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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Suspension rudder bar for an aircraft turbojet and a suspension with fan hanger provided therewith

Invented by: Yoann Marechal
Dommarie les Lys, FR Applicant: Name City State Country Type Marechal

Originally Assigned to: SNECMA
Paris, FR
[Now assigned to . . .]

Issued:2014-01-07
Filed:2011-04-15
Application No:13087693
Examined by:Bonzell; Philip J

A suspension rudder bar has the shape of a bar with a transversal axis (Y'Y), symmetrical with respect to a plane (P.sub.S) intersecting the rotation axis (X'X) of the engine, and includes links with transmission connecting rods between a rear casing for ejecting gases and a front casing hub of the fan, and a central link to a fastening fixation to an engine fastening pylon. The links of the rudder bar to the transmission connecting rods are arranged on the transversal ends of the rudder bar, and the rudder bar extends, perpendicularly to the axis of the bar (Y'Y), with spars over a sufficient portion and at a determined distance from the edges of the plate to act as an abutment to the plate in the case of a torsion around the central link or of a connecting rod breaking.

[pdf] U.S. Pat. No. 8,622,341

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This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.

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