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:
Sep. 08, 2015

Filed:

Nov. 19, 2009
Applicant:

Karl Schreiber, Am Mellensee, DE;

Inventor:

Karl Schreiber, Am Mellensee, DE;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B29C 59/14 (2006.01); B32B 38/00 (2006.01); B29C 70/02 (2006.01); B08B 7/00 (2006.01); B29C 65/00 (2006.01); B29C 70/08 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); F04D 29/02 (2006.01); F04D 29/32 (2006.01); F04D 29/38 (2006.01); F04D 29/54 (2006.01); B29C 65/48 (2006.01); B29L 31/08 (2006.01); B29L 31/00 (2006.01);
U.S. Cl.
CPC ...
B29C 59/14 (2013.01); B08B 7/0042 (2013.01); B29C 65/48 (2013.01); B29C 66/721 (2013.01); B29C 66/742 (2013.01); B29C 70/028 (2013.01); B29C 70/088 (2013.01); B32B 38/0008 (2013.01); F01D 5/147 (2013.01); F01D 5/282 (2013.01); F04D 29/023 (2013.01); F04D 29/324 (2013.01); F04D 29/388 (2013.01); F04D 29/542 (2013.01); B29C 66/028 (2013.01); B29L 2031/082 (2013.01); B29L 2031/7504 (2013.01); Y02T 50/672 (2013.01);
Abstract

When manufacturing hybrid components, especially the fan blades or stator vanes of an aircraft gas turbine including a metallic enveloping structure and a supporting structure in fiber-composite material, the mating faces of the metallic structure are cleaned and roughened with plasma prior to fitting the fiber-composite material and the metallic molecules activated so that high attractive forces take effect and an intimate, extremely strong adhesive connection is produced between the metal and the fiber-composite material. Fan blades or stator vanes of the fan structure of a gas-turbine engine which are manufactured according to this method are capable of transmitting high loads and feature a long service life.


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