公开(公告)号：US09096325B2

公开(公告)日：2015-08-04

申请号：US14082615

申请日：2013-11-18

Applicant: Bell Helicopter Textron Inc.

Inventor： Erik Oltheten ,  James M. McCollough ,  Peter F. Scheidler ,  Jeffery S. Greenwood

IPC: B64D31/14 ,  B64D31/04

CPC classification number: B64D31/14 ,  B64D31/04 ,  B64D31/06 ,  F02C9/42 ,  F05D2220/329 ,  Y02T50/671

Abstract: According to one embodiment, a method of managing pilot and copilot control of engine power in an aircraft includes receiving, from a first pilot input device, a first signal representative of a pilot selection of an increase power position or a decrease power position and receiving, from a second pilot input device, a second signal representative of a pilot selection of an increase power position or a decrease power position. One of the first signal and the second signal is prioritized. An aircraft engine is then instructed to change power output based on the prioritized signal.

Abstract translation: 根据一个实施例，一种管理飞行器中的发动机功率的先导和副驾驶控制的方法包括从第一导频输入装置接收代表增加功率位置或减小功率位置的飞行员选择的第一信号， 来自第二导频输入装置的代表增加功率位置或减小功率位置的导频选择的第二信号。 第一个信号和第二个信号之一被优先排列。 然后指示飞机发动机基于优先化信号来改变功率输出。

公开(公告)号：US20140246537A1

公开(公告)日：2014-09-04

申请号：US13932456

申请日：2013-07-01

Applicant: Bell Helicopter Textron Inc.

Inventor： Erik Oltheten ,  Aaron Halverson

IPC: B64D45/00

CPC classification number: B64D43/00 ,  B64C27/008 ,  G01D7/08

Abstract: According to one embodiment, a gauge display prioritization system comprises a priority engine and an output engine. The priority engine is operable to receive a measurement from a first sensor associated with a first aircraft component and a measurement from a second sensor associated with a second aircraft component, select a prioritization criterion based on the received measurements, and select one priority measurement from the received measurements based on the prioritization criterion. The output engine is operable to instruct a gauge disposed within a cockpit to display information representative of the one priority measurement to a pilot.

Abstract translation: 根据一个实施例，量规显示优先级系统包括优先级引擎和输出引擎。 优先级引擎可操作以从与第一飞行器部件相关联的第一传感器接收测量值和从与第二飞行器部件相关联的第二传感器测量值，基于所接收的测量值选择优先级标准，并从 基于优先级标准接收测量。 输出引擎可操作地指示设置在驾驶舱内的计量器向飞行员显示表示一个优先级测量的信息。

公开(公告)号：US09630724B2

公开(公告)日：2017-04-25

申请号：US13932456

申请日：2013-07-01

Applicant: Bell Helicopter Textron Inc.

Inventor： Erik Oltheten ,  Aaron Halverson

IPC: B64C27/00 ,  B64D43/00 ,  G01D7/08

CPC classification number: B64D43/00 ,  B64C27/008 ,  G01D7/08

Abstract: According to one embodiment, a gauge display prioritization system comprises a priority engine and an output engine. The priority engine is operable to receive a measurement from a first sensor associated with a first aircraft component and a measurement from a second sensor associated with a second aircraft component, select a prioritization criterion based on the received measurements, and select one priority measurement from the received measurements based on the prioritization criterion. The output engine is operable to instruct a gauge disposed within a cockpit to display information representative of the one priority measurement to a pilot.

公开(公告)号：US20150142215A1

公开(公告)日：2015-05-21

申请号：US14082615

申请日：2013-11-18

Applicant: Bell Helicopter Textron Inc.

Inventor： Erik Oltheten ,  James M. McCollough ,  Peter F. Scheidler ,  Jeffrey S. Greenwood

IPC: B64D31/14 ,  B64D31/04

CPC classification number: B64D31/14 ,  B64D31/04 ,  B64D31/06 ,  F02C9/42 ,  F05D2220/329 ,  Y02T50/671

Abstract: According to one embodiment, a method of managing pilot and copilot control of engine power in an aircraft includes receiving, from a first pilot input device, a first signal representative of a pilot selection of an increase power position or a decrease power position and receiving, from a second pilot input device, a second signal representative of a pilot selection of an increase power position or a decrease power position. One of the first signal and the second signal is prioritized. An aircraft engine is then instructed to change power output based on the prioritized signal.

Abstract translation: 根据一个实施例，一种管理飞行器中的发动机功率的先导和副驾驶控制的方法包括从第一导频输入装置接收代表增加功率位置或减小功率位置的飞行员选择的第一信号， 来自第二导频输入装置的代表增加功率位置或减小功率位置的导频选择的第二信号。 第一个信号和第二个信号之一被优先排列。 然后指示飞机发动机基于优先化信号来改变功率输出。