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:
Sep. 22, 2026

Filed:

Jan. 25, 2024
Applicant:

Honeywell International Inc., Charlotte, NC (US);

Inventors:

Gang He, Morris Plains, NJ (US);

Zuowei He, Shanghai, CN;

Ye He, Shanghai, CN;

Hao Chen, Shanghai, CN;

Assignee:

Honeywell Aerospace US LLC, Phoenix, AZ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); B64C 29/00 (2006.01); G06T 11/00 (2026.01); G06T 19/00 (2011.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); G06T 11/00 (2013.01); G06T 19/006 (2013.01); B64C 29/0008 (2013.01);
Abstract

A method and system for computing the deceleration performance to a destination point of a vertical takeoff and landing (VTOL) aircraft has been developed. First, predicted performance of the deceleration of the VTOL aircraft is generated and based on pre-determined data for the VTOL aircraft. Sensors of the VTOL aircraft are monitored to capture real-time performance of the deceleration of the VTOL aircraft. A blended display is created of deceleration of the VTOL aircraft by blending the predicted performance and the real-time performance and is shown to the pilot of the VTOL aircraft. The blended display is continuously adjusted by weighting emphasis on the predicted performance based on the degree of correlation to the real-time performance.


Find Patent Forward Citations

He, Gang. (2026). Method and system to compute de-acceleration performance for a vtol aircraft during approach and landing (U.S. Patent No. 12741751). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12741751

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

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