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:
Mar. 07, 2017

Filed:

Oct. 17, 2014
Applicant:

Kenneth A. Cote, San Diego, CA (US);

Inventor:

Kenneth A. Cote, San Diego, CA (US);

Assignee:

Northrop Grumman Systems Corporation, Falls Church, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/00 (2006.01); B64C 27/26 (2006.01); B64C 27/30 (2006.01); B64C 27/473 (2006.01);
U.S. Cl.
CPC ...
B64C 11/003 (2013.01); B64C 27/26 (2013.01); B64C 27/30 (2013.01); B64C 27/473 (2013.01); Y02T 50/66 (2013.01);
Abstract

A retractable rotor system for an aircraft includes a rotor blade with a leading edge, a trailing edge, and an internal collapsible web. The leading edge includes a flexible portion whose lower edge contacts but is not structurally joined to the lower skin. When the leading edge is peeled forward from the lower skin, the blade elastically collapses to the thickness of its constituent layers. The rotor blade extends through a support frame connectable to the aircraft to secure the rotor blade to a spool. Rotating the spool retracts the rotor blade through the support frame while pulling the rotor blade over a fixed actuating member, placing the rotor blade in the collapsed condition and winding the rotor blade onto the spool. Rotating the spool in the opposite direction unwinds the rotor blade from the spool, through the frame, causing the rotor blade to relax into the expanded condition.


Find Patent Forward Citations

Cote, Kenneth. (2017). Collapsible airfoil spooled retractable rotor (U.S. Patent No. 9586674). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9586674

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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