Compliant composite component and method of manufacture

US9249684B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9249684-B2
Application numberUS-201314095604-A
CountryUS
Kind codeB2
Filing dateDec 3, 2013
Priority dateMar 13, 2013
Publication dateFeb 2, 2016
Grant dateFeb 2, 2016

How to read this patent

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  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.

A composite component includes a bonded portion and a component mount. The component mount is coupled to the bonded portion to move relative to the bonded portion. The bonded portion includes a fiber portion and a ceramic portion.

First claim

Opening claim text (preview).

What is claimed is: 1. A composite component comprising a bonded portion made from a ceramic matrix composite material and an un-bonded portion made from the ceramic matrix composite material and coupled to the bonded portion to move relative to the bonded portion in response to application of a load to cause the composite component to deform in a controlled manner without fracture of the composite component, wherein the un-bonded portion includes a first un-bonded section coupled to the bonded portion to move relative to the bonded portion in response to application of the load, a second un-bonded section coupled to the bonded portion to move relative to the bonded portion and the first un-bonded section in response to application of the load, and a third un-bonded section coupled to the bonded portion to move relative to the bonded portion, the first un-bonded section, and the second un-bonded section in response to application of the load. 2. The composite component of claim 1 , wherein the third un-bonded section is located between the bonded portion and the second un-bonded section and the second un-bonded section is located between the third un-bonded section and the first un-bonded section. 3. The composite component of claim 2 , wherein the composite component has a load vs. deflection curve including, in series, a first segment provided by the first un-bonded section and having a first slope, a second segment provided by the second un-bonded section and having a second slope, a third segment provided by the third un-bonded section and having a third slope, and a fourth segment provided by the bonded portion and having a fourth slope. 4. The composite component of claim 3 , wherein the second slope is greater than the first slope, the third slope is greater than the fourth slope, and the fourth slope is greater than the third slope. 5. A composite component comprising a bonded portion made from a ceramic matrix composite material and an un-bonded portion made from the ceramic matrix composite material and coupled to the bonded portion to move relative to the bonded portion in response to application of a load to cause the composite component to deform in a controlled manner without fracture of the composite component, wherein the un-bonded portion includes a first lower un-bonded section coupled to the bonded portion to move relative to the bonded portion in response to application of the load, a second lower un-bonded section coupled to the bonded portion to move relative to the bonded portion and the first lower un-bonded section in response to application of the load, and a third lower un-bonded section coupled to the bonded portion to move relative to the bonded portion, the first lower un-bonded section, and the second lower un-bonded section in response to application of the load. 6. The composite component of claim 5 , wherein the un-bonded portion further includes a first upper un-bonded section coupled to the bonded portion to move relative to the bonded portion in response to application of the load, a second upper un-bonded section coupled to the bonded portion to move relative to the bonded portion and the first upper un-bonded section in response to application of the load, and a third upper un-bonded section coupled to the bonded portion to move relative to the bonded portion, the first upper un-bonded section, and the second upper un-bonded section in response to application of the load. 7. The composite component of claim 6 , wherein the bonded portion includes a first bonded section and a second bonded section and the second bonded section is located between the third lower and upper un-bonded sections, the second upper un-bonded section is located between the third upper un-bonded section and the first upper un-bonded section, and the second lower un-bonded section is located between the third lower un-bonded section and the first lower un-bonded section. 8. The composite component of claim 7 , wherein the composite component has a load vs. deflection curve including, in series, a first segment provided by the first lower and upper un-bonded sections and having a first slope, a second segment provided by the second lower and upper un-bonded sections and having a second slope, a third segment provided by the third upper and lower un-bonded sections and having a third slope, and a fourth segment provided by the second bonded section having a fourth slope and the first slope is greater than the second slope, the third slope is greater than the second slope, fourth slope is greater than the second and the third slopes, and the first slope and the fourth slope are about equal. 9. The composite component of claim 8 , further comprising a component mount coupled to the un-bonded portion and configured to apply the load which is a pre-loading of the un-bonded portion. 10. The composite component of claim 8 , further comprising a component mount coupled to the un-bonded portion and the load includes a first force applied by the component mount to the un-bonded portion and a second force applied to the bonded portion in a direction opposite the first force. 11. The composite component of claim 7 , wherein the composite component has a load vs. deflection curve including, in series, a first segment provided by the first lower and upper un-bonded sections and having a first slope, a second segment provided by the second lower and upper un-bonded sections and having a second slope, a third segment provided by the third upper and lower un-bonded sections and having a third slope, and a fourth segment provided by the second bonded section having a fourth slope, and a fifth section provided by the first, second, and third upper and lower section and the bonded portion, the first slope is greater than the second slope, the third slope is greater than the second slope, third slope is greater than the second and the third slopes, the first and second slopes are about equal, and the fifth slope is less than the second slope. 12. A composite component comprising a bonded portion made from a ceramic matrix composite material and an un-bonded portion made from the ceramic matrix composite material and coupled to the bonded portion to move relative to the bonded portion in response to application of a load to cause the composite component to deform in a controlled manner without fracture of the composite component, wherein the bonded portion includes a first bonded section and a second bonded section and the second bonded section is appended to the first bonded section to extend away from the first bonded section, and wherein the un-bonded portion includes a first un-bonded section appended to the second bonded section to move relative to the second bonded section in response to application of the load, a second un-bonded section appended to the second bonded section to move relative to the second bonded section and the first un-bonded section in response to application of the load, and a third un-bonded section appended to the second bonded section to move relative to the second bonded section, the first un-bonded section, and the second un-bonded section in response to application of the load. 13. The composite component of claim 12 , wherein the third un-bonded section is coupled to the first bonded section to translate relative to the first bonded section and appended to the second bonded section to pivot relative to the second bonded section, the second un-bonded section, and the first un-bonded section. 14. The composite component of claim 13 , wherein the second un-bonded section is coupled to the third un-bonded section to translate re

Assignees

Inventors

Classifications

  • Cross-Sectional Technologies · mapped topic

  • the structure being shaped to form a three-dimensional configuration · CPC title

  • F01D5/282Primary

    Selecting composite materials, e.g. blades with reinforcing filaments · CPC title

  • Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion (F01D5/288 takes precedence) · CPC title

  • Superposed movable attached layers or components · CPC title

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Frequently asked questions

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What does patent US9249684B2 cover?
A composite component includes a bonded portion and a component mount. The component mount is coupled to the bonded portion to move relative to the bonded portion. The bonded portion includes a fiber portion and a ceramic portion.
Who is the assignee on this patent?
Rolls Royce Corp, Rolls Royce Nam Tech Inc
What technology area does this patent fall under?
Primary CPC classification F01D5/282. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Feb 02 2016 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).