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公开(公告)号：US10282077B2
公开(公告)日：2019-05-07
申请号：US14851690
申请日：2015-09-11
申请人： Exelis Inc.
发明人： Christopher F. Rossano , Lado Tonia , Joel Kimble
IPC分类号： G06F3/0487 , B64F5/20 , G06F3/0484
摘要： An apparatus for monitoring and controlling operations for deicing aircraft at an airport facility includes a display device configured to display a visual data presentation of deicing operations data. The visual data presentation including at least one map depicting: a visual representation of at least one aircraft participating in a deicing process, wherein the visual representation of the aircraft includes attributes identifying the aircraft and indicating a stage of the deicing process the aircraft is undergoing; and a visual representation of a deicing facility with a plurality of deicing bays for deicing aircraft, wherein the visual representation of the deicing facility presents each of the deicing bays as a distinct geofenced area with display attributes indicating an operating status of each of the deicing bays.
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公开(公告)号：US12103051B2
公开(公告)日：2024-10-01
申请号：US17108889
申请日：2020-12-01
发明人： J. David Smith , Sushant Anand , Srinivas Prasad Bengaluru Subramanyam , Konrad Rykaczewski , Kripa K. Varanasi
IPC分类号： B08B17/06 , B64D15/06 , B64F5/20 , C09D5/16 , C09D167/00 , C09D179/08 , C09D183/04 , F28F19/00
CPC分类号： B08B17/065 , B64D15/06 , B64F5/20 , C09D5/1656 , C09D5/1662 , C09D5/1675 , C09D5/1681 , C09D5/1693 , C09D167/00 , C09D179/08 , C09D183/04 , F28F19/006 , F28F2245/04
摘要： In certain embodiments, the invention is directed to apparatus comprising a liquid-impregnated surface, said surface comprising an impregnating liquid and a matrix of solid features spaced sufficiently close to stably contain the impregnating liquid therebetween or therewithin, and methods thereof. In some embodiments, one or both of the following holds: (i) 0
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公开(公告)号：US20220411105A1
公开(公告)日：2022-12-29
申请号：US17362372
申请日：2021-06-29
申请人： Air T, Inc.
发明人： Jeffrey C. Walsh
摘要： Devices, systems, and methods for remote deicing/anti-icing of an aircraft are described herein. One remote operator deicing/anti-icing station located in a remote location from a deicing/anti-icing rig includes a number of remote rig control components for actuation by a remote operator, wherein the remote rig control components include a remote operator user interface, located outside of a rig being at least partially controlled by the remote operator deicing/anti-icing station, the rig including a truck and a deicing/anti-icing control cabin that controls disbursement of substances to deice/anti-ice an aircraft, and a communication device that communicates instructions from the remote operator user interface and the number of remote rig control components to the rig to control at least one of the truck and the deicing/anti-icing control cabin.
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公开(公告)号：US20180229860A1
公开(公告)日：2018-08-16
申请号：US15743024
申请日：2015-09-07
申请人： GUINAULT S.A.
发明人： LIONEL CLERMONT , CHAFA CHAOURAR
CPC分类号： B64F1/364 , B64F1/228 , B64F1/28 , B64F1/315 , B64F1/34 , B64F1/368 , B64F5/20 , B64F5/40 , G05D1/0278 , G07C5/008
摘要： An aircraft ground support unit (1) for supplying a service to an aircraft (3) on the ground according to a specific servicing program is provided that includes reception means (5) suitable for identifying an aircraft (3) in motion or parked on the ground by receiving information emitted by a transponder (7) of said aircraft including an instantaneous GPS coordinates of the position of the aircraft, the identity of the aircraft, the type of aircraft, and the company of the aircraft, aircraft status data. A microprocessor is provided that is suitable for selecting and implementing a predefined servicing program stored in a database corresponding to the type and company of the thus identified aircraft (3) on the basis of the information received by the reception means. A data record device is also provided that is to store the events, aircraft status data, ground unit data for airlines operation optimization.
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公开(公告)号：US12084204B2
公开(公告)日：2024-09-10
申请号：US17362372
申请日：2021-06-29
申请人： Air T, Inc.
发明人： Jeffrey C. Walsh
摘要： Devices, systems, and methods for remote deicing/anti-icing of an aircraft are described herein. One remote operator deicing/anti-icing station located in a remote location from a deicing/anti-icing rig includes a number of remote rig control components for actuation by a remote operator, wherein the remote rig control components include a remote operator user interface, located outside of a rig being at least partially controlled by the remote operator deicing/anti-icing station, the rig including a truck and a deicing/anti-icing control cabin that controls disbursement of substances to deice/anti-ice an aircraft, and a communication device that communicates instructions from the remote operator user interface and the number of remote rig control components to the rig to control at least one of the truck and the deicing/anti-icing control cabin.
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公开(公告)号：US20210291243A1
公开(公告)日：2021-09-23
申请号：US17108889
申请日：2020-12-01
发明人： J. David Smith , Sushant Anand , Srinivas Prasad Bengaluru Subramanyam , Konrad Rykaczewski , Kripa K. Varanasi
IPC分类号： B08B17/06 , C09D5/16 , B64F5/20 , B64D15/06 , C09D167/00 , C09D179/08 , C09D183/04
摘要： In certain embodiments, the invention is directed to apparatus comprising a liquid-impregnated surface, said surface comprising an impregnating liquid and a matrix of solid features spaced sufficiently close to stably contain the impregnating liquid therebetween or therewithin, and methods thereof. In some embodiments, one or both of the following holds: (i) 0
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公开(公告)号：US09776737B2
公开(公告)日：2017-10-03
申请号：US14351711
申请日：2011-11-21
申请人： Stefan Vestergaard , Elo Svanebjerg
发明人： Stefan Vestergaard , Elo Svanebjerg
摘要： A method for de-icing liquid on a surface of an airplane includes supplying de-icing liquid to and through a spraying nozzle of a de-icing vehicle through a pipe that connects the nozzle with a tank assembly of the de-icing vehicle, where the liquid is delivered to the spraying nozzle as a mix of an anti-freeze liquid and additives, the anti-freeze liquid is delivered to the pipe from an anti-freeze liquid tank via a first dosage pump, and the additives are delivered from an additives tank via a second dosage pump.
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公开(公告)号：US20240308686A1
公开(公告)日：2024-09-19
申请号：US18575920
申请日：2021-07-13
申请人： ATHENA PI
发明人： Lionel Clermont
摘要： An aircraft ground support unit (1) (GSU) for supplying a specific service according to a specific set of service parameters to an aircraft (2) on the ground and consuming a specific service energy is provided that includes:
a rechargeable energy storage unit (3) (RESU) for autonomously delivering the specific service energy required for supplying the specific service in the given available service duration;
an energy sensor (4) for measuring an instantaneous state of energy parameters of the RESU; and
a control unit. The RESU,
identifying the aircraft (2),
identifying in a database the specific set of service parameters for identified aircraft,
establishing a specific service energy budget estimate,
determining an instantaneous charge level of the RESU,
comparing the specific service energy budget estimate with the instantaneous charge level of the RESU, and
generating an output signal representative of a capacity of the RESU to deliver the specific service energy budget estimate as a function of the instantancous charge level.-
公开(公告)号：US11214381B2
公开(公告)日：2022-01-04
申请号：US15227501
申请日：2016-08-03
发明人： Anthony Jones , Andre Julien , David Menheere , Jean Thomassin , Richard Ullyott , Daniel Van Den Hende
摘要： An aircraft heating assembly including an internal combustion engine having a liquid coolant system distinct from any fuel and lubricating system of the engine and including cooling passages in the internal combustion engine for circulating a liquid coolant from a coolant inlet to a coolant outlet, a coolant circulation path outside of the internal combustion engine and in fluid communication with the coolant inlet and the coolant outlet, and a heating element in heat exchange relationship with a portion of the aircraft to be heated. The coolant circulation path extends through a heat exchanger configured to remove a portion of a waste heat from the liquid coolant. The heating element is in heat exchange relationship with the coolant circulation path to receive another portion of the waste heat therefrom. A method of heating a portion of an aircraft is also discussed.
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公开(公告)号：US10882085B2
公开(公告)日：2021-01-05
申请号：US14443620
申请日：2013-11-19
发明人： J. David Smith , Sushant Anand , Srinivas Prasad Bengaluru Subramanyam , Konrad Rykaczewski , Kripa K. Varanasi
IPC分类号： B32B37/02 , B08B17/06 , C09D5/16 , B64F5/20 , B64D15/06 , C09D167/00 , C09D179/08 , C09D183/04 , F28F19/00
摘要： In certain embodiments, the invention is directed to apparatus comprising a liquid-impregnated surface, said surface comprising an impregnating liquid and a matrix of solid features spaced sufficiently close to stably contain the impregnating liquid therebetween or therewithin, and methods thereof. In some embodiments, one or both of the following holds: (i) 0
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