Component repair using brazed surface textured superalloy foil
US-2015375346-A1 · Dec 31, 2015 · US
US10414005B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10414005-B2 |
| Application number | US-201415302239-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 9, 2014 |
| Priority date | Apr 9, 2014 |
| Publication date | Sep 17, 2019 |
| Grant date | Sep 17, 2019 |
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Official abstract text for this publication.
An apparatus and method for servicing a combustion liner in a combustion case of a turbine is provided. The apparatus includes an elongated bar having a handle at one end and a force applying member at an opposing end of the elongated bar. An attachment member is configured for attachment to a flange of the combustion case. The attachment member is also configured for pivotal attachment to the elongated bar. The apparatus is configured to apply a radially outward force on a downstream portion of the combustion liner when a radially inward force is applied to the handle.
Opening claim text (preview).
The invention claimed is: 1. An apparatus for servicing a combustion liner in a combustion case of a turbine, the apparatus comprising: an elongated bar having a handle at one end and a force applying member at an opposing end of the elongated bar; an attachment member configured for attachment to a flange of the combustion case, the attachment member also configured for pivotal attachment to the elongated bar, the attachment member comprising a hook that is configured for attachment to the flange by mechanical fasteners, wherein the hook projects axially upstream from the flange; a bracket configured to support and allow slidable motion of the elongated bar therethrough, the bracket including a pin configured to hang on the hook, wherein both the hook and pin are configured to allow the elongated bar to pivot along two substantially orthogonal axes; and wherein the apparatus is configured to apply a radially outward force on a downstream portion of the combustion liner when a radially inward force is applied to the handle. 2. The apparatus of claim 1 , the elongated bar further comprising: a bracket assembly located near a middle portion of the elongated bar, the bracket assembly configured for pivotal attachment to the attachment member. 3. The apparatus of claim 1 , the force applying member further comprising: a wheel or ball comprised of a material configured to resist damaging the combustion liner. 4. The apparatus of claim 3 , wherein the wheel or ball are comprised of or coated with: acetal resin, plastic, polypropylene, polytetrafluoroethylene, or rubber. 5. The apparatus of claim 1 , the attachment member further comprising: a liner guide having a slot configured for guiding a liner stop on the combustion liner. 6. The apparatus of claim 1 , the attachment member further comprising: a clamp configured for clamping onto the flange. 7. The apparatus of claim 1 , wherein an opening of the hook is sized to be larger than a diameter of the pin. 8. The apparatus of claim 7 , wherein the opening of the hook is sized to be at least about 50% to about 100% larger than the diameter of the pin. 9. The apparatus of claim 7 , the force applying member further comprising: a wheel or ball comprised of a material configured to resist damaging the combustion liner. 10. The apparatus of claim 9 , wherein the wheel or ball are comprised of or coated with: acetal resin, plastic, polypropylene, polytetrafluoroethylene, or rubber. 11. A method of servicing a combustion liner in a combustion case of a turbine, the method comprising: providing an elongated bar having a handle at one end and a force applying member at an opposing end of the elongated bar; attaching an attachment member to a flange of the combustion case, the attachment member configured for pivotal attachment to the elongated bar, the attachment member comprising a hook configured for attachment to the flange by mechanical fasteners, wherein the hook projects axially upstream from the flange, and a bracket configured to support and allow slidable motion of the elongated bar therethrough, the bracket including a pin configured to hang on the hook, and both the hook and pin are configured to allow the elongated bar to pivot along two substantially orthogonal axes; and applying force to the handle of the elongated bar to apply a related force to the combustion liner, wherein a radially inward force applied to the handle causes a radially outward force on a downstream portion of the combustion liner. 12. The method of claim 11 , the attaching step further comprising: clamping the attachment member onto the flange. 13. The method of claim 11 , the attaching step further comprising: using mechanical fasteners that are screwed into the flange to secure the attachment member to the flange. 14. The method of claim 11 , wherein the elongated bar further comprises: a bracket assembly located near a middle portion of the elongated bar, the bracket assembly configured for pivotal attachment to the attachment member. 15. The method of claim 14 , wherein the attachment member further comprises: a liner guide having a slot configured for guiding a liner stop on the combustion liner. 16. The method of claim 11 , wherein the force applying member further comprises: a wheel or ball comprised of a material configured to resist damaging the combustion liner; and wherein the material is comprised of acetal resin, plastic, polypropylene, polytetrafluoroethylene or rubber.
Repairing or maintaining combustion chamber liners or subparts · CPC title
Assembling combustion chamber liners or subparts · CPC title
using only replacement pieces of a particular form · CPC title
by attaching repair preform, e.g., remaking, restoring, or patching · CPC title
Replacing of defective part · CPC title
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