Nosecap

US2016273451A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016273451-A1
Application numberUS-201415032517-A
CountryUS
Kind codeA1
Filing dateOct 15, 2014
Priority dateOct 30, 2013
Publication dateSep 22, 2016
Grant date

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  1. Title

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  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present disclosure relates generally to a nosecap for a gas turbine engine. The nosecap may be injection molded in an embodiment. The nosecap may have bolt holes surrounded by bolt pockets that are asymmetric about a plane passing through a geometric center of the nosecap and passing through and dividing the bolt hole in an embodiment.

First claim

Opening claim text (preview).

What is claimed: 1 . A nosecap for a gas turbine engine, the nosecap comprising: an injection molded body having a forward surface and an aft surface separated by an edge. 2 . The nosecap of claim 1 , wherein the body is formed from a material selected from the group consisting of: plastic, polycarbonate, polyetherimide, polyether ether ketone, and nylon. 3 . The nosecap of claim 1 , further comprising at least one rib disposed on the aft surface. 4 . The nosecap of claim 3 , wherein the at least one rib comprises at least one circumferential rib and at least one axial rib. 5 . The nose cap of claim 1 , further comprising at least one wear indicator hole disposed in the aft surface, wherein the at least one wear indicator hole extends to a location aft of the forward surface. 6 . The nosecap of claim 5 , further comprising a wear indicator material at least partially filling the at least one wear indicator hole. 7 . The nosecap of claim 6 , wherein the wear indicator material is visually distinct from the body. 8 . The nosecap of claim 6 , wherein the wear indicator material comprises room temperature vulcanizing silicone. 9 . The nosecap of claim 1 , further comprising: at least one bolt hole formed through the body; and at least one bolt pocket, each at least one bolt pocket extending from the edge and surrounding a respective one of the at least one bolt hole; wherein at least one of the at least one bolt pockets is asymmetric about a plane passing through a geometric center of the body and passing through and dividing the respective one of the at least one bolt hole. 10 . The nosecap of claim 9 , wherein: each of the at least one bolt pockets comprises a leading edge wall, a trailing edge wall, and a transition area wall disposed between the leading edge wall and the trailing edge wall; and the trailing edge wall is curved. 11 . A nosecap for a gas turbine engine, the nosecap comprising: a body having a forward surface and an aft surface separated by an edge; at least one bolt hole formed through the body; and at least one bolt pocket, each at least one bolt pocket extending from the edge and surrounding a respective one of the at least one bolt hole; wherein at least one of the at least one bolt pockets is asymmetric about a plane passing through a geometric center of the body and passing through and dividing the respective one of the at least one bolt hole. 12 . The nosecap of claim 11 , wherein: each of the at least one bolt pockets comprises a leading edge wall, a trailing edge wall, and a transition area wall disposed between the leading edge wall and the trailing edge wall; and the trailing edge wall is curved. 13 . The nosecap of claim 11 , wherein the body is formed from a material selected from the group consisting of: plastic, polycarbonate, polyetherimide, polyether ether ketone, and nylon. 14 . The nosecap of claim 11 , further comprising at least one rib disposed on the aft surface. 15 . The nosecap of claim 14 , wherein the at least one rib comprises at least one circumferential rib and at least one axial rib. 16 . The nose cap of claim 11 , further comprising at least one wear indicator hole disposed in the aft surface, wherein the at least one wear indicator hole does not extend through the forward surface. 17 . The nosecap of claim 16 , further comprising a wear indicator material at least partially filling the at least one wear indicator hole. 18 . The nosecap of claim 17 , wherein the wear indicator material is a different color than the body. 19 . The nosecap of claim 17 , wherein the wear indicator material comprises room temperature vulcanizing silicone. 20 . The nosecap of claim 11 , wherein the body comprises an injection molded body.

Assignees

Inventors

Classifications

  • Maintenance · CPC title

  • Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor (injection blow-moulding B29C49/06) · CPC title

  • Polyetherketones, e.g. PEEK · CPC title

  • asymmetric · CPC title

  • Polyamides, e.g. NYLON · CPC title

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Frequently asked questions

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What does patent US2016273451A1 cover?
The present disclosure relates generally to a nosecap for a gas turbine engine. The nosecap may be injection molded in an embodiment. The nosecap may have bolt holes surrounded by bolt pockets that are asymmetric about a plane passing through a geometric center of the nosecap and passing through and dividing the bolt hole in an embodiment.
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F02C7/04. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Sep 22 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).