A retention pin assembly may include a stud having a head, a shaft, and a deformable end. The shaft may include a stepped surface having a greater diameter than the deformable end. The assembly may include a support member having an opening for receiving the deformable end. The support member may in
A retention pin assembly may include a stud having a head, a shaft, and a deformable end. The shaft may include a stepped surface having a greater diameter than the deformable end. The assembly may include a support member having an opening for receiving the deformable end. The support member may include a pocket. The stepped surface of the shaft may position the stud in relation to the support member. The deformable end of the stud may be operable to be melted to form a mechanical retainer within the pocket without forming a metallurgical joint between the stud and the pocket.
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1. A retention pin assembly comprising: a stud including a head, a shaft, and a deformable end disposed at a distal end thereof, wherein the shaft includes a stepped surface having a greater diameter than the deformable end;a housing wall defining a base;a support member extending transversely from
1. A retention pin assembly comprising: a stud including a head, a shaft, and a deformable end disposed at a distal end thereof, wherein the shaft includes a stepped surface having a greater diameter than the deformable end;a housing wall defining a base;a support member extending transversely from the base, the support member having an opening extending therethrough for receiving the deformable end, the opening of the support member further including a pocket on one side of the support member;a nub disposed on the support member between the base and the opening, the nub extending transversely to the base along the support member towards the opening and projecting outwardly from the support member on a side opposite the pocket;a leaf seal pivotally mounted on the shaft; anda bias member coaxially arranged on the shaft and disposed between the head and the leaf seal, wherein the bias member exerts a force on the leaf seal;wherein the deformable end is deformed to occupy the pocket, and wherein the deformable end and the stepped surface provide a mechanical retainer to secure the stud to the support member; andwherein the nub is configured to position the leaf seal apart from a distal end of the support member. 2. The pin assembly as claimed in claim 1, wherein the stepped surface of the shaft is hardened via heat treatment. 3. The pin assembly as claimed in claim 1, wherein the stud includes a wear resistant coating. 4. The pin assembly as claimed in claim 1, wherein the support member includes an upper section and a lower section disposed proximal to the base in relation to the upper section, wherein the upper section comprises a single crystal material. 5. The pin assembly as claimed in claim 4, wherein the nub projects substantially orthogonally from the lower section of the support member and is configured to position the leaf seal apart from the upper section of the support member. 6. The pin assembly as claimed in claim 1, wherein the housing wall defining the base is part of a gas turbine engine disposed along a gas pathway between a combustor and a turbine, and wherein the leaf seal is operable to direct a gas flow onto rotor blades of the turbine. 7. The pin assembly as claimed in claim 1, wherein the pocket is conic shaped, and wherein at least part of the deformable end is melted and defines a melted portion occupying the conic shaped pocket without forming a material connection. 8. A leaf seal assembly of a structure, comprising: a stud including a head, a shaft, and a deformable end disposed at a distal end thereof, wherein the shaft includes a stepped surface having a greater diameter than the deformable end;a base defined by a housing wall of the structure, the base including a transversely extended support member, the support member having an opening extending therethrough for receiving the deformable end and a pocket arranged at a mouth of the opening on one side of the support member, the support member further including a nub disposed between the base and the opening, the nub extending transversely to the housing wall along the support member towards the opening on a side opposite the pocket;a leaf seal pivotally mounted on the shaft; anda bias member coaxially arranged on the shaft and disposed between the head and the leaf seal, wherein the bias member exerts a force on the leaf seal;wherein the stepped surface of the shaft positions the stud in a predefined position with respect to the support member, and the deformable end is received in the pocket and is deformed to occupy the pocket to secure the stud to the support member; andwherein the nub projects outwardly from the support member towards the head of the stud to position the leaf seal apart from a portion of the support member distal to the base. 9. The assembly as claimed in claim 8, wherein at least one of the stepped surface of the shaft is hardened via heat treatment and the stud includes a wear resistant coating. 10. The assembly as claimed in claim 8, wherein the bias member includes a wear resistant coating. 11. The assembly as claimed in claim 8, wherein the support member includes an upper section and a lower section, wherein the upper section defines the portion of the support member distal to the housing wall and comprises a single crystal material, and wherein the nub extends from the base towards the opening and projects outwardly from the lower section to facilitate positioning the leaf seal apart from the upper section. 12. The assembly as claimed in claim 8, wherein the structure is a gas turbine engine having a longitudinal center axis and the housing wall defining the base is disposed radially outwards from the longitudinal center axis, and wherein the nub extends transversely from the base along the support member and projects outwardly in an axial direction of the longitudinal center axis. 13. The assembly as claimed in claim12, wherein the housing wall is disposed in a region of a gas flow path between a combustor and a turbine such that the leaf seal is arranged to direct combustion gases onto rotor blades of the turbine. 14. The assembly as claimed in claim 8, wherein the leaf seal is operable to engage an opposing member to seal off a gas pathway. 15. A method of forming a joint for a machine, comprising: providing a stud, the stud including a head, a shaft, and a deformable end disposed at a distal end thereof, wherein the shaft includes a stepped surface having a greater diameter than the deformable end;providing a base defined by a housing wall of the machine and including a support member extending transversely from the base for receiving the stud via an opening extending therethrough, the support member including an upper section and a lower section proximal to the base in relation to the upper section;providing a leaf seal pivotally mounted on the shaft; andproviding a bias member coaxially arranged on the shaft and disposed between the head and the leaf seal, wherein the bias member exerts a force on the leaf seal;forming a pocket at an end of the opening in the support member on one side of the support member;inserting the deformable end through the opening, wherein the stepped surface of the shaft stops the stud in a predefined position with respect to the support member;securing the stud to the support member via melting the deformable end in the pocket thereby forming a mechanical retainer within the pocket without forming a metallurgical joint between the stud and the pocket;wherein providing the base and the support member includes forming a nub on the lower section extending transversely from the base along the support member towards the opening, wherein the nub projects substantially orthogonally from the lower section on a side of the support member opposite the pocket; andwherein the nub is configured to position the leaf seal apart from a distal end of the support member. 16. The method as claimed in claim 15, further comprising at least one of applying a wear resistant coating to the stud and hardening the stepped surface of the shaft via a heat treatment. 17. The method as claimed in claim 15, wherein securing the stud to the support member via melting the deformable end in the pocket includes welding the deformable end to provide a melted portion occupying the pocket by filling the pocket with molten material of the deformable end and cooling the molten material to facilitate forming the mechanical retainer without forming the metallurgical joint.
Doyle Thomas E. (Columbus OH) Hauser Daniel (Columbus OH) Martin David C. (Worthington OH) Hayes Michael D. (Minas Gerais BRX), Apparatus and method for double end stud welding.
Mitchell, Krista Anne; Bulman, David Edward; Noe, Mark Eugene; Hansel, Harold Ray; Glynn, Christopher Charles; Bibler, John David, Sealing assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor.
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