18071141. INTEGRATED THRUST REVERSER AND BRAKE CONTROL FOR AN AIRCRAFT simplified abstract (Raytheon Technologies Corporation)

INTEGRATED THRUST REVERSER AND BRAKE CONTROL FOR AN AIRCRAFT

Organization Name

Raytheon Technologies Corporation

Inventor(s)

David Wasselin of Longmeadow MA (US)

Nancy Poisson of Avon CT (US)

Brian V. Winebrenner of Vernon CT (US)

Bradley C. Schafer of Ellington CT (US)

Ramesh Rajagopalan of Glastonbury CT (US)

INTEGRATED THRUST REVERSER AND BRAKE CONTROL FOR AN AIRCRAFT - A simplified explanation of the abstract

This abstract first appeared for US patent application 18071141 titled 'INTEGRATED THRUST REVERSER AND BRAKE CONTROL FOR AN AIRCRAFT

Simplified Explanation

The patent application describes a system for controlling the deployment of thrust reversers and operation of brakes on an aircraft during landing. The system includes a controller that detects landing conditions, determines control parameters based on current conditions at the target location, and controls the thrust reversers and brakes accordingly.

• The system includes a thrust reverser control and a brake control to manage the deployment of thrust reversers and operation of brakes on the aircraft.
• The controller is responsible for detecting landing conditions, determining control parameters based on current conditions at the target location, and controlling the thrust reversers and brakes during landing.
• The controller can adjust control parameters based on changes in current conditions at the target location or in the event of a fault condition of the aircraft.

Potential Applications

The technology can be applied in commercial aircraft, military aircraft, and other types of aircraft that require precise control of thrust reversers and brakes during landing.

Problems Solved

This technology helps improve the safety and efficiency of aircraft landings by providing automated control of thrust reversers and brakes based on current conditions at the target location.

Benefits

- Enhanced safety during landings - Improved efficiency in aircraft operations - Reduced pilot workload during critical phases of flight

Potential Commercial Applications

"Automated Aircraft Landing Control System: Enhancing Safety and Efficiency"

Possible Prior Art

There are existing systems for controlling thrust reversers and brakes on aircraft during landing, but the specific approach outlined in this patent application may offer unique features or improvements.

Unanswered Questions

How does the system handle emergency situations during landing?

The patent application does not specify how the system responds to emergency scenarios such as engine failure or brake malfunctions.

What are the potential maintenance requirements for this system?

The patent application does not address the maintenance needs or potential challenges associated with implementing and maintaining this technology on aircraft.

Original Abstract Submitted

A system of an aircraft includes a thrust reverser control configured to control deployment of one or more thrust reversers of the aircraft, a brake control configured to control operation of one or more brakes of the aircraft, and a controller. The controller is configured to detect a landing condition of the aircraft, determine one or more thrust reverser deployment and brake control parameters for one or more current conditions at a target location of the aircraft, and control the one or more thrust reversers and the one or more brakes upon landing at the target location based on the one or more thrust reverser deployment and brake control parameters. The controller can modify one or more control parameters of the aircraft based on detecting a change in the one or more current conditions at the target location or a fault condition of the aircraft.