公开(公告)号：US11136135B2

公开(公告)日：2021-10-05

申请号：US15477889

申请日：2017-04-03

Applicant: Bell Helicopter Textron Inc.

Inventor： Daniel Robert Lewis ,  Alan Soo Love

IPC: B64D45/00 ,  B64F5/60 ,  G07C5/00 ,  G07C5/08 ,  B64C27/04

Abstract: A regime recognition system for an aircraft has a regime engine configured to identify a sub-regime performance of the aircraft only after having identified a top tier or top level regime performance that can include the sub-regime performance.

公开(公告)号：US20170203854A1

公开(公告)日：2017-07-20

申请号：US15477889

申请日：2017-04-03

Applicant: Bell Helicopter Textron Inc.

Inventor： Daniel Robert Lewis ,  Alan Soo Love

IPC: B64D45/00 ,  B64C27/04

CPC classification number: B64D45/00 ,  B64C27/04 ,  B64D2045/0085 ,  B64F5/60 ,  G07C5/00 ,  G07C5/08

Abstract: A regime recognition system for an aircraft has a regime engine configured to identify a sub-regime performance of the aircraft only after having identified a top tier or top level regime performance that can include the sub-regime performance.

公开(公告)号：US10518906B2

公开(公告)日：2019-12-31

申请号：US15634903

申请日：2017-06-27

Applicant: Bell Helicopter Textron Inc.

Inventor： Alan Soo Love

IPC: G07C5/00 ,  B64F5/60 ,  B64C27/04 ,  B64D45/00 ,  G07C5/08

Abstract: A system has a flight measurement sensor configured to provide a flight measurement of an aircraft, a regime engine configured to identify a plurality of flight regimes that the aircraft operated in during a period of time, a component engine configured to assign a first flight regime of the plurality of flight regimes to a first component of the aircraft for the period of time, and a health assessment system configured to determine an amount of damage inflicted on the component as a result of the first component spending time in the first flight regime assigned by the component engine.

公开(公告)号：US20170291726A1

公开(公告)日：2017-10-12

申请号：US15634903

申请日：2017-06-27

Applicant: Bell Helicopter Textron Inc.

Inventor： Alan Soo Love

IPC: B64F5/60 ,  G07C5/00

CPC classification number: B64F5/60 ,  B64C27/04 ,  B64D45/00 ,  B64D2045/0085 ,  G07C5/00 ,  G07C5/085

Abstract: A system has a flight measurement sensor configured to provide a flight measurement of an aircraft, a regime engine configured to identify a plurality of flight regimes that the aircraft operated in during a period of time, a component engine configured to assign a first flight regime of the plurality of flight regimes to a first component of the aircraft for the period of time, and a health assessment system configured to determine an amount of damage inflicted on the component as a result of the first component spending time in the first flight regime assigned by the component engine.