公开(公告)号：US10674080B2

公开(公告)日：2020-06-02

申请号：US15651567

申请日：2017-07-17

申请人： Sikorsky Aircraft Corporation

发明人： Carl A. Palmer ,  Ronald Moffatt ,  Cody M. Ture ,  Craig D. Reed

IPC分类号： H04N5/225 ,  H04N5/232 ,  H04N5/247 ,  G03B15/03 ,  B64D47/08 ,  B64F5/60 ,  G03B17/02 ,  G03B17/38 ,  G03B15/00 ,  B64C27/06 ,  G03B15/05

摘要： An integrated inspection system including at least one surface defining an enclosed space, at least one camera mounted in the enclosed space, and an interrogator device operatively coupled to the at least one camera. The interrogator device provides power to and receives images from the camera.

公开(公告)号：US10773814B2

公开(公告)日：2020-09-15

申请号：US15744422

申请日：2016-07-20

申请人： Sikorsky Aircraft Corporation

发明人： Michael Peter Strauss ,  Michael Joseph DeVita ,  Mark Denton Bystry, Jr. ,  Joseph Lawrence Simonetti ,  Carl A. Palmer

IPC分类号： B64D31/06 ,  B64C27/12 ,  F02C7/262 ,  F02C7/268 ,  B64D31/14 ,  F02C7/26 ,  B64D27/14 ,  B64D45/00

摘要： A control system for an in-flight engine restart system of a rotorcraft includes an engine control unit that controls and detects status of an engine. The control system also includes a flight control computer that communicates with the engine control unit, an engine operation control system, and a pilot interface including pilot controls. The engine operation control system includes a processor that initiates a health check of the in-flight engine restart system to determine an in-flight engine restart system status. The engine operation control system processes engine mode of operation commands to establish an engine mode of operation, and delivers commands to aspects of the in-flight engine restart system including the engine control unit based on processing of the engine mode of operation commands. The engine operation control system reports the in-flight engine restart system status and results of the engine mode of operation commands to the flight control computer.

公开(公告)号：US20180201386A1

公开(公告)日：2018-07-19

申请号：US15744422

申请日：2016-07-20

申请人： Sikorsky Aircraft Corporation

发明人： Michael Peter Strauss ,  Michael Joseph DeVita ,  Mark Denton Bystry, Jr. ,  Joseph Lawrence Simonetti ,  Carl A. Palmer

IPC分类号： B64D31/06 ,  B64C27/12 ,  F02C7/262 ,  B64D45/00 ,  B64D27/14

CPC分类号： B64D31/06 ,  B64C27/12 ,  B64D27/14 ,  B64D31/14 ,  B64D45/00 ,  B64D2045/0085 ,  F02C7/26 ,  F02C7/262 ,  F02C7/268 ,  F05D2220/329 ,  F05D2260/40311 ,  F05D2260/80 ,  F05D2260/85 ,  F05D2270/093

摘要： A control system for an in-flight engine restart system of a rotorcraft includes an engine control unit that controls and detects status of an engine. The control system also includes a flight control computer that communicates with the engine control unit, an engine operation control system, and a pilot interface including pilot controls. The engine operation control system includes a processor that initiates a health check of the in-flight engine restart system to determine an in-flight engine restart system status. The engine operation control system processes engine mode of operation commands to establish an engine mode of operation, and delivers commands to aspects of the in-flight engine restart system including the engine control unit based on processing of the engine mode of operation commands. The engine operation control system reports the in-flight engine restart system status and results of the engine mode of operation commands to the flight control computer.

公开(公告)号：US20180027183A1

公开(公告)日：2018-01-25

申请号：US15651567

申请日：2017-07-17

申请人： Sikorsky Aircraft Corporation

发明人： Carl A. Palmer ,  Ronald Moffatt ,  Cody M. Ture ,  Craig D. Reed

IPC分类号： H04N5/232 ,  B64D47/08 ,  G03B15/03 ,  G03B15/00 ,  H04N5/225 ,  H04N5/247

CPC分类号： H04N5/23241 ,  B64C27/06 ,  B64D47/08 ,  B64F5/60 ,  G03B15/006 ,  G03B15/03 ,  G03B15/05 ,  G03B17/02 ,  G03B17/38 ,  G03B2206/00 ,  G03B2217/007 ,  H04N5/2256 ,  H04N5/2257 ,  H04N5/247

摘要： An integrated inspection system including at least one surface defining an enclosed space, at least one camera mounted in the enclosed space, and an interrogator device operatively coupled to the at least one camera. The interrogator device provides power to and receives images from the camera.