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:
Apr. 14, 2009

Filed:

Aug. 11, 2005
Applicants:

Ross Steven Reynolds, La Habra, CA (US);

Doug Ellwood Shultz, La Habra, CA (US);

Inventors:

Ross Steven Reynolds, La Habra, CA (US);

Doug Ellwood Shultz, La Habra, CA (US);

Assignee:

Northrop Grumman Corporation, Los Angeles, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/58 (2006.01);
U.S. Cl.
CPC ...
Abstract

An aircraft motion control mechanism for regulating aircraft motion from a location remote from an aircraft body portion. The aircraft auxiliary control mechanism has at least one control surface support arm connected to and extending from the aircraft body portion, and an auxiliary flow control surface connected to the support arm. By pivotally controlling the movement of the support arm, the auxiliary flow control surface is operative to deflect airflow to regulate orientation of the aircraft. In addition, the auxiliary flow control surface may further deflect the airflow by deflecting about the support arm.


Find Patent Forward Citations

Reynolds, Ross. (2009). Forward pivoted full flying control tail boom (U.S. Patent No. 7516921). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/7516921

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

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