Turbomachine geared architecture support assembly

US9017010B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9017010-B2
Application numberUS-201213362389-A
CountryUS
Kind codeB2
Filing dateJan 31, 2012
Priority dateJan 31, 2012
Publication dateApr 28, 2015
Grant dateApr 28, 2015

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  1. Title

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  2. Abstract

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  4. Key dates

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  5. First independent claim

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Abstract

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An example turbomachine geared architecture support assembly includes a subpart having a more compliant portion and a less compliant portion. The less compliant portion includes a stop that limits axial movement of a geared architecture within a turbomachine.

First claim

Opening claim text (preview).

I claim: 1. A turbomachine geared architecture support assembly, comprising: a support having a more compliant portion and a less compliant portion, wherein the less compliant portion includes a stop that limits axial movement of a geared architecture within a turbomachine, the stop configured to be spaced from a rigid member during normal operation of a turbomachine that includes the geared architecture, the stop further configured to contact the rigid member during abnormal oper…

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What does patent US9017010B2 cover?
An example turbomachine geared architecture support assembly includes a subpart having a more compliant portion and a less compliant portion. The less compliant portion includes a stop that limits axial movement of a geared architecture within a turbomachine.
Who is the assignee on this patent?
Otto John R, United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F02C7/20. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 28 2015 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).