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公开(公告)号:US09418493B1
公开(公告)日:2016-08-16
申请号:US14700333
申请日:2015-04-30
Applicant: The Boeing Company
Inventor: Jian Dong
CPC classification number: G05B23/0221 , G05B23/0235 , G05B2219/37534
Abstract: A method includes receiving a stream of sensor data regarding operating conditions of a vehicle, and processing first and second data sets of the stream of sensor data in time and frequency domains. The method also includes identifying differences within and between processing results from processing the first and second data sets, and determining that at least one difference in the identified differences is greater than or equal to one or more predefined thresholds. Further, the method includes, based on determining the at least one difference in the identified differences being greater than or equal to the one or more predefined thresholds, recording one or more processing results corresponding to the identified at least one difference in a data index map (DIM), and analyzing contents of the DIM to evaluate operating conditions of the vehicle.
Abstract translation: 一种方法包括接收关于车辆的操作条件的传感器数据流,以及处理时域和频域中的传感器数据流的第一和第二数据集。 该方法还包括识别处理结果内和之间处理第一和第二数据集之间的差异,以及确定所识别的差异中的至少一个差异大于或等于一个或多个预定阈值。 此外,该方法包括:基于确定所识别的差异中的至少一个差异大于或等于一个或多个预定阈值,在数据索引图中记录与所识别的至少一个差异相对应的一个或多个处理结果 (DIM),并且分析DIM的内容以评估车辆的操作条件。
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公开(公告)号:US10011372B2
公开(公告)日:2018-07-03
申请号:US14926669
申请日:2015-10-29
Applicant: THE BOEING COMPANY
Inventor: Jian Dong , Naveed Moayyed Hussain
CPC classification number: B64G1/543 , B64G1/12 , B64G1/546 , B64G2001/525
Abstract: A system is configured to shield an interior chamber of a structure. The system may include a power source, an outer shield assembly operatively connected to the power source and coupled to an outer wall of the structure, and an inner shield assembly surrounding the internal chamber. The outer shield assembly generates a magnetic field through and around the structure. The inner shield assembly deflects radiation particles away from the interior chamber and re-directs portions of the magnetic field around the interior chamber.
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公开(公告)号:US10442559B2
公开(公告)日:2019-10-15
申请号:US15226219
申请日:2016-08-02
Applicant: The Boeing Company
Inventor: Jian Dong , Naveed Moayyed Hussain
IPC: B64G1/54 , B64G1/56 , E04B1/92 , E04C2/284 , E04C2/34 , E04C2/36 , E04C2/52 , B32B5/02 , B32B7/12 , B32B9/00 , B32B15/02 , B32B27/06 , B32B27/12 , B32B27/32 , B32B1/08 , B32B3/08 , B32B3/12 , B64C1/06 , B64C1/12 , B64C1/40
Abstract: A multi-functional composite structure has a modular design that can be altered depending on an extreme environment in which the structure will be exposed such as hazardous radiation, micro-meteoroid and orbital debris impacts, extreme temperature changes, etc. The material combinations employed in the multi-functional composite structure provide a supporting structure with low weight and maximum protection from radiation, debris impacts and temperature variations.
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公开(公告)号:US10116665B2
公开(公告)日:2018-10-30
申请号:US14958017
申请日:2015-12-03
Applicant: The Boeing Company
Inventor: Jian Dong , Michael W. Pieknik , Joshua L. DeLong , Sean T. Johnson
Abstract: This disclosure is directed to securely exchanging information between private domains. Methods and systems of the disclosure perform operations including providing a user identifier (“ID”) and a first session ID to a user of a first private domain. The operations further include receiving from the user a service call for a first analytic service. Additionally, the operations include providing a service message for a second analytic service residing in a second private domain. Moreover, the operations include receiving a first verification message from the second private domain. The operations also include validating the first verification message. The operations further include providing a second verification message. Additionally, the operations include receiving a response message from the second private domain, the response message including information determined by the second analytic service based on job information in the service message.
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公开(公告)号:US20170163659A1
公开(公告)日:2017-06-08
申请号:US14958017
申请日:2015-12-03
Applicant: The Boeing Company
Inventor: Jian Dong , Michael W. Pieknik , Joshua L. DeLong , Sean T. Johnson
IPC: H04L29/06
CPC classification number: H04L63/0815
Abstract: This disclosure is directed to securely exchanging information between private domains. Methods and systems of the disclosure perform operations including providing a user identifier (“ID”) and a first session ID to a user of a first private domain. The operations further include receiving from the user a service call for a first analytic service. Additionally, the operations include providing a service message for a second analytic service residing in a second private domain. Moreover, the operations include receiving a first verification message from the second private domain. The operations also include validating the first verification message. The operations further include providing a second verification message. Additionally, the operations include receiving a response message from the second private domain, the response message including information determined by the second analytic service based on job information in the service message.
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公开(公告)号:US20170121038A1
公开(公告)日:2017-05-04
申请号:US14926669
申请日:2015-10-29
Applicant: THE BOEING COMPANY
Inventor: Jian Dong , Naveed Moayyed Hussain
IPC: B64G1/54
CPC classification number: B64G1/543 , B64G1/12 , B64G1/546 , B64G2001/525
Abstract: A system is configured to shield an interior chamber of a structure. The system may include a power source, an outer shield assembly operatively connected to the power source and coupled to an outer wall of the structure, and an inner shield assembly surrounding the internal chamber. The outer shield assembly generates a magnetic field through and around the structure. The inner shield assembly deflects radiation particles away from the interior chamber and re-directs portions of the magnetic field around the interior chamber.
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公开(公告)号:US09469391B1
公开(公告)日:2016-10-18
申请号:US13871296
申请日:2013-04-26
Applicant: The Boeing Company
Inventor: Jian Dong
CPC classification number: B64C3/56 , B64C3/385 , B64C3/546 , B64C9/34 , B64C23/072 , B64C23/076 , Y02T50/14 , Y02T50/164
Abstract: An adaptive wing for an aircraft includes a first wing portion, a second wing portion, and a third wing portion. The second wing portion is telescopically attached to the first wing portion to selectively change an overall length of the wing based on real-time flight conditions or airport space constraints. The third wing portion is rotate-ably attached to one end of the second wing portion, and a dihedral angle between the second wing portion and the third wing portion is changeable based on real-time flight conditions or airport space constraints.
Abstract translation: 用于飞行器的自适应翼包括第一翼部分,第二翼部分和第三翼部分。 第二翼部分可伸缩地附接到第一翼部分,以基于实时飞行条件或机场空间限制选择性地改变翼的总长度。 第三翼部分旋转地附接到第二翼部的一端,并且第二翼部和第三翼部之间的二面角可以基于实时飞行条件或机场空间限制而改变。
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8.
公开(公告)号:US10281913B2
公开(公告)日:2019-05-07
申请号:US15676380
申请日:2017-08-14
Applicant: The Boeing Company
Inventor: Jian Dong , Naveed Moayyed Hussain
Abstract: An example method for predictive take-off rejection (TOR) of an aircraft includes receiving, at a computing device on the aircraft and at a time before the aircraft takes off for a current flight, outputs from a plurality of sensors positioned on the aircraft, comparing the outputs received from the plurality of sensors for the current flight to reference flight data, based on comparing the outputs received from the plurality of sensors for the current flight to the reference flight data the computing device making a determination of whether to initiate a TOR procedure before the aircraft reaches a takeoff speed on a runway, and based on determining to initiate the TOR procedure, the computing device sending a signal to a control device on the aircraft to initiate the TOR procedure.
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9.
公开(公告)号:US20190049953A1
公开(公告)日:2019-02-14
申请号:US15676380
申请日:2017-08-14
Applicant: The Boeing Company
Inventor: Jian Dong , Naveed Moayyed Hussain
Abstract: An example method for predictive take-off rejection (TOR) of an aircraft includes receiving, at a computing device on the aircraft and at a time before the aircraft takes off for a current flight, outputs from a plurality of sensors positioned on the aircraft, comparing the outputs received from the plurality of sensors for the current flight to reference flight data, based on comparing the outputs received from the plurality of sensors for the current flight to the reference flight data the computing device making a determination of whether to initiate a TOR procedure before the aircraft reaches a takeoff speed on a runway, and based on determining to initiate the TOR procedure, the computing device sending a signal to a control device on the aircraft to initiate the TOR procedure.
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公开(公告)号:US20180037342A1
公开(公告)日:2018-02-08
申请号:US15226219
申请日:2016-08-02
Applicant: The Boeing Company
Inventor: Jian Dong , Naveed Moayyed Hussain
CPC classification number: B64G1/54 , B32B1/08 , B32B3/08 , B32B3/12 , B32B5/02 , B32B7/12 , B32B9/007 , B32B15/02 , B32B27/065 , B32B27/12 , B32B27/32 , B32B2250/05 , B32B2250/40 , B32B2262/0253 , B32B2262/0269 , B32B2262/105 , B32B2262/106 , B32B2262/14 , B32B2266/0278 , B32B2307/202 , B32B2307/212 , B32B2307/304 , B32B2307/558 , B32B2307/56 , B32B2307/71 , B32B2307/7246 , B32B2571/02 , B32B2605/00 , B32B2605/18 , B64C1/064 , B64C1/12 , B64C1/406 , B64C2001/0072 , B64D2221/00 , B64G1/56 , E04B1/92 , E04B2001/925 , E04C2/284 , E04C2/3405 , E04C2/365 , E04C2/521 , E04C2/526 , E04C2002/345
Abstract: A multi-functional composite structure has a modular design that can be altered depending on an extreme environment in which the structure will be exposed such as hazardous radiation, micro-meteoroid and orbital debris impacts, extreme temperature changes, etc. The material combinations employed in the multi-functional composite structure provide a supporting structure with low weight and maximum protection from radiation, debris impacts and temperature variations.
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