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1.
公开(公告)号:US09580180B2
公开(公告)日:2017-02-28
申请号:US14200263
申请日:2014-03-07
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Michel A. Jonqueres , Roy Araki
CPC classification number: B64D13/08 , B64D13/06 , B64D2013/0618 , B64D2013/0674 , Y02T50/56
Abstract: An aircraft environmental control system (ECS) may be configured to operate in first mode and a second mode. The ECS may include an air cycle machine (ACM), a by-pass valve positioned to allow bleed air to by-pass the air cycle machine so that when the by-pass valve is open, the ECS operates in the first mode with bleed air at a first pressure and when the by-pass valve is closed the ECS operates in the second mode at a second bleed air pressure, higher than the first bleed air pressure. A bleed air system controller and ECS controller may be configured to selectively couple high pressure or low pressure bleed air ports of an engine of an aircraft to the ECS and control the by-pass valve position.
Abstract translation: 飞机环境控制系统(ECS)可以被配置为在第一模式和第二模式下操作。 ECS可以包括空气循环机(ACM),旁路阀,其设置成允许排放空气绕过空气循环机,使得当旁通阀打开时,ECS在第一模式下以流出 空气处于第一压力,并且当旁通阀关闭时,ECS在第二排气压力下工作在第二模式,高于第一排气压力。 排气系统控制器和ECS控制器可以被配置为选择性地将飞机发动机的高压或低压排放空气端口耦合到ECS并控制旁路阀位置。
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公开(公告)号:US10242508B2
公开(公告)日:2019-03-26
申请号:US15402910
申请日:2017-01-10
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Kyusung Kim , Qingqiu Ginger Shao , Roy Araki , Andrew Earl , Bin Dong , Wenyan Guo , Eric Shi
Abstract: A maintenance system is provided for an environmental conditioning element of an environmental control system of a vehicle. The maintenance system includes a data acquisition module configured to determine an ambient temperature, an altitude of the vehicle, and a measured ECS compressor temperature; a fouling module coupled to receive the ambient temperature, the altitude, and the measured ECS compressor temperature from the data acquisition module and configured to generate a fouling condition of the environmental conditioning element based on at least the ambient temperature, the altitude, and the measured ECS compressor temperature; and a reporting module coupled to receive the fouling condition from the fouling module and configured to generate a report for a user that includes the fouling condition.
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公开(公告)号:US11780591B2
公开(公告)日:2023-10-10
申请号:US16949993
申请日:2020-11-23
Applicant: Honeywell International Inc.
Inventor: Kyusung Kim , Qingqiu Ginger Shao , Roy Araki , Bin Dong , Qi Li , Gary Kumagai
IPC: B64D13/06
CPC classification number: B64D13/06 , B64D2013/0611
Abstract: An example system for determining a performance status of an environmental control system (ECS) in a vehicle includes memory and processing circuitry. The processing circuitry is configured to determine, based on one or more of the aircraft data, the weather data, or the trending data, an estimated compressor exit temperature. The processing circuitry is configured to determine a current residual compressor exit temperature based on the estimated compressor exit temperature and a current compressor exit temperature. The processing circuitry is configured to determine whether a residual condition is met based at least in part on the residual compressor exit temperature and whether a pack condition is met based at least in part on a pack temperature. The processing circuitry is configured to provide an indication of the performance status of the ECS based on at least one of the residual condition or the pack condition being met.
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公开(公告)号:US20220161931A1
公开(公告)日:2022-05-26
申请号:US16949993
申请日:2020-11-23
Applicant: Honeywell International Inc.
Inventor: Kyusung Kim , Qingqiu Ginger Shao , Roy Araki , Bin Dong , Qi Li , Gary Kumagai
IPC: B64D13/06
Abstract: An example system for determining a performance status of an environmental control system (ECS) in a vehicle includes memory and processing circuitry. The processing circuitry is configured to determine, based on one or more of the aircraft data, the weather data, or the trending data, an estimated compressor exit temperature. The processing circuitry is configured to determine a current residual compressor exit temperature based on the estimated compressor exit temperature and a current compressor exit temperature. The processing circuitry is configured to determine whether a residual condition is met based at least in part on the residual compressor exit temperature and whether a pack condition is met based at least in part on a pack temperature. The processing circuitry is configured to provide an indication of the performance status of the ECS based on at least one of the residual condition or the pack condition being met.
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公开(公告)号:US20180197350A1
公开(公告)日:2018-07-12
申请号:US15402910
申请日:2017-01-10
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Kyusung Kim , Qingqiu Ginger Shao , Roy Araki , Andrew Earl , Bin Dong , Wenyan Guo , Eric Shi
CPC classification number: G07C5/006 , B64D13/02 , B64D13/08 , B64D45/00 , B64D2013/0603 , B64D2045/0085 , G05B23/0254 , G05B23/0283 , G05B2219/2614 , G05B2219/2638 , G05B2219/45071
Abstract: A maintenance system is provided for an environmental conditioning element of an environmental control system of a vehicle. The maintenance system includes a data acquisition module configured to determine an ambient temperature, an altitude of the vehicle, and a measured ECS compressor temperature; a fouling module coupled to receive the ambient temperature, the altitude, and the measured ECS compressor temperature from the data acquisition module and configured to generate a fouling condition of the environmental conditioning element based on at least the ambient temperature, the altitude, and the measured ECS compressor temperature; and a reporting module coupled to receive the fouling condition from the fouling module and configured to generate a report for a user that includes the fouling condition.
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6.
公开(公告)号:US20150251765A1
公开(公告)日:2015-09-10
申请号:US14200263
申请日:2014-03-07
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Michel A. Jonqueres , Roy Araki
IPC: B64D13/08
CPC classification number: B64D13/08 , B64D13/06 , B64D2013/0618 , B64D2013/0674 , Y02T50/56
Abstract: An aircraft environmental control system (ECS) may be configured to operate in first mode and a second mode. The ECS may include an air cycle machine (ACM), a by-pass valve positioned to allow bleed air to by-pass the air cycle machine so that when the by-pass valve is open, the ECS operates in the first mode with bleed air at a first pressure and when the by-pass valve is closed the ECS operates in the second mode at a second bleed air pressure, higher than the first bleed air pressure. A bleed air system controller and ECS controller may be configured to selectively couple high pressure or low pressure bleed air ports of an engine of an aircraft to the ECS and control the by-pass valve position.
Abstract translation: 飞机环境控制系统(ECS)可以被配置为在第一模式和第二模式下操作。 ECS可以包括空气循环机(ACM),旁路阀,其设置成允许排放空气绕过空气循环机,使得当旁通阀打开时,ECS在第一模式下以流出 空气处于第一压力,并且当旁通阀关闭时,ECS在第二排气压力下工作在第二模式,高于第一排气压力。 排气系统控制器和ECS控制器可以被配置为选择性地将飞机发动机的高压或低压排放空气端口耦合到ECS并控制旁路阀位置。
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