DIAMETER SCALLOP CASE FLANGE FOR A CASE OF A GAS TURBINE ENGINE 有权
用于气体涡轮发动机的内径直径的SCALLOP壳法兰

INNER DIAMETER SCALLOP CASE FLANGE FOR A CASE OF A GAS TURBINE ENGINE
Abstract:
A case for a gas turbine engine incudes a radial flange with a partial scallop along an inner diameter of the radial flange. A case assembly for a gas turbine engine incudes a first case with an a first radial flange with a partial scallop along an inner diameter of the first radial flange, the partial scallop adjacent to a first aperture thorough the first radial flange and a second case with an a second radial flange with a second aperture thorough the second radial flange the second radial flange mountable to the first radial flange at an interface such that the second aperture is axially aligned with the first aperture and a seal lip that extends from the second case interfaces with said first case at a longitudinal interface
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