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公开(公告)号：US12129037B2
公开(公告)日：2024-10-29
申请号：US18054624
申请日：2022-11-11
Applicant: Textron Aviation Inc.
Inventor： Robert Glynn Wiegers , Clinton Lee Thompson , Robin L. Young
CPC classification number: B64D13/08 , B60H1/0073 , G05D23/1931 , B64D2013/0618
Abstract: A method for heating an unpressurized aircraft includes receiving a desired air temperature, calculating a target duct air temperature based on the desired air temperature, determining an actual duct air temperature via a duct air temperature sensor, calculating a target modulation of one or more ram air valves based on a difference between the target duct air temperature and the actual duct air temperature, modulating one or more of the ram air valves based on the target modulation, introducing a bleed air from a turbine engine to a heat exchanger, introducing a temperature control air from one of the one or more ram air valves to the heat exchanger for cooling the bleed air to provide a temperature-controlled air, mixing the temperature-controlled air from the heat exchanger with an ejector ram air in an ejector, and providing air from the ejector to an occupied compartment of the unpressurized aircraft.
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公开(公告)号：US11528165B2
公开(公告)日：2022-12-13
申请号：US16225056
申请日：2018-12-19
Applicant: Textron Aviation Inc.
Inventor： Joseph Andrew Ohol , Robin L. Young
IPC: H04L12/403 , B64F5/60 , H04L67/12 , H04L12/46 , H04L12/40
Abstract: A remote sensor data acquisition system for an aircraft includes a plurality of remote sensors co-located onboard the aircraft and adapted to measure one or more aircraft-related parameters. A remote sensor interface is co-located with the plurality of remote sensors. The remote sensor interface includes a communication bus having a plurality of nodes to transmit data from the plurality of remote sensors. A plurality of subsystems are each adapted to receive data from the plurality of remote sensors simultaneously and in real time via the remote sensor interface. A remote sensor data acquisition method for an aircraft includes sensing one or more parameters onboard the aircraft via a plurality of remote sensors and transmitting sensor data from the plurality of remote sensors to a plurality of subsystems independently and in real time via a remote sensor interface.
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公开(公告)号：US20230142953A1
公开(公告)日：2023-05-11
申请号：US18054624
申请日：2022-11-11
Applicant: Textron Aviation Inc.
Inventor： Robert Glynn Wiegers , Clinton Lee Thompson , Robin L. Young
CPC classification number: B64D13/08 , G05D23/1931 , B60H1/0073 , B64D2013/0618
Abstract: A method for heating an unpressurized aircraft includes receiving a desired air temperature, calculating a target duct air temperature based on the desired air temperature, determining an actual duct air temperature via a duct air temperature sensor, calculating a target modulation of one or more ram air valves based on a difference between the target duct air temperature and the actual duct air temperature, modulating one or more of the ram air valves based on the target modulation, introducing a bleed air from a turbine engine to a heat exchanger, introducing a temperature control air from one of the one or more ram air valves to the heat exchanger for cooling the bleed air to provide a temperature-controlled air, mixing the temperature-controlled air from the heat exchanger with an ejector ram air in an ejector, and providing air from the ejector to an occupied compartment of the unpressurized aircraft.
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公开(公告)号：US20190229947A1
公开(公告)日：2019-07-25
申请号：US16225056
申请日：2018-12-19
Applicant: Textron Aviation Inc.
Inventor： Joseph Andrew Ohol , Robin L. Young
IPC: H04L12/403 , H04L29/08 , B64F5/60
Abstract: A remote sensor data acquisition system for an aircraft includes a plurality of remote sensors co-located onboard the aircraft and adapted to measure one or more aircraft-related parameters. A remote sensor interface is co-located with the plurality of remote sensors. The remote sensor interface includes a communication bus having a plurality of nodes to transmit data from the plurality of remote sensors. A plurality of subsystems are each adapted to receive data from the plurality of remote sensors simultaneously and in real time via the remote sensor interface. A remote sensor data acquisition method for an aircraft includes sensing one or more parameters onboard the aircraft via a plurality of remote sensors and transmitting sensor data from the plurality of remote sensors to a plurality of subsystems independently and in real time via a remote sensor interface.
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