公开(公告)号：CA2767796C

公开(公告)日：2014-09-16

申请号：CA2767796

申请日：2009-07-27

Applicant: BELL HELICOPTER TEXTRON INC

Inventor： HILL ANDREW T ,  SMITH MICHAEL R ,  COVINGTON CHARLES E ,  LAPPOS NICHOLAS ,  SONNEBORN WALTER

IPC: B64D45/00 ,  B64C25/56 ,  B64C25/62

Abstract: An occupant protection system for an aircraft comprising a sensor system for sensing flight condition information and a control system, which includes an impending crash detection system and an impact detection system. The impending crash detection system receives flight information from the sensors determines whether a crash is likely to occur. If an impending crash is detected, the impending crash detection system activates impact modes of a first group of aircraft systems. The impact detection system receives flight information from the sensor system and determines whether an impact has occurred or is occurring. If an impact is detected, the impact detection system activates impact modes of a second group of aircraft systems.

公开(公告)号：CA2820001C

公开(公告)日：2016-06-07

申请号：CA2820001

申请日：2010-12-22

Applicant: BELL HELICOPTER TEXTRON INC

Inventor： MCCOLLOUGH JAMES M ,  OLTHETEN ERIK ,  LAPPOS NICHOLAS

IPC: B64D43/00 ,  B64D31/00

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：CA2820001A1

公开(公告)日：2012-06-28

申请号：CA2820001

申请日：2010-12-22

Applicant: BELL HELICOPTER TEXTRON INC

Inventor： MCCOLLOUGH JAMES M ,  OLTHETEN ERIK ,  LAPPOS NICHOLAS

IPC: B64D43/00 ,  B64D31/00

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：CA2767796A1

公开(公告)日：2011-02-03

申请号：CA2767796

申请日：2009-07-27

Applicant: BELL HELICOPTER TEXTRON INC

Inventor： HILL ANDREW T ,  SMITH MICHAEL R ,  COVINGTON CHARLES E ,  LAPPOS NICHOLAS ,  SONNEBORN WALTER

IPC: G06F7/70 ,  G06F19/00 ,  G06G7/00 ,  G06G7/76

Abstract: An occupant protection system for an aircraft comprising a sensor system for sensing flight condition information and a control system, which includes an impending crash detection system and an impact detection system. The impending crash detection system receives flight information from the sensors determines whether a crash is likely to occur. If an impending crash is detected, the impending crash detection system activates impact modes of a first group of aircraft systems. The impact detection system receives flight information from the sensor system and determines whether an impact has occurred or is occurring. If an impact is detected, the impact detection system activates impact modes of a second group of aircraft systems.

公开(公告)号：EP2635874A4

公开(公告)日：2014-06-25

申请号：EP10861026

申请日：2010-12-22

Applicant: BELL HELICOPTER TEXTRON INC

Inventor： MCCOLLOUGH JAMES M ,  OLTHETEN ERIK ,  LAPPOS NICHOLAS

IPC: B64D43/00 ,  B64C27/04

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 (301) is configured to provide power information in an aircraft (101). The power safety system (301) includes a power safety instrument (303) having a power required indicator (311) and a power available indicator (313), each being located on a display. A position of the power required indicator (311) and the power available indicator (313) represent the power available and power required to perform a hover flight maneuver. The power safety system (301) may be operated in a flight planning mode or in a current flight mode. The power safety system (301) uses at least one sensor (309) to measure variables having an effect on the power required and the power available.

公开(公告)号：EP2460070A4

公开(公告)日：2013-03-06

申请号：EP09847898

申请日：2009-07-27

Applicant: BELL HELICOPTER TEXTRON INC

Inventor： HILL ANDREW T ,  SMITH MICHAEL R ,  COVINGTON CHARLES E ,  LAPPOS NICHOLAS ,  SONNEBORN WALTER

IPC: G06F7/70 ,  B64D25/00 ,  G05D1/00 ,  G06F19/00 ,  G06G7/00 ,  G06G7/76

CPC classification number: B64D25/00 ,  B64D2201/00