Turbine with a shroud ring around rotor blades and method of limiting leakage of working fluid in a turbine
US-2024280031-A1 · Aug 22, 2024 · US
US2016333741A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016333741-A1 |
| Application number | US-201415111038-A |
| Country | US |
| Kind code | A1 |
| Filing date | Dec 18, 2014 |
| Priority date | Jan 17, 2014 |
| Publication date | Nov 17, 2016 |
| Grant date | — |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
According to some embodiments, a ceramic matrix composite (CMC) hanger sleeve is provided for retaining a ceramic matrix composite shroud panel. The sleeve may be connected to an upper hanger by a retainer or a casing. The hanger sleeve includes a radially inward opening with a flowpath panel disposed therein. When the CMC flowpath panel is worn due to time, rubs or both, the panel may be replaced without need to replace the entire assembly.
Opening claim text (preview).
What is claimed is: 1 . A ceramic matrix composite (CMC) hanger assembly, comprising: a CMC hanger sleeve having a first CMC hanger sleeve leg and a second CMC hanger sleeve leg, wherein the first and second CMC hanger sleeve legs are spaced apart at a radial inward end; a CMC flowpath panel disposed between the first and second CMC hanger sleeve legs at the radial inward end; a spacing between a radial outer end of the first and second CMC hanger sleeve legs; and, a cooling air flowpath passing through the CMC hanger sleeve and cooling the flowpath panel. 2 . The ceramic matrix composite hanger assembly of Claim further comprising an upper shroud hanger connectable to a turbine case. 3 . The ceramic matrix composite hanger assembly of Claim further comprising a retainer disposed adjacent to the hanger sleeve, wherein the retainer has a dimension in one direction which is greater than a window of the hanger sleeve in the one direction. 4 . The ceramic matrix composite hanger assembly of claim 3 , wherein the first CMC hanger sleeve leg and the second CMC hanger sleeve leg is a unitary structure. 5 . The ceramic matrix composite hanger assembly of claim 4 , wherein the unitary structure is an inverted U-shape in section. 6 . The ceramic matrix composite hanger assembly of Claim further comprising a fastener passing through the upper shroud hanger to the retainer. 7 . The ceramic matrix composite hanger assembly of claim 2 , wherein the upper shroud hanger has a first leg and a second leg. 8 . The ceramic matrix composite hanger assembly of claim 7 , wherein the first hanger sleeve leg is fastened to the upper shroud hanger. 9 . The ceramic matrix composite hanger assembly of claim 8 , wherein the second hanger sleeve leg is fastened to the upper shroud hanger. 10 . The ceramic matrix composite hanger assembly of claim 1 , wherein the first leg and the second leg have a surface for engaging a shoulder of the flowpath panel. 11 . The ceramic matrix composite hanger assembly of claim 1 , further comprising a leaf seal extending between one of an upper shroud hanger and a retainer and the CMC flowpath panel. 12 . The ceramic matrix composite hanger assembly of claim 1 , wherein the CMC flowpath panel is U-shaped. 13 . The ceramic matrix composite hanger assembly of claim 12 , wherein the CMC flowpath panel has shoulders which are seated on the first and second CMC hanger sleeve legs. 14 . The ceramic matrix composite hanger assembly of claim 13 , wherein the shoulder is horizontal. 15 . The ceramic matrix composite hanger assembly of claim 13 , wherein the shoulder is angled. 16 . The ceramic matrix composite hanger assembly of claim 1 , further comprising an upper shroud hanger connectable to a turbine case, wherein the cooling air flowpath extends through the upper shroud hanger. 17 . The ceramic matrix composite hanger assembly of claim 16 , wherein the first CMC hanger sleeve leg and the second CMC hanger sleeve leg is a unitary structure. 18 . The ceramic matrix composite hanger assembly of claim 16 , further comprising the upper shroud hanger and at least a portion of the CMC hanger sleeve being integrally formed and define depending retaining legs. 19 . The ceramic matrix composite hanger assembly of claim 18 , wherein the CMC hanger sleeve first leg and second leg are independent of one another and connected to the retaining legs. 20 . The ceramic matrix composite hanger assembly of claim 1 , further comprising a retainer disposed adjacent to the spacing, wherein the retainer has a dimension in one direction which is greater than the spacing in the one direction.
Fastening of diaphragms or stator-rings · CPC title
Ceramic matrix composites [CMC] · CPC title
Casings modified therefor (double casings F01D25/26) · CPC title
Efficient propulsion technologies, e.g. for aircraft · CPC title
in gas turbines · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.