Turbomachine casing assembly
US-9206706-B2 · Dec 8, 2015 · US
US2016208652A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016208652-A1 |
| Application number | US-201514600239-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jan 20, 2015 |
| Priority date | Jan 20, 2015 |
| Publication date | Jul 21, 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.
A case assembly is provided. The case assembly comprises a first flange and a spot face in the first flange. The spot face has a D-shaped perimeter. A jacking insert is disposed in the spot face and has a D-shaped geometry. A threaded cylinder extends from the jacking insert into the first flange. A jacking insert is also provided. The jacking insert comprises a flat portion having a D-shaped geometry and a cylindrical portion having an internal thread configured to interface with a bolt.
Opening claim text (preview).
What is claimed is: 1 . A case assembly, comprising: a flange; a recess in the flange defined by a spot face surrounded by a D-shaped wall; a jacking insert comprising a back plate disposed in the recess and having a D-shaped geometry; and a threaded cylinder extending from the back plate into the flange. 2 . The case assembly of claim 1 , further comprising a second flange that is snap fitted to the flange with the jacking insert at least partially between the flange and the second flange. 3 . The case assembly of claim 2 , further comprising a bolt configured to interface with the threaded cylinder. 4 . The case assembly of claim 3 , wherein the bolt is configured to press the flange and the second flange away from one another in response to the bolt entering the jacking insert. 5 . The case assembly of claim 1 , wherein the D-shaped wall comprises a complete hoop around the back plate. 6 . The case assembly of claim 1 , wherein the D-shaped wall is configured to limit rotation of the jacking insert. 7 . The case assembly of claim 1 , further comprising a bulkhead pressed against the flange and covering the spot face. 8 . The case assembly of claim 7 , wherein a bolt is configured to pass through the jacking insert and an opening defined by the bulkhead. 9 . A gas turbine engine, comprising: a static frame component comprising a first flange; a low-pressure compressor aft of the static frame component; a case around the low-pressure compressor and aft of the static frame component, the case comprising a second flange; and a jacking insert between the first flange and the second flange. 10 . The gas turbine engine of claim 9 , further comprising a recess defined by at least one of the first flange and the second flange with the jacking insert disposed in the recess. 11 . The gas turbine engine of claim 10 , wherein the recess is defined by a contoured sidewall matching a geometry of the jacking insert. 12 . The gas turbine engine of claim 11 , wherein the geometry of the jacking insert is D-shaped. 13 . The gas turbine engine of claim 9 , further comprising a threaded cylinder extending from the jacking insert into the first flange. 14 . The gas turbine engine of claim 13 , wherein the second flange is snap fitted to the first flange. 15 . The gas turbine engine of claim 14 , further comprising a bolt configured to interface with the threaded cylinder. 16 . The gas turbine engine claim 15 , wherein the bolt is configured to press the first flange away from the second flange in response to the bolt entering the jacking insert. 17 . The gas turbine engine of claim 10 , wherein the flange comprises a complete hoop around the recess. 18 . A jacking insert, comprising: a back plate having a D-shaped geometry; and a cylindrical portion having an internal thread configured to interface with a bolt. 19 . The jacking insert of claim 18 , wherein the D-shaped geometry is configured to interact with a contoured wall to limit rotation of the jacking insert. 20 . The jacking insert of claim 18 , wherein the D-shaped geometry comprises a round portion and a square portion.
Fastening of diaphragms or stator-rings · CPC title
fixing blades to stators (fixing stator-rings in the casing or to each other F01D25/246) · CPC title
Threaded inserts, e.g. "rampa bolts" · CPC title
Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title
Repairing methods or devices · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.