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公开(公告)号：US20240270388A1
公开(公告)日：2024-08-15
申请号：US18629328
申请日：2024-04-08
申请人： ZSM HOLDINGS LLC
发明人： Jason C. Bell , Etan D. Karni , Scott David Rewerts , Ravi Singh
IPC分类号： B64D9/00 , B64C1/06 , B64C1/14 , B64C1/20 , B64C1/22 , B64C3/32 , B64C3/34 , B64C17/08 , B64D37/04 , B64F1/32 , F03D13/40
CPC分类号： B64D9/003 , B64C1/0683 , B64C1/1415 , B64C1/20 , B64C1/22 , B64C3/32 , B64C3/34 , B64C17/08 , B64D9/00 , B64D37/04 , B64F1/32 , F03D13/40 , B64D2009/006 , F05B2260/02
摘要： Systems and methods for loading a cargo aircraft are described. The system includes at least one rail disposed in an interior cargo bay of a cargo aircraft that extends at an angle relative to an interior bottom contact surface of a forward portion of the interior cargo bay, through a kinked portion and an aft portion of the interior cargo bay. Payload-receiving fixtures are described that can be used in conjunction with the rail system, allowing for large cargo, such as wind turbine blades, to be transported by aircraft. Methods of loading a cargo aircraft can include advancing the large payload into the interior cargo bay of the aircraft such that at least one of the payload-receiving fixtures rises relative to a plane defined by the interior bottom contact surface of the forward portion of the interior cargo bay. Various systems, methods, components, and related tooling are also provided.
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公开(公告)号：US12054256B2
公开(公告)日：2024-08-06
申请号：US17865058
申请日：2022-07-14
申请人： Wing Aviation LLC
发明人： Jesse Blake , Andre Prager , Evan Twyford , Ivan Qiu , Jasper Lewin
IPC分类号： B64C1/20 , B64C39/02 , B64D1/02 , B64D9/00 , B64U101/60
CPC分类号： B64C39/024 , B64C1/20 , B64D9/003 , B64D1/02 , B64U2101/60
摘要： A unmanned aerial vehicle (UAV) includes a fuselage body including a cavity that forms a cargo bay for transporting a payload, an upper access opening for receiving the payload into the cargo bay from a first direction, and a lower access opening for lowering the payload from the cargo bay. The UAV also includes an upper door associated with the upper access opening that is movable between a closed position in which the upper access opening is obstructed and an open position providing a path for the payload into the cargo bay. The upper door includes a winch configured to unwind or retract a tether secured to the payload.
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3.发明授权公开(公告)号：US12017794B2
公开(公告)日：2024-06-25
申请号：US17226962
申请日：2021-04-09
申请人： Goodrich Corporation
发明人： Brandon David Lee , Wallace Harold Larson , Alexander Mitchell Heyd , Lynne M Almvig , Zachary Meyer
摘要： A cargo restraint system includes a driving shaft, a first restraint, and a second restraint. The first restraint is operatively coupled to the driving shaft via a first indexing mechanism arrangement. The second restraint is operatively coupled to the driving shaft via a second indexing mechanism arrangement. The first and second indexing mechanism arrangements are arranged such that rotation of the driving shaft in a first rotational direction causes the first restraint to rotate between a lowered position and a raised position, and further rotation of the driving shaft in the same rotational direction causes the second restraint to rotate between the lowered position and the raised position. The first restraint may be axially offset from the second restraint to allow sequential loading and unloading of cargo.
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公开(公告)号：US11987365B2
公开(公告)日：2024-05-21
申请号：US17749013
申请日：2022-05-19
发明人： Torsten Noebel , Andreas Dresel , Mathieu Bonnet
CPC分类号： B64D11/0696 , B64C1/20
摘要： A device for attaching an object to an attachment rail, particularly a seat rail, in an aircraft or spacecraft. A base part has a support surface to be placed onto an outer surface of the rail, and a locking element to partially protrude from the support surface along a line of protrusion. The base part and locking element are coupled or configured to be coupled wherein the locking element can be moved relative to the base part along the line of protrusion and rotated with respect to the base part. An end section of the locking element has a tip portion shaped in a dovetail-type manner. The device includes a tensioning arrangement for tensioning the locking element with respect to the rail. An arrangement includes such a device as well as an attachment rail with a rail main body and a plurality of bushes. A method for attaching an object, and a seat rail are disclosed.
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公开(公告)号：US11945569B2
公开(公告)日：2024-04-02
申请号：US17586134
申请日：2022-01-27
CPC分类号： B64C1/20 , B64D11/0696 , C23C30/00 , C23F11/185
摘要： An anchor rail for an aircraft floor includes an upper flange with a guideway and two flange wings. The rail is formed of a beam and of an anti-corrosion protection. The beam is formed at least of a body made from a first material and defining the lower stiffening structure and an upper platform. The anti-corrosion protection wholly covers an upper face of the upper platform and therewith constitutes the upper flange of the rail, thus layered. The anti-corrosion protection is at least formed of a protective sheet made of a second material more resistant to corrosion than the first material and selected from a metal and a fiber-reinforced plastic composite material. Such a rail exhibits good corrosion resistance for modest cost.
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6.发明授权公开(公告)号：US11807393B2
公开(公告)日：2023-11-07
申请号：US17362052
申请日：2021-06-29
发明人： Oliver Nuessen , Martin Guse , Dirk Meiranke , Sascha Nowarre , Dennis Fischer , Uwe Panzram , Matthias Horst
CPC分类号： B64D9/003 , B64C1/20 , B64D2009/006
摘要： In an aircraft, bi-stable power drive units (PDUs) move and secure cargo within an aircraft cargo hold. Such a PDU includes a frame, by which the PDU is rigidly attached to the cargo hold floor; a body pivotably attached, via a hinge, at a first end of the frame at least one drive roller attached at a second end of the body; and an actuator attached to the body and which causes a pivoting angular movement of the body, relative to the frame, about the hinge. The actuator maintains an angular position of the body relative to the frame even upon a loss of power to the PDU. The body is movable between and including a retracted position and a deployed position. A cargo management system includes a plurality of such PDUs, at least one having a controlled area network (CAN) bus interface to control and communicate with a controller.
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公开(公告)号：US11807392B2
公开(公告)日：2023-11-07
申请号：US17361999
申请日：2021-06-29
发明人： Oliver Nuessen , Martin Guse , Dirk Meiranke , Sascha Nowarre , Dennis Fischer , Uwe Panzram , Matthias Horst
CPC分类号： B64D9/003 , B64C1/20 , B64D2009/006
摘要： A system for ensuring proper installation of components of a cargo management system within a cargo hold has cleats rigidly attached to a floor of the cargo hold, a first subset of the cleats having insets of a first shape, a second subset of cleats having insets of a second shape, keys and rotatable fasteners attached to the components of the cargo management system, a first subset of the keys having the first shape and a second subset of the keys having the second shape. The first subset of keys can only engage with the first subset of cleats and the second subset of keys can only engage with the second subset of cleats and the rotatable fasteners utilize a rotary movement to secure the components of the cargo management system to a respective cleat, against which the rotary fastener is engaged.
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公开(公告)号：US11772796B2
公开(公告)日：2023-10-03
申请号：US17048631
申请日：2019-04-23
摘要： An item to be secured to an aircraft floor can be secured to a Load Transfer Structure that resides under the floor, via access passages provided in selected floor panels. The Load Transfer Structure transfers the weight of the item to members of the airframe, and is designed to accommodate loads during normal flight without restricting the designed movement of the airframe; however, under abnormal conditions such as a crash, the Load Transfer Structure engages members of the airframe to transfer loads thereto to secure the item.
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公开(公告)号：US11667370B2
公开(公告)日：2023-06-06
申请号：US16837422
申请日：2020-04-01
CPC分类号： B64C1/20 , B29C45/0055 , B32B3/04 , B29C2045/0008 , B32B15/08 , B32B15/14 , B32B15/20 , B32B2311/18 , B32B2605/18
摘要： A rail for the fastening of equipment elements, such as, in particular, seats, in aircraft, includes a holding region for connection to an equipment element of an aircraft, and a support region to fasten the rail to a carrier element of the aircraft. The rail has a metallic shell which is, for example, made of titanium and which is filled with a fiber-reinforced thermoplastic filler material which is reinforced by short fibers. To produce the rail, a metallic molded part is used as a casting mold and is filled, for example by injection, with the filler material and, after the rail has been produced, forms the metallic shell for the filler material.
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公开(公告)号：US20180194451A1
公开(公告)日：2018-07-12
申请号：US15405246
申请日：2017-01-12
CPC分类号： B64C1/20 , B64C1/12 , B64C1/22 , B64C2001/0072 , B64D11/0601 , B64D11/0696 , F16B2/12 , F16B5/01 , Y02T50/46
摘要： In one embodiment, an apparatus may comprise an attachment device configured to be embedded in a structure, wherein the attachment device comprises: a body comprising a first flange and a second flange, wherein the body is configured such that the first flange and the second flange are coupled together internally within the body when the attachment device is embedded in the structure; an attachment fitting for coupling a component to the structure in which the attachment device is embedded.
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