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:
Jul. 05, 2016

Filed:

Mar. 13, 2014
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Jia Luo, Belllevue, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01P 3/62 (2006.01); G01C 21/20 (2006.01); G01P 5/14 (2006.01); G01P 5/00 (2006.01); G01P 5/16 (2006.01); G01P 21/02 (2006.01); G01P 5/10 (2006.01);
U.S. Cl.
CPC ...
G01P 5/14 (2013.01); G01C 21/20 (2013.01); G01P 5/00 (2013.01); G01P 5/10 (2013.01); G01P 5/16 (2013.01); G01P 21/025 (2013.01);
Abstract

An airspeed calculation system for determining the airspeed of an aircraft includes a static pressure device, a global positioning system device, an inertial measurement unit device, an angle of attack device, a total pressure sensor, a total air temperature sensor, at least one processor, and a memory. The at least one processor is in electronic communication with the memory, the static pressure device, the global positioning system device, the inertial measurement unit device, the angle of attack device, the total pressure sensor, and the total air temperature sensor. The memory includes programming code for execution by the at least one processor. The programming code is configured to determine the airspeed of the aircraft using data obtained from each of the static pressure device, the global positioning system device, the inertial measurement unit device, the angle of attack device, the total pressure sensor, and the total air temperature sensor.


Find Patent Forward Citations

Luo, Jia. (2016). Airspeed calculation system for an aircraft (U.S. Patent No. 9383381). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9383381

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

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