Compression ring for exhaust nozzle and center body attachment

Patent metadata

Field	Value
Publication number	US-11459980-B2
Application number	US-201916700636-A
Country	US
Kind code	B2
Filing date	Dec 2, 2019
Priority date	Dec 2, 2019
Publication date	Oct 4, 2022
Grant date	Oct 4, 2022

Abstract

An attachment system for an exhaust component is disclosed. In various embodiments, the attachment system includes a radial attachment flange of the exhaust component; and a radial ring having at least one of a radially outer surface configured for engagement with a radially inner surface of the radial attachment flange or a radially inner surface configured for engagement with a radially outer surface of the radial attachment flange.

First claim

What is claimed:

1. An attachment system for an exhaust component, comprising:
a radial attachment flange of the exhaust component;
a radial ring having a radially inner surface configured to contact a radially outer surface of the radial attachment flange in response to heating of the attachment system; and
a radially inner ring having a radially outer surface configured for engagement with a radially inner surface of the radial attachment flange;
wherein the radial attachment flange exhibits a coefficient of thermal expansion lower in value than the coefficient of thermal expansion of the radially inner ring; and
wherein the radial ring is a radially outer ring and the radial attachment flange exhibits a coefficient of thermal expansion higher in value than the coefficient of thermal expansion of the radially outer ring.

2. The attachment system of claim 1 , wherein the radially inner ring is configured to engage the radial attachment flange via a clearance fit between the radially outer surface of the radially inner ring and the radially inner surface of the radial attachment flange.

3. The attachment system of claim 2 , wherein the radially inner ring is configured to apply a radially outwardly facing compressive load against the radially inner surface of the radial attachment flange.

4. The attachment system of claim 3 , wherein the radially inner ring is configured to apply the radially outwardly facing compressive load against the radially inner surface of the radial attachment flange upon being exposed to a hot exhaust stream.

5. The attachment system of claim 4 , wherein the radially inner ring includes a plurality of apertures configured to accommodate a plurality of bolts configured to secure the radial attachment flange to an attachment ring.

6. The attachment system of claim 1 , wherein the radially inner ring is configured to apply a radially outwardly facing compressive load against the radially inner surface of the radial attachment flange upon being exposed to a hot exhaust stream.

7. The attachment system of claim 6 , wherein the radially outer ring is configured to apply a radially inwardly facing compressive load against the radially outer surface of the radial attachment flange upon being exposed to the hot exhaust stream.

8. The attachment system of claim 7 , wherein the radially outer ring includes a plurality of apertures configured to accommodate a plurality of bolts configured to secure the radial attachment flange to an attachment ring.

9. A method of attaching an exhaust component to an attachment ring, comprising:
positioning a radially outer ring around a radially outer surface of a radial attachment flange of the exhaust component;
securing the radial attachment flange to the attachment ring via a plurality of bolts; and
positioning a radially inner ring against a radially inner surface of the radial attachment flange of the exhaust component;
wherein the radial attachment flange exhibits a coefficient of thermal expansion lower in value than the coefficient of thermal expansion of the radially inner ring;
wherein the radial attachment flange exhibits a coefficient of thermal expansion higher in value than the coefficient of thermal expansion of the radially outer ring; and
a radially inner surface of the radially outer ring is configured to contact the radially outer surface in response to heating of the radial attachment flange and the radially outer ring,
wherein the radial attachment flange exhibits a coefficient of thermal expansion lower in value than the coefficient of thermal expansion of the radially inner ring.

10. The method of claim 9 , wherein the radially inner ring is configured to apply a radially outwardly facing compressive load against the radially inner surface of the radial attachment flange upon being exposed to a hot exhaust stream and the radially outer ring is configured to apply a radially inwardly facing compressive load against the radially outer surface of the radial attachment flange upon being exposed to the hot exhaust stream.

11. The method of claim 9 , further comprising applying a coating to a surface of the radially outer ring, the coating configured to prevent degradation.

12. An exhaust system for a gas turbine engine, comprising:
an exhaust component having a radial attachment flange;
an attachment ring configured to secure the exhaust component to the gas turbine engine; and
a radial ring having a radially inner surface configured to contact a radially outer surface of the radial attachment flange in response to heating of the exhaust system;
a radially inner ring having a radially outer surface configured for engagement with a radially inner surface of the radial attachment flange;
wherein the radial attachment flange exhibits a coefficient of thermal expansion lower in value than the coefficient of thermal expansion of the radially inner ring; and
wherein the radial ring is a radially outer ring and the radial attachment flange exhibits a coefficient of thermal expansion higher in value than the coefficient of thermal expansion of the radially outer ring.

Assignees

• Rohr Inc

Inventors

• Kelford Bryce Tyler
• Saunders Adam
• Alloway Richard Scott
• Pujar Vijay V

Classifications

• F02K1/80 Primary

  Couplings or connections · CPC title

• F02K1/04 Primary

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

• F05D2300/50212

  dissimilar · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F05D2260/31

  Retaining bolts or nuts · CPC title