公开(公告)号：USD878258S1

公开(公告)日：2020-03-17

申请号：US29675582

申请日：2019-01-03

Applicant: Bell Helicopter Textron Inc.

Designer： James Gibson ,  Carey Cannon ,  William Kyle Heironimus

公开(公告)号：US11021244B2

公开(公告)日：2021-06-01

申请号：US15913526

申请日：2018-03-06

Applicant: Bell Helicopter Textron Inc.

Inventor： Yann Lavallee ,  Carey Cannon

IPC: B64C27/56 ,  B64D31/04

Abstract: A helicopter includes a full authority digital engine controlled (FADEC) engine, a first two-position throttle switch disposed on a first collective control stick, the first two-position throttle switch being movable between a Fly position and an Idle position, and a second two-position throttle switch disposed on a second collective control stick, the second two-position throttle switch being movable between a Fly position and an Idle position.

公开(公告)号：US11238200B2

公开(公告)日：2022-02-01

申请号：US16293425

申请日：2019-03-05

Applicant: Bell Helicopter Textron Inc.

Inventor： Michael McNair ,  Brent Chadwick Ross ,  Christopher Stroncek ,  Kip Gregory Campbell ,  Joseph Scott Drennan ,  Brett Zimmerman ,  Carey Cannon

IPC: G06F30/33 ,  H01R13/66 ,  G06F30/15 ,  G06F30/367 ,  G09B9/42 ,  G09B9/00 ,  G09B9/12 ,  G09B19/16

Abstract: A method of operating a targeting system simulation tool (TSST) includes providing a TSST configured to receive an obstacle/effect parameterization, a simulation parameterization, a sensor parameterization, an aircraft parameterization, and an autonomy parameterization. The method further includes receiving by the TSST, at least one of each of an obstacle/effect parameterization and a simulation parameterization. The method further includes receiving by the TSST, either (1) a sensor parameterization or (2) an aircraft parameterization. The method further includes operating the TSST to apply the provided ones of the obstacle/effect parameterization, simulation parameterization, sensor parameterization, and aircraft parameterization to generate a value, value range, or value limit for the unprovided aircraft parameterization or unprovided sensor parameterization.

公开(公告)号：US20180251214A1

公开(公告)日：2018-09-06

申请号：US15913526

申请日：2018-03-06

Applicant: Bell Helicopter Textron Inc.

Inventor： Yann Lavallee ,  Carey Cannon

IPC: B64C27/56 ,  B64C27/58

CPC classification number: B64C27/56 ,  B64C27/58 ,  B64D31/04 ,  G05G1/00

Abstract: A helicopter includes a full authority digital engine controlled (FADEC) engine, a first two-position throttle switch disposed on a first collective control stick, the first two-position throttle switch being movable between a Fly position and an Idle position, and a second two-position throttle switch disposed on a second collective control stick, the second two-position throttle switch being movable between a Fly position and an Idle position.

公开(公告)号：US20200026811A1

公开(公告)日：2020-01-23

申请号：US16293425

申请日：2019-03-05

Applicant: Bell Helicopter Textron Inc.

Inventor： Michael McNair ,  Brent Chadwick Ross ,  Christopher Stroncek ,  Kip Gregory Campbell ,  Joseph Scott Drennan ,  Brett Zimmerman ,  Carey Cannon

IPC: G06F17/50 ,  H01R13/66

Abstract: A method of operating a targeting system simulation tool (TSST) includes providing a TSST configured to receive an obstacle/effect parameterization, a simulation parameterization, a sensor parameterization, an aircraft parameterization, and an autonomy parameterization. The method further includes receiving by the TSST, at least one of each of an obstacle/effect parameterization and a simulation parameterization. The method further includes receiving by the TSST, either (1) a sensor parameterization or (2) an aircraft parameterization. The method further includes operating the TSST to apply the provided ones of the obstacle/effect parameterization, simulation parameterization, sensor parameterization, and aircraft parameterization to generate a value, value range, or value limit for the unprovided aircraft parameterization or unprovided sensor parameterization.