Exhaust nozzle center body attachment

Patent metadata

Field	Value
Publication number	US-9784215-B2
Application number	US-201414536273-A
Country	US
Kind code	B2
Filing date	Nov 7, 2014
Priority date	Nov 7, 2014
Publication date	Oct 10, 2017
Grant date	Oct 10, 2017

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.

First claim

We claim:

1. 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.

2. The system of claim 1 , wherein the housing comprises a ceramic matrix composite.

3. The system of claim 1 , wherein the housing has a coefficient of thermal expansion which is less than a coefficient of thermal expansion of the attachment ring.

4. The system of claim 1 , wherein the attachment ring is configured to couple to an engine flange.

5. The system of claim 1 , wherein the bolt is configured to slide within the bushing in response to temperature thermal expansion of the attachment ring.

6. The system of claim 1 , wherein the attachment ring comprises an austenitic nickel-chromium-based alloy.

7. The system of claim 1 , further comprising a nutplate mounted on the attachment ring, wherein the bolt is configured to threadingly engage the nutplate.

8. The system of claim 1 , wherein the housing is configured to be separated from the attachment ring by a gap.

9. 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.

10. The system of claim 9 wherein the cylindrical housing of the exhaust component is formed from a ceramic.

11. The system of claim 9 further comprising a seal positioned between the metallic attachment ring and a forward end of the cylindrical housing which seals therebetween at least when the metallic attachment ring has thermally expanded according to its max operating temperature.

12. The system of claim 9 wherein each of the plurality of metallic bushings is tapered where it contacts the respective radially-spaced aperture and the respective radially-spaced aperture is correspondingly tapered.

13. The system of claim 12 further comprising an insert housing attached to each of the plurality of metallic bushings, wherein the cylindrical housing is positioned and clamped between each of the plurality of metallic bushings and the insert housing.

14. The system of claim 9 wherein the recessed head of each of the plurality of bolts comprises a recessed hex head and a smooth, cylindrical outer head surface.

Assignees

• Rohr Inc

Inventors

• Lu Jacques Jinqiu
• Franks Chad
• Alloway Richard S

Classifications

• F05D2300/176

  Heat-stable alloys · CPC title

• F05D2220/30

  in turbines · CPC title

• F05D2300/6033

  Ceramic matrix composites [CMC] · CPC title

• F01D25/30

  Exhaust heads, chambers, or the like · CPC title

• F02K1/04

  Mounting of an exhaust cone in the jet pipe · CPC title