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:
Oct. 25, 2022

Filed:

Sep. 19, 2018
Applicant:

Rosemount Aerospace Inc., Burnsville, MN (US);

Inventors:

Brian Brent Naslund, Chanhassen, MN (US);

John D. Winter, Apple Valley, MN (US);

Assignee:

Rosemount Aerospace Inc., Burnsville, MN (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); B64C 13/10 (2006.01); B64D 43/02 (2006.01); G05D 1/00 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0816 (2013.01); B64C 13/10 (2013.01); B64D 43/02 (2013.01); G05D 1/0088 (2013.01);
Abstract

An anti-spin system for an aircraft can include an anti-spin module configured to execute a computer implemented method. The method can include receiving flight data from one or more aircraft flight data systems, determining if the aircraft is near stall or in a stall using the flight data, and determining if the aircraft is in uncoordinated flight while near stall or in a stall to determine if the aircraft is near spin or in a spin using the flight data. If the aircraft is determined to be near spin, the method includes at least one of sending an alert to a warning indicator in a cockpit to warn the pilot of a spin or near spin condition, or sending a signal to an automated control system for inputting automatic control to the aircraft to avoid a spin by coordinating the aircraft or avoiding a stall while uncoordinated.


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