Bombardier Inc.

C Series Aircraft Limited Partnership

Short Brothers Plc

Learjet Inc.

Benoit Ouellette

Sophie Duchesne

Robert H Grant

Olivier Lebegue

Marc Bergeron

Joseph Patrick Etienne Cote

Nadia Routhier

Frederic Lecoq

Philippe Doyon Poulin

Philippe Doyon-Poulin

Noemie Seguin Tremblay

Simon Labonté

Frederic Leblanc

Mathieu Lavoie

Kosmas Colocythas

Aurélien Blond

Marie-Eve Cote

Aurelien Blond

Apparatus and methods for assisting a flight crew with (e.g., pre-flight) functional testing of aircraft systems are disclosed. An aircraft condition can be used to select one or more functional tests that are applicable based on the aircraft condition. The aircraft condition can be used to initiate the execution of the one or more applicable selected functional tests. The aircraft condition can also be used to identify the one or more functional tests that are applicable on a display device so as to guide the flight crew during the execution of the functional tests.

Apparatus and method for assisting with functional testing of aircraft systems

Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the relevant condition associated with the aircraft; receiving data indicative of a substantially real-time value of a dynamic parameter associated with the relevant condition; and displaying an awareness-enhancing indication associated with the relevant condition in a display area of the crew alerting system of the aircraft. The awareness-enhancing indication comprises a textual message and a supplemental indication indicative of the substantially real-time value of the dynamic parameter associated with the relevant condition. In various embodiments, the supplemental indication may be textual or graphical. The supplemental indication may also be indicative of a target value of the dynamic parameter.

Crew alerting systems and methods for mobile platforms

A crew alerting system for a mobile platform includes a display device defining a display area, a processor operatively coupled to the display device, and a memory storing instructions that cause the processor to: upon receiving notification of an occurrence of a manual system configuration associated with the mobile platform, generate a first output for causing the display device to display a first indication in the display area, the first indication comprising a first textual message. The processor is further configured to, upon receiving notification of an occurrence of an automated system configuration associated with the mobile platform, generate a second output for causing the display device to display a second indication in the display area, the second indication comprising a second textual message accompanied by a supplemental indication such as a graphical indication.

The present disclosure describes displaying on a flight deck () graphical presentations indicative of performance limitations of an aircraft () resulting from an in-flight aircraft reconfiguration. The graphical presentations are co-located on the flight deck () with the graphical presentations of the aircraft () and/or system () parameters to which the performance limitations apply.

Displaying performance limitations in aircraft display

Methods and systems for assisting a pilot during flight of an aircraft are disclosed. The method includes receiving data indicative of a current location of the aircraft during flight and data indicative of a flight boundary, and determining that the flight boundary is relevant to the aircraft. The method also includes causing a display device to display a surface representing the flight boundary relative to the current location of the aircraft.

Aircraft system and method for assisting a pilot during flight

Systems and methods for assisting a flight crew of an aircraft with controller-pilot data link communication (CPDLC) are provided. A display device defines a display area on a flight deck of the aircraft. A controller is operatively coupled to the display device and configured to control a presence of a CPDLC window containing a CPDLC message in the display area. A plurality of tactile buttons are disposed proximally to each other on a glare shield panel of the flight deck. The plurality of tactile buttons comprises a first tactile button operatively coupled to the controller for selectively instructing the controller to cause the presence of the CPDLC window in the display area by actuation of the first tactile button, and a second tactile button configured to permit the flight crew to respond to the CPDLC message by actuation of the second tactile button.

System and method for assisting a flight crew with controller-pilot data link communication

Systems, methods and computer program products for controlling the movement of a cursor on a display device in an aircraft are disclosed. An exemplary method disclosed comprises the use of a digital representation of a grid defining a plurality of cells overlaying at least a portion of a display area of the display device to control the movement of the cursor over the display area. The grid may be invisible to the user during operation.

Cursor control for aircraft display device

Systems, devices and methods a for assisting a pilot with aircraft landing are disclosed. One exemplary method comprises receiving data representative of a current approach/landing capability of the aircraft and data representative of an approach/landing intent of the pilot; and showing a combined indicator graphically and simultaneously indicating the current approach/landing capability of the aircraft and the approach/landing intent of the pilot on a display device of the aircraft. The approach/landing intent of the pilot may be graphically indicated via cooperation between a first graphical object of the indicator and a second graphical object of the indicator. The method may graphically indicate a system degradation affecting the current approach/landing capability of the aircraft with the same indicator.

Systems and methods for assisting with aircraft landing

Systems, devices and methods a for use with one or more high-lift flight control surfaces () of aircraft are disclosed. One exemplary method comprises receiving data representative of a commanded configuration () for a high-lift flight control surface (); and on a display device () of the aircraft, showing an indicator () indicating the commanded configuration and a corresponding commanded position () for the high-lift flight control surface (). The indicator () graphically indicates a correlation between the commanded configuration () and the corresponding commanded position () for the high-lift flight control surface ().

Indicating systems, devices and methods for high-lift flight control surfaces of aircraft

The present disclosure relates to a check-list display system (), a method, a graphical interface () and a computer program product. The checklist display system, method, graphical interface and computer program product display in a first segment () of one page of the checklist display () at least one normal checklist identifier (). The checklist display system, method, graphical interface and computer program further display in a second segment () of the one page of the checklist display at least one non-normal checklist identifier () and at least one limitation information () relating to one of the non-normal checklist.

Checklist display system, method and graphical display therefor

A controller includes a first body portion, adapted to be grasped by a person's middle finger, ring finger, and pinky finger, a second body portion adapted to be grasped by a person's index finger, and a third body portion that defines a first surface adapted to receive a person's thumb. A finger switch is positioned on a front surface of the second body portion. The finger switch is positioned such that it may be actuated by the person's index finger. The second body portion is disposed between the first body portion and the third body portion. The second body portion defines an offset with respect to the first body portion. The third body portion defines a second surface above the finger switch, which may receive the person's index finger.

Controller

The present invention relates to a fly-by-wire type of aircraft flight control system having a pair of sidesticks for pilot and co-pilot input, respectively, and having logic that controls the priority of input as between the two sidesticks in certain aircraft flight situations. It allows either the pilot or co-pilot to ensure that his/her sidestick is the only one issuing flight control commands at any one moment in time by first pressing a simple latch button located, for example, on the glareshield in the cockpit and then maneuvering the sidestick in the desired manner to effectuate flight control, e.g., pitch and/or roll, of the aircraft.

Growing community of inventors

Verdun, Canada

Benoit Ouellette