Sliding joint assembly for two parts subjected to large mechanical and thermal stresses

• US 5,445,469 A
• Filed: 12/15/1993
• Issued: 08/29/1995
• Est. Priority Date: 12/30/1992
• Status: Expired due to Fees

• Current Assignee: Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA (Safran SA)
• Original Assignee: Societe Europeenne de Propulsion
• Inventors: Huck, Andre, Indersie, Dominique
• Primary Examiner(s): Reese, Randolph A.
• Assistant Examiner(s): KIM, HARRY CHONG HYUN
• Application Number:
  US08/166,918
• Time in Patent Office: 622 Days
• Field of Search: 403/28, 403/29, 403/30, 403/24, 403/41, 403/335, 403/336, 403/337, 403/338, 60/39.32, 416/241 B
• US Class Current: 403/30
• CPC Class Codes: F01D 25/243 Flange connections; Bolting arrangements F01D25/265 takes precedence
• CPC Class Codes: F02K 9/343 Joints, connections, seals therefor
• CPC Class Codes: F02K 9/97 Rocket nozzles thrust or thrust vector control F02K9/80
• CPC Class Codes: F16B 2200/509 clamped
• CPC Class Codes: Y10T 403/217 Members having different coefficients of expansion

Abstract

The sliding joint assembly for a first part and a second part having different expansion coefficients comprises a plurality of radially-acting spring blades connected firstly at first ends to the first part only in the vicinity of a contact interface, and secondly via second ends to the second part only in a zone that is axially remote from the contact interface, the contact interface constituting a sliding contact interface between the first and second parts while the second ends of the spring blades are connected to the second part by mechanical fasteners constituted by detachable screw-and-nut type assemblies provided with spring washers for damping forces exerted in the axial direction.

Claims

1. A sliding joint assembly comprising a first part and a second part that have different expansion coefficients and that are subject to large mechanical and thermal stresses, the assembly including at least one substantially radial contact interface which is located between the first and second parts, a sealing gasket disposed at said contact interface, mechanical fastening means between the first and second parts, and a plurality of radially acting spring blades each having first and second ends, said spring blades being connected firstly via said first ends thereof to the first part only in a vicinity of said contact interface, and secondly via said second ends thereof to the second part only in a zone that is axially remote from said contact interface, said contact interface constituting a sliding contact surface between the first and second parts, while the second ends of the spring blades are connected to the second part via said mechanical fastening means constituted by detachable screw-and-nut type assemblies provided with spring washers for damping forces exerted in an axial direction which is substantially perpendicular to said radial contact interface.

2. A sliding joint assembly according to claim 1, wherein the spring blades are connected to the first part via radial screw connections acting on flanges secured to the first part and formed perpendicularly to said contact interface.

3. A sliding joint assembly according to claim 1, wherein the spring blades are connected to the first part by weld fillets formed in a vicinity of said contact interface.

4. A sliding joint assembly according to claim 1, wherein the spring blades are integral with a portion of the first part that defines said contact interface.

5. A sliding joint assembly according to claim 1, wherein the spring blades are constituted by narrow individual blades leaving empty gaps between one another, the gaps being of width greater than the width of the spring blades.

6. A sliding joint assembly according to claim 1, wherein the spring blades are constituted by a single skirt that is split so as to form narrow empty gaps between the spring blades, the gaps being narrower than the spring blades.

7. A sliding joint assembly according to claim 1, wherein the detachable screw-and-nut type assemblies provided with said spring washers serve to connect the second ends of the spring blades to a segmented ring assembled together by means of radial pegs and made of a material that has an expansion coefficient close to that of the second part, and that bears against a bottom face of a flange formed on said second part.

8. A sliding joint assembly according to claim 1, wherein said detachable screw-and-nut type assemblies provided with said spring washers connect the second ends of the spring blades with a flange formed directly on the second part.

9. A sliding joint assembly according to claim 1, wherein said first and second parts are circularly symmetrical and superposed axially.

10. A sliding joint assembly according to claim 1, wherein said first part is made of metal and said second part is made of ceramic or composite material.

11. A sliding joint assembly according to claim 1, wherein said second part comprises a portion of an exit cone of a nozzle and said first part comprises a portion of a combustion changer of a rocket engine.