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. 27, 2020

Filed:

May. 31, 2016
Applicant:

Embraer S.a., São José dos Campos-SP, BR;

Inventors:

Jose Roberto Ferreira Clark Reis, São José dos Campos, BR;

Patrice London Guedes, São José dos Campos, BR;

Jonatan Teruo Yamazaki, São José dos Campos, BR;

Nelson Barbosa, São José dos Campos, BR;

Assignee:

Embraer S.A., Sao Jose dos Campos-SP, BR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); B64D 43/00 (2006.01); B64C 3/58 (2006.01); B64C 13/16 (2006.01); B64C 25/42 (2006.01); B64D 31/06 (2006.01); B64D 33/04 (2006.01); B64D 43/02 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); B64C 3/58 (2013.01); B64C 13/16 (2013.01); B64C 25/426 (2013.01); B64D 31/06 (2013.01); B64D 33/04 (2013.01); B64D 43/00 (2013.01); B64D 43/02 (2013.01); B64D 2045/0085 (2013.01); Y02T 50/44 (2013.01);
Abstract

The disclosed non-limiting embodiment provides important improvements in aircraft performance in short rejected takeoff systems by automatically detecting whether the speed of the aircraft does not exceed Vshort, where Vshort>V; automatically detecting whether one of said plural engines has failed during takeoff while the aircraft is still in contact with the ground; and if the aircraft speed does not exceed vshort and an engine has failed, automatically performing an autonomous abort takeoff sequence to allow an improved takeoff weight in case of a single engine failure autonomously rejected takeoff. The aircraft's take off weight increase leads to increased payload or fuel quantity. The Payload increase allows for increased passenger and/or cargo capability. The fuel quantity increased allows the aircraft to achieve greater ranges. An aircraft provided with the proposed system, which reduces accelerate-stop distance, may then operate in shorter runways as compared to the prior art.


Find Patent Forward Citations

Loading…