FASTENER

• US 20140023490A1
• Filed: 07/18/2013
• Published: 01/23/2014
• Est. Priority Date: 07/23/2012
• Status: Abandoned Application

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: HILLIER, Steven
• Application Number:
  US13/945,327
• Publication Number:
  US 20140023490A1
• Time in Patent Office: Days
• US Class Current: 415/173.6
• CPC Class Codes: F01D 11/00 Preventing or minimising internal leakage of working-fluid, e.g. between stages sealings in general F16J ; sealing arrangements for transition ducts of combustor cans F01D9/023
• CPC Class Codes: F01D 11/005 Sealing means between non relatively rotating elements
• CPC Class Codes: F01D 11/24 by selectively cooling-heating stator or rotor components
• CPC Class Codes: F01D 25/246 Fastening of diaphragms or stator-rings
• CPC Class Codes: F05D 2220/32 in gas turbines
• CPC Class Codes: F05D 2240/11 Shroud seal segments
• CPC Class Codes: F05D 2250/13 trapezoidal
• CPC Class Codes: F05D 2260/201 by impingement of a fluid
• CPC Class Codes: F05D 2260/30 Retaining components in desired mutual position
• CPC Class Codes: F05D 2260/36 by a form fit connection, e.g. by interlocking
• CPC Class Codes: F05D 2300/20 Oxide or non-oxide ceramics
• CPC Class Codes: F16L 19/00 Joints in which sealing surfaces are pressed together by means of a member, e.g. a swivel nut, screwed on or into one of the joint parts screw-threaded joints F16L15/00; F16L17/00 takes precedence; if using bolts or equivalent connecting means F16L23/00; electrically insulating F16L25/02; adjustable joints, joints allowing movement F16L27/00; specially adapted for pipes of brittle material F16L49/06

Abstract

A fastener is provided for connecting two or more structural elements having matching apertures which, when aligned, form a frusto-conical cavity. The fastener includes a body portion having a frusto-conical outer surface which is receivable in the aligned apertures of the structural elements such that the outer surface of the body portion is in mating engagement with the cavity formed by the aligned apertures. The fastener further includes an elongate member which extends from the body portion at the narrow end of the frusto-conical outer surface. The fastener further includes a fixing element carried by the elongate member. The fixing element is operable to exert a clamping force between the frusto-conical outer surface and the fixing element to retain the structural elements in connection therebetween. The fastener further includes a through-hole which extends along the elongate member and which allows fluid communication between opposing sides of the connected structural elements.

Claims

1. A fastener for connecting two or more structural elements having matching apertures which, when aligned, form a frusto-conical cavity, the fastener including:

a body portion having a frusto-conical outer surface which is receivable in the aligned apertures of the structural elements such that the outer surface of the body portion is in mating engagement with the cavity formed by the aligned apertures;

an elongate member which extends from the body portion at the narrow end of the frusto-conical outer surface; and

a fixing element carried by the elongate member, the fixing element being operable to exert a clamping force between the frusto-conical outer surface and the fixing element to retain the structural elements in connection therebetween;

wherein the fastener further includes a through-hole which extends along the elongate member and which allows fluid communication between opposing sides of the connected structural elements.

2. A fastener according to claim 1 further having an impingement plate arranged such that fluid exiting the through-hole at the body portion end of the elongate member impinges on the impingement plate.

3. A fastener as claimed in claim 2, further comprising a duct which is sealably connected to the fastener so as to received and redistribute fluid exiting the through-hole.

4. A fastener as claimed in claim 3, wherein the duct and impingement plate are provided by a unitary homogenous structure.

5. A hollow sectioned seal segment for a shroud ring of a rotor of a gas turbine engine, in use, the seal segment being positioned radially adjacent the rotor, and being attached on its radially outer side to an inner side of a backing plate of the shroud ring, a cooling air plenum being formed on the outer side of the backing plate;

wherein the seal segment has one or more outlets for a flow of cooling air from its hollow interior, the seal segment and the backing plate have matching apertures which, when aligned, form a frusto-conical cavity, and the seal segment has a fastener according to claim 1 for connecting the seal segment to the backing plate at the aligned apertures, whereby cooling air can flow through the fastener from the plenum into the hollow interior of the seal segment, and thence to the outlets.

6. A hollow sectioned seal segment for a shroud ring of a rotor of a gas turbine engine, in use, the seal segment being positioned radially adjacent the rotor, and being attached on its radially outer side to an inner side of a backing late of the shroud ring, a cooling air plenum being formed on the outer side of the backing plate;

wherein the seal segment has one or more outlets for a flow of cooling air from its hollow interior, the seal segment and the backing plate have matching apertures which, when aligned, form a frusto-conical cavity, and the seal segment has a fastener according to claim 1 for connecting the seal segment to the backing plate at the aligned apertures, whereby cooling air can flow through the fastener from the plenum into the hollow interior of the seal segment, and thence to the outlets;

the fastener further having

an impingement plate arranged such that fluid exiting the through-hole at the body portion end of the elongate member impinges on the impingement plate, and

a duct which is sealably connected to the fastener so as to received and redistribute fluid exiting the through-hole.

wherein the duct is held within the hollow interior.

7. A hollow sectioned seal segment according to claim 6, wherein the duct comprises arcuate sections which are circumferentially joined to at least one corresponding adjacent arcuate section of duct.

8. A hollow sectioned seal segment according to either of claim 6 wherein the duct comprises a plurality of cooling holes, a first group of holes directly opposing a portion of the seal segment which bounds a main gas path of the gas turbine engine and a second group which is remote to the first group such that air exit the second group undergoes preheating before impinging on a portion of the seal segment which bounds a main gas path of the gas turbine engine.

9. A hollow sectioned seal segment according to claim 5, wherein the duct comprises projections in a space between the seal segment and the duct.

10. A hollow sectioned seal segment according to claim 5, wherein the seal segment is formed of a ceramic material.

11. A hollow sectioned seal segment according to claim 10, wherein the seal segment is formed of a ceramic matrix composite material.

12. A shroud ring of a rotor of a gas turbine engine, the shroud ring including an annular array of hollow sectioned seal segments according to claim 5 connected to the backing plate of the shroud ring.

13. A shroud ring according to claim 12, wherein the backing plate is metallic.

14. The use of a fastener according to claim 1 for connecting two or more structural elements having matching apertures which, when aligned, form a frusto-conical cavity, and for allowing fluid communication between opposing sides of the connected structural elements.