公开(公告)号：US09663243B2

公开(公告)日：2017-05-30

申请号：US15168356

申请日：2016-05-31

Applicant: TEXTRON INNOVATIONS INC.

Inventor： James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

IPC: G08B21/00 ,  B64D45/00 ,  B64C27/04 ,  B60Q1/00 ,  B64D43/00 ,  B64C27/00 ,  B64C27/52 ,  B64C29/00 ,  B64C39/02

CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

公开(公告)号：US09352849B2

公开(公告)日：2016-05-31

申请号：US14715236

申请日：2015-05-18

Applicant: TEXTRON INNOVATIONS INC.

Inventor： James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

IPC: G08B21/00 ,  B64D45/00 ,  B64C27/04 ,  B60Q1/00 ,  B64D43/00

CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

公开(公告)号：US10145708B2

公开(公告)日：2018-12-04

申请号：US15608696

申请日：2017-05-30

Applicant: TEXTRON INNOVATIONS INC.

Inventor： James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

IPC: G08B21/00 ,  G01C23/00 ,  B64D45/00 ,  B64C27/04 ,  B60C1/00 ,  B64D43/00 ,  G01D7/02 ,  B64C27/00 ,  B64C27/52 ,  B64C29/00 ,  B64C39/02 ,  G01C21/00 ,  G05D17/02

Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

公开(公告)号：US20170307401A1

公开(公告)日：2017-10-26

申请号：US15608696

申请日：2017-05-30

Applicant: TEXTRON INNOVATIONS INC.

Inventor： James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

IPC: G01C23/00 ,  B64D43/00 ,  G01D7/02 ,  G01C21/00 ,  B64C27/00 ,  G05D17/02

CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

公开(公告)号：US20160272342A1

公开(公告)日：2016-09-22

申请号：US15168356

申请日：2016-05-31

Applicant: TEXTRON INNOVATIONS INC.

Inventor： James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

IPC: B64D45/00 ,  B64C27/04 ,  B64D43/00

CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

Abstract translation: 电力安全系统被配置为在飞行器中提供电力信息。 电力安全系统包括具有电力需求指示器和功率可用指示器的电力安全仪器，每个都位于显示器上。 所需电源指示灯和电源指示灯的位置表示执行悬停飞行操作所需的电力和功率。 电力安全系统可以在飞行计划模式或当前飞行模式下操作。 电力安全系统使用至少一个传感器来测量对所需功率和可用功率有影响的变量。