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公开(公告)号:US11794923B2
公开(公告)日:2023-10-24
申请号:US17276559
申请日:2019-09-20
Applicant: Eaton Intelligent Power Limited
Inventor: Abhijit A. Bodkhe , Ashok K. Vishwakarma , Jaspal Rawat , Steven Hum , Parag More , Chandrashekhar S. Nehete , Robert L. Sbonek , Jeffrey M. Laing , Taruna Khandelwal , Vivek Agarwal
CPC classification number: B64F1/28 , B64D37/16 , G05B19/052 , G05B23/0232 , B67D7/0401
Abstract: An aircraft refueling system (10) includes a master controller (12), a fleet controller (14) in communication with the master controller, a platform controller (18) in communication with the fleet controller, and a fuel control system (16) in communication with the platform controller. Embodiments of an aircraft refueling system may include a primary pressure controller (20), a secondary pressure controller (22), a programmable logic controller (24), and a data logger controller (26). The master controller may be configured to receive and analyze data from at least one of the fleet controller, the platform controller, and the fuel control system; and to modify operational parameters or upgrade the fuel control system based at least in part on the analysis of received data.
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公开(公告)号:US20180319514A1
公开(公告)日:2018-11-08
申请号:US15961070
申请日:2018-04-24
Applicant: Eaton Intelligent Power Limited
Inventor: Parag More , Ashok K. Vishwakarma
CPC classification number: B64F1/28 , B60K15/04 , B60K2015/0483
Abstract: A fluid coupler includes a housing with an inlet port and an outlet port, a piston disposed in the housing and configured to control fluid flow between the inlet port and the outlet port, and a piston retainer disposed in the housing. A piston may include at least one radially-extending support member, and the radially-extending support member may include an aperture. The at least one radially-extending support member may be substantially planar.
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