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US 4,541,778 AGranted
Pin rooted blade biaxial air seal
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorJames D. Adams
Life of this patent
Estimating the term…
Abstract
In an axial flow compressor rotor stage having a blade mount rail about the eriphery thereof, a seal is positioned below the blade platforms to provide improved compressor gas path efficiency. Each blade platform has a seal bonded to the underside thereof, said seals extending toward adjacent blade platforms and providing sealing means in the interstices between said platforms as well as between said platforms and said blade mount rail.
Claims1
A rotor assembly comprising a rotor having a circumferential blade mount rail;
- a plurality of blades circumferentially spaced around the outer rim of said rotor leaving a slot between adjacent blades for the assembly, thermal expansion and efficient operation of said rotor assembly, each blade having a platform from which a pair of parallel, slotted roots circumferentially dimensioned less than said platform extend radially inward to straddle said rail and are secured thereto by a fastener that passes through said roots and said rail, wherein said roots join near said platform in an arcuate curve radially spaced from the perimeter of said rail;
- and an elastometric seal bonded to the radially inner surface of said platform and having first and second parallel sections in axial alignment with said rotor and joined by a third, crossbar, section perpendicular to said parallel sections and in radial contact with said rail, wherein the radial dimension of said seal is slightly greater than the separation of said platform from said rail so as to cause said seal to be compressed when said blade is secured to said rotor, the axial dimension of said crossbar section being approximately equal to the axial dimension of said rail and the combined circumferential dimensions of said crossbar section, and said first and second parallel sections being equal to said circumferential spacing between said blades, such that the length of said rail under each said blade is sealed to said blade by said crossbar section in cooperation with said parallel sections, and the slot between said circumferentially spaced blades is sealed by the abutting parallel sections of adjacent blades.
Dependencies are inferred from the claim text.