Exhaust nozzle center body attachment
AssigneeRohr, Inc.
InventorsJacques Jinqiu Lu, Chad Franks, Richard S. Alloway
Life of this patent
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Abstract
A ceramic turbine engine exhaust component, such as a ceramic matrix composite (“CMC”) exhaust center body may be positioned around a metallic attachment ring. The attachment ring may have a greater coefficient of thermal expansion than the CMC center body. A plurality of bolts radially-spaced around the circumference of the attachment ring may be inserted through apertures in the center body with a sliding fit, and may be coupled to the attachment ring. The bolts may slide within the apertures, allowing the attachment ring to thermally expand without applying extra loads on the exhaust center body due to the expansion.
Claims14
A mechanical attachment system for an exhaust component of a turbine engine comprising:
- the exhaust component constituting either a nozzle or a center body and comprising a housing, the housing comprising an aperture;
- a bushing inserted at least partially within the aperture;
- an attachment ring;
- and
- a bolt configured to be inserted at least partially within the bushing and forming a sliding fit therewith, and the bolt is coupled to the attachment ring, wherein a head of the bolt is in contact with the attachment ring, wherein the head of the bolt is contained within a cylinder formed by the bushing and the head of the bolt is recessed within the cylinder.
A mechanical attachment system for an exhaust component of a turbine propulsion engine of an aircraft, the system comprising:
- the exhaust component constituting either a nozzle or a center body and formed from a material have a first coefficient of thermal expansion, the exhaust component comprising a cylindrical housing, the cylindrical housing comprising a plurality of radially-spaced apertures around its circumference;
- a plurality of metallic bushings, one inserted at least partially within each of the plurality of radially-spaced apertures;
- a metallic attachment ring configured to be attached to the turbine propulsion engine and formed from a metallic material having a second coefficient of thermal expansion which is greater than the first coefficient of thermal expansion;
- and
- a plurality of bolts, one inserted at least partially within each of each of the plurality of metallic bushings and forming a sliding fit therewith, the plurality of bolts each coupled to the metallic attachment ring, wherein each of the plurality of bolts comprises a head in contact with the metallic attachment ring, wherein the head of each of the plurality of bolts is contained within a cylinder formed by each of the plurality of metallic bushings and the head of the bolt is recessed within the cylinder.
Dependencies are inferred from the claim text.