公开(公告)号：US20170297725A1

公开(公告)日：2017-10-19

申请号：US15131677

申请日：2016-04-18

Applicant: GOODRICH CORPORATION

Inventor： Matthew Campbell ,  Luis G. Interiano ,  James Tulloch ,  John Hampton

IPC: B64D25/10

CPC classification number: B64D25/10

Abstract: A system for selecting an ejection mode on an aircraft may include an egress actuator, a ballistic signal system operatively connected to the egress actuator, and a processor operatively connected to the ballistic signal system and the egress actuator. The processor may be configured to receive, from an aircraft controller, a flight characteristic, and select, based on the flight characteristic, an ejection mode from two ejection modes. The processor may be further configured to receive a pilot egress command from the ballistic signal system, and transmit, to the egress actuator, a signal to actuate the ejection mode from the two ejection modes.

公开(公告)号：US10384788B2

公开(公告)日：2019-08-20

申请号：US15131677

申请日：2016-04-18

Applicant: GOODRICH CORPORATION

Inventor： Matthew Campbell ,  Luis G. Interiano ,  James Tulloch ,  John Hampton

IPC: B64D25/10

Abstract: A system for selecting an ejection mode on an aircraft may include an egress actuator, a ballistic signal system operatively connected to the egress actuator, and a processor operatively connected to the ballistic signal system and the egress actuator. The processor may be configured to receive, from an aircraft controller, a flight characteristic, and select, based on the flight characteristic, an ejection mode from two ejection modes. The processor may be further configured to receive a pilot egress command from the ballistic signal system, and transmit, to the egress actuator, a signal to actuate the ejection mode from the two ejection modes.