초록 ▼

The present invention provides a system for providing a stress reduction apparatus for a ceramic electrical penetrator or pin in a subsea environment. More specifically, the present invention provides a deformable translatable seat in an annular pocket that prevents the transfer of shear forces from

The present invention provides a system for providing a stress reduction apparatus for a ceramic electrical penetrator or pin in a subsea environment. More specifically, the present invention provides a deformable translatable seat in an annular pocket that prevents the transfer of shear forces from a shell or fixture to a ceramic electrical penetrator or pin. The present invention provides a relatively soft metal seat that conforms to the profile of the shoulder of a mating electrical penetrator or pin and deforms to reduce or eliminate concentrated bearing stresses. The deformable translatable seat may also shift and deform within the annular pocket to relieve shearing stresses exerted on the electrical penetrator or pin by the shell or fixture.

대표청구항 ▼

1. A bulkhead penetrator assembly and stress reduction apparatus for use in subsea environments, the penetrator assembly comprising: a central element having a first end and second end and having a substantially cylindrical body comprising an enlarged central portion, the enlarged central portion be

1. A bulkhead penetrator assembly and stress reduction apparatus for use in subsea environments, the penetrator assembly comprising: a central element having a first end and second end and having a substantially cylindrical body comprising an enlarged central portion, the enlarged central portion being ceramic and having first and second shoulders that gradually transition down respectively to the first and second ends;a first fixture having an opening adapted to receive the first end of the central element and a metallic seal surface comprising an annular pocket;a second fixture having an opening adapted to receive the second end of the central element and a metallic seal surface geometrically configured to abut the second shoulder of the central element;a deformable translatable seat disposed within the pocket of the first fixture and adjacent to the first shoulder of the central element, the deformable translatable seat comprising a deformable material geometrically configured in cooperation with adjoining surfaces of the first fixture and the first shoulder to abut the first shoulder of the central element;wherein the annular pocket forms a recessed space in the metallic seal surface of the first fixture for receiving the deformable translatable seat; andwherein the annular pocket in which the deformable translatable seat is disposed is relatively larger than the deformable translatable seat and is adapted to provide for a change in size of the deformable translatable seat by deformation of the deformable translatable seat, and is further adapted to provide for translation of the deformable translatable seat by movement of the deformable translatable seat within the relatively larger annular pocket. 2. The assembly of claim 1 wherein the deformable translatable seat is adapted to deform within the pocket when under pressure. 3. The assembly of claim 1 wherein the annular pocket is adapted to enable the deformable translatable seat to deform within the annular pocket. 4. The assembly of claim 1 wherein the annular pocket is larger than the deformable translatable seat when the deformable translatable seat is in a non-deformed condition. 5. The assembly of claim 1 wherein the deformable material of the deformable translatable seat is a deformable metal having a hardness relatively less than the first fixture. 6. The assembly of claim 5 wherein the deformable metal is nickel. 7. The assembly of claim 1 wherein the deformable translatable seat is adapted to relieve concentrating bearing stress and shearing stress on the central element. 8. The assembly of claim 1 wherein the central element is a ceramic penetrator. 9. The assembly of claim 1 wherein the deformable translatable seat comprises a ring with a substantially triangular cross-section, the ring comprising: an exterior surface adapted to fit within the pocket; andan interior surface having a profile adapted to geometrically match an exterior surface of the first shoulder of the central element. 10. An apparatus for use in reducing concentric bearing and shearing stresses on ceramic bulkhead penetrators in subsea environments, the apparatus comprising: a deformable translatable annular seat disposed within an annular pocket formed in a bulkhead penetrator assembly, the annular pocket forming a recessed space in a metallic seal surface of the bulkhead penetrator assembly for receiving the deformable translatable annular seat, the annular pocket being relatively larger than the deformable translatable annular seat and adapted to provide for a change in size of the deformable translatable annular seat by deformation of the deformable translatable annular seat and provide for translation of the deformable translatable annular seat by movement of the deformable translatable annular seat within the relatively larger annular pocket, the deformable translatable seat comprising a deformable metal; andwherein the deformable translatable seat is disposed about a ceramic penetrator and is adapted to deform under stress to prevent damage to the ceramic penetrator. 11. The apparatus of claim 10 wherein the deformable translatable seat comprises a ring with a substantially triangular cross-section, the ring comprising: an exterior surface adapted to fit within the annular pocket; andan interior surface having a profile adapted to geometrically match an exterior surface of a first shoulder of a central element of the ceramic penetrator. 12. The apparatus of claim 10 wherein the deformable metal of the deformable translatable seat is a metal having a hardness relatively less than the metal forming the annular pocket. 13. The apparatus of claim 10 wherein the deformable translatable seat is adapted to relieve concentrating bearing stress and shearing stress on the ceramic penetrator. 14. The apparatus of claim 10 wherein the annular pocket is larger than the deformable translatable seat when the deformable translatable seat is in a non-deformed condition. 15. A method for reducing stress for ceramic penetrators in bulkhead penetrator assemblies in subsea environments, the method comprising: placing a ring-shaped deformable translatable seat in an annular pocket formed in a support component of the bulkhead penetrator assembly, the annular pocket forming a recessed space in a sealing surface of the support component for receiving the ring-shaped deformable translatable seat, the annular pocket being relatively larger than the ring-shaped deformable translatable seat and adapted to provide for a change in size of the ring-shaped deformable translatable seat by deformation of the ring-shaped deformable translatable seat and provide for translation of the ring-shaped deformable translatable seat by movement of the ring-shaped deformable translatable seat within the relatively larger annular pocket, the ring-shaped deformable translatable seat comprising a deformable metal;positioning a ceramic penetrator through an opening of the support component defined by the annular pocket and the ring-shaped deformable translatable seat disposed therein wherein a shoulder of the ceramic penetrator abuts an interior surface of the ring-shaped deformable translatable seat; andsecuring the ceramic penetrator in the bulkhead penetrator assembly. 16. The method for stress reduction of claim 15 wherein the ring-shaped deformable translatable seat comprises a substantially triangular cross-section, and wherein the ring-shaped deformable translatable seat further comprises: an exterior surface adapted to matingly fit within the annular pocket; andan interior surface having a profile adapted to geometrically match an exterior surface of the shoulder of the ceramic penetrator. 17. The method for stress reduction of claim 15 wherein the securing comprises subjecting the ceramic penetrator to a compressive force. 18. The method for stress reduction of claim 15 wherein the deformable metal of the deformable translatable seat is a metal having a hardness relatively less than the annular pocket. 19. The method for stress reduction of claim 15 wherein the deformable translatable seat is adapted to relieve concentrating bearing stress and shearing stress on the ceramic penetrator. 20. The method for stress reduction of claim 15 wherein the annular pocket is larger than the deformable translatable seat when the deformable translatable seat is in a non-deformed condition.