The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 30, 2017

Filed:

Feb. 12, 2014
Applicant:

Teledyne Scientific & Imaging, Llc, Thousand Oaks, CA (US);

Inventors:

David B. Marshall, Thousand Oaks, CA (US);

Brian N. Cox, Sherman Oaks, CA (US);

Olivier H. Sudre, Thousand Oaks, CA (US);

Assignee:

TELEDYNE SCIENTIFIC & IMAGING, LLC, Thousand Oaks, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); F01D 5/14 (2006.01); F01D 5/18 (2006.01); B32B 18/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); B32B 18/00 (2013.01); F01D 5/147 (2013.01); F01D 5/187 (2013.01); F01D 5/284 (2013.01); C04B 2237/365 (2013.01); C04B 2237/38 (2013.01); F05D 2300/6033 (2013.01); F05D 2300/6034 (2013.01);
Abstract

An integral textile structure for 3-D CMC turbine airfoils includes top and bottom walls made from an angle-interlock weave, each of the walls comprising warp and weft fiber tows. The top and bottom walls are merged on a first side parallel to the warp fiber tows into a single wall along a portion of their widths, with the weft fiber tows making up the single wall interlocked through the wall's thickness such that delamination of the wall is inhibited. The single wall suitably forms the trailing edge of an airfoil; the top and bottom walls are preferably joined along a second side opposite the first side and parallel to the radial fiber tows by a continuously curved section in which the weave structure remains continuous with the weave structure in the top and bottom walls, the continuously curved section being the leading edge of the airfoil.


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