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公开(公告)号：US12116146B2
公开(公告)日：2024-10-15
申请号：US18121788
申请日：2023-03-15
申请人： BETA AIR, LLC
发明人： John Charles Palombini , Jake Pill
CPC分类号： B64F5/40 , B64D27/24 , B64D33/08 , B60L58/26 , B60L58/32 , B60L58/33 , B60L58/34 , B60L2240/545
摘要： A system for thermal management ground service equipment and a method of use is disclosed. The system may include ground service equipment, wherein the ground service equipment may be configured to manage a temperature of a power source of an electric aircraft. The ground service equipment may include a coolant source, wherein the coolant source may include a reservoir containing a coolant. The ground service equipment may include a coolant heating system, wherein the coolant heating system may be configured to increase thermal energy of the coolant. The coolant heating system may include an electric resistance heating element. The system may include a controller communicatively connected to the ground service equipment, wherein the controller may be configured to receive an optimal temperature of the coolant and control the electric resistance heating element of the coolant heating system to increase the thermal energy of the coolant to the optimal temperature.
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公开(公告)号：US12103710B1
公开(公告)日：2024-10-01
申请号：US18341459
申请日：2023-06-26
发明人： Tanner Jones , Gabriel Myers
摘要： A stand for holding a flight control surface of an aircraft wing. The stand has a longitudinal spine supported by plural uprights and supporting at least two hanger assemblies. Each hanger assembly has attachment points transversely outboard of the spine. Rods articulably depend downwardly from the respective attachment points to be articulably connected at a cradle. The cradle is configured to fixedly hold an aircraft flight control surface for maintenance. By adjusting the transverse spacing of the rods from the spine, the attitude of the flight control surface can be adjusted as needed for a particular maintenance task.
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公开(公告)号：US20240308693A1
公开(公告)日：2024-09-19
申请号：US18602536
申请日：2024-03-12
发明人： Jacques FOURNIE , Julien POTEAU , Noël PERNALON
摘要： A support for the maintenance of an aircraft radome comprising an annular element having a flat surface and from which extend at least three feet. The support comprising a plurality of articulated holding elements, for example articulated fittings, applying a lock function and each comprising a bearing surface on a surface portion of an aircraft radome, for example an interface fitting, when said radome is placed on said flat surface of said annular element.
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公开(公告)号：US20240308691A1
公开(公告)日：2024-09-19
申请号：US18121788
申请日：2023-03-15
申请人： BETA AIR, LLC
发明人： John Charles Palombini , Jake Pill
CPC分类号： B64F5/40 , B64D27/24 , B64D33/08 , B60L58/26 , B60L58/32 , B60L58/33 , B60L58/34 , B60L2240/545
摘要： A system for thermal management ground service equipment and a method of use is disclosed. The system may include ground service equipment, wherein the ground service equipment may be configured to manage a temperature of a power source of an electric aircraft. The ground service equipment may include a coolant source, wherein the coolant source may include a reservoir containing a coolant. The ground service equipment may include a coolant heating system, wherein the coolant heating system may be configured to increase thermal energy of the coolant. The coolant heating system may include an electric resistance heating element. The system may include a controller communicatively connected to the ground service equipment, wherein the controller may be configured to receive an optimal temperature of the coolant and control the electric resistance heating element of the coolant heating system to increase the thermal energy of the coolant to the optimal temperature.
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公开(公告)号：US20240270409A1
公开(公告)日：2024-08-15
申请号：US18646108
申请日：2024-04-25
发明人： Daniel MACKAY
摘要： A system for an aircraft, comprises an electric energy module; and a connector module operatively connected to the electric energy module. The connector module is: structured to attach the electric energy module to the aircraft when the connector module in an engaged mode while in use, and operable between the engaged mode and a disengaged mode, the connector module in the disengaged mode while in use disengaging the electric energy module from the aircraft.
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6.发明公开公开(公告)号：US20240265351A1
公开(公告)日：2024-08-08
申请号：US18564865
申请日：2022-06-03
申请人： LEONARDO S.P.A.
发明人： Alessandro Collini , Andrea Piccoli
摘要： Method implemented through a computer for determining a maintenance plan of a group of aircraft, comprising receiving a data structure with a plurality of groups of values associated with a plurality of flights of the aircraft, wherein each flight has a duration, each group of values relates to a physical quantity associated with the use of an aircraft, and wherein each group of values is acquired during a flight by a detection system coupled to an aircraft. The method further comprises identifying one or more representative flights from the plurality of flights, starting from the data structure and using at least one statistical test, wherein the groups of values associated with the representative flights are, from a statistical viewpoint, values of typical use of the group of aircraft; determining a load sequence comprising the groups of values associated with the representative flights repeated a number of times, as a function of the duration of the respective representative flight; and determining a state of use of the group of aircraft, starting from the load sequence.
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公开(公告)号：US12053847B2
公开(公告)日：2024-08-06
申请号：US17888624
申请日：2022-08-16
发明人： Craig M. Beers , Lino S. Italia , John M. Beck
CPC分类号： B23P6/00 , B23K15/0053 , B23P6/002 , B64F5/40
摘要： A replacement compressor outlet housing includes a compressor outlet housing, having a volute and a radially inwardly extending finger extending from a radially inner end of the volute. The radially inwardly extending finger is welded to an insert. The insert has a bearing support defining a bore. The insert has a web connecting a ledge to the bearing support. The radially inwardly extending finger welded to the ledge.
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公开(公告)号：US12036623B2
公开(公告)日：2024-07-16
申请号：US17498270
申请日：2021-10-11
发明人： Mark W. Knight , Patrick W. Shindo , Connor Limburg , Jesse Tice
CPC分类号： B23K26/009 , B05D5/067 , B05D7/5883 , B23K26/362 , B64C1/12 , B64F5/40
摘要： An aircraft skin coating assembly for an aircraft. The coating assembly includes a primer layer deposited on the aircraft skin, an optical stop-etch layer deposited on the primer layer that is reflective at a predetermined wavelength, a coating stack-up deposited on the optical etch-stop layer that provides performance features for the aircraft, and a sealant layer deposited on the stack-up. When a laser coating removal process employing a laser beam is used to remove the coating stack-up for replacement, the stop-etch layer reflects the laser beam to prevent it from penetrating and possibly damaging the aircraft skin.
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公开(公告)号：US11999509B2
公开(公告)日：2024-06-04
申请号：US17322739
申请日：2021-05-17
发明人： Daniel Mackay
摘要： A system for an aircraft includes an electric energy module and a connector module operatively connected to the electric energy module. The connector module is: structured to attach the electric energy module to the aircraft when the connector module is in an engaged mode while in use, and operable between the engaged mode and a disengaged mode. The connector module in the disengaged mode while in use disengages the electric energy module from the aircraft.
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10.发明公开公开(公告)号：US20240174379A1
公开(公告)日：2024-05-30
申请号：US18519418
申请日：2023-11-27
申请人： Airbus SAS , Airbus Operations GmbH
摘要： A method for determining a probability of occurrence of a malfunction creating a performance defect in an aircraft makes it possible to process a set of input data so as to retain only measurements relevant with regard to determining the probability of occurrence of the malfunction following a previous event. In other words, the method makes it possible to refine a set of input data so as to establish relevant causal links between records of measurements and a malfunction, so as to determine a probability of occurrence of a malfunction based on the occurrence of one or more previous events.
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