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公开(公告)号:US11148788B2
公开(公告)日:2021-10-19
申请号:US15430661
申请日:2017-02-13
Applicant: Textron Aviation Inc.
Inventor: David James Swanson
IPC: B64C23/06
Abstract: Embodiments of the present disclosure include a curved planar wingtip for a straight wing and a curved planar wingtip for a swept wing of an aircraft. The curved planar wingtips include a member that extends from the end of the wing in a direction aft of the wing trailing edge while remaining substantially planar with the wing. The curved planar wingtips curve continuously from leading and trailing edges of the wing to form a tip located aft of the wing. Other embodiments of the curved planar wingtip are configured for a horizontal or vertical tail. Yet another embodiment includes a curved wingtip that extends aft of a trailing edge of the wing by a distance greater than the curved wingtip extends above a top surface of the wing.
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公开(公告)号:US20170233065A1
公开(公告)日:2017-08-17
申请号:US15430661
申请日:2017-02-13
Applicant: Textron Aviation Inc.
Inventor: David James Swanson
CPC classification number: B64C23/069 , Y02T50/164
Abstract: Embodiments of the present disclosure include a curved planar wingtip for a straight wing and a curved planar wingtip for a swept wing of an aircraft. The curved planar wingtips include a member that extends from the end of the wing in a direction aft of the wing trailing edge while remaining substantially planar with the wing. The curved planar wingtips curve continuously from leading and trailing edges of the wing to form a tip located aft of the wing. Other embodiments of the curved planar wingtip are configured for a horizontal or vertical tail. Yet another embodiment includes a curved wingtip that extends aft of a trailing edge of the wing by a distance greater than the curved wingtip extends above a top surface of the wing.
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公开(公告)号:US11021254B2
公开(公告)日:2021-06-01
申请号:US15824309
申请日:2017-11-28
Applicant: Textron Aviation Inc.
Inventor: David James Swanson , Michael Allen Bullard , Phillip Anthony Kendrick
IPC: B64D11/04
Abstract: A multi-rail galley includes a countertop on top of a first storage portion, and a second storage portion above the countertop. The countertop includes a first plurality of rails on a top surface that are configured for receiving at least one countertop insert. The second storage portion has a second plurality of rails beneath a bottom surface of the second storage portion and configured for receiving at least one hanging insert. A method of providing a customizable aircraft galley includes providing a countertop above a storage compartment, the countertop having a horizontal surface facing upwards with a plurality of rails disposed on top of the horizontal surface, installing a galley insert onto one of the plurality of rails via a matching slot in the galley insert, and removing the galley insert from one of the plurality of rails, enabling stowage of the galley insert.
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公开(公告)号:US20180162532A1
公开(公告)日:2018-06-14
申请号:US15824309
申请日:2017-11-28
Applicant: Textron Aviation Inc.
Inventor: David James Swanson , Michael Allen Bullard , Phillip Anthony Kendrick
IPC: B64D11/04
CPC classification number: B64D11/04
Abstract: A multi-rail galley includes a countertop on top of a first storage portion, and a second storage portion above the countertop. The countertop includes a first plurality of rails on a top surface that are configured for receiving at least one countertop insert. The second storage portion has a second plurality of rails beneath a bottom surface of the second storage portion and configured for receiving at least one hanging insert. A method of providing a customizable aircraft galley includes providing a countertop above a storage compartment, the countertop having a horizontal surface facing upwards with a plurality of rails disposed on top of the horizontal surface, installing a galley insert onto one of the plurality of rails via a matching slot in the galley insert, and removing the galley insert from one of the plurality of rails, enabling stowage of the galley insert.
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