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ISLN:
903164908
Admitted:
1975
University:
Stanford University, B.A., 1972
Law School:
Willamette University, J.D., 1975
Us Patents
Turbine Shroud Segment With Serpentine Cooling Channels
Ralph J. Thompson - Tolland CT Daniel E. Kane - Tolland CT
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F01D 2512
US Classification:
4151731
Abstract:
A turbine shroud segment for use in a gas turbine engine includes a serpentine channel along at least one axial edge of the segment. Various construction details are developed that disclose a channel for efficiently flowing cooling fluid through an axial edge of a shroud segment. In a particular embodiment, a turbine shroud segment includes a leading edge serpentine channel and a trailing edge serpentine channel. Both serpentine channels include ducts that extend to the serpentine channels from a point inward of adjacent retaining hooks. Cooling fluid flowing onto the outward surface of the segments flows through the ducts and along the serpentine channels to cool the leading and trailing edges of the segments.
A shroud segment for a gas turbine engine includes a hook having an undercut surface. Various construction details are developed that provide a segment having a hook with minimized bending stress. In a particular embodiment, a shroud segment includes a plurality of hooks spaced along the leading and trailing edges of the shroud segment. Each of the plurality of hooks includes a positioning surface, a support surface and an undercut surface therebetween. The positioning surface defines the limits of axial movement of the shroud segment. The support surface reacts the radial loading on the shroud segment during operation of the gas turbine engine. The undercut surface is offset from the stator assembly to define the maximum length of the support surface.
Turbine Shroud Segment With Serpentine Cooling Channels Having A Bend Passage
Ralph J. Thompson - Tolland CT Daniel E. Kane - Tolland CT Robert W. Sunshine - Hobe Sound FL
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F01D 2512
US Classification:
415115
Abstract:
A turbine shroud segment for use in a gas turbine engine includes a serpentine channel along at least one axial edge of the segment. Various construction details are developed that disclose a channel for efficiently flowing cooling fluid through an axial edge of a shroud segment. In a particular embodiment, a turbine shroud segment includes a leading edge serpentine channel having a bend passage which includes a purge hole to avoid separating flow in the bend passage.
father of slain hatchet loon Zale Thompson, 32, told The Post Saturday. I think he committed suicide and he was taking one of yall with him, his father, Ralph Thompson, said, speaking through the screen door of the two-story Queens Village house where his unhinged son also once lived.
UtahPresident at Novus Promotions, LLC hard to read, easy going until sufficiently abused or taken advantage of. Pessimistically optimistic. My only kryptonite is negativity, I find it toxic.