公开(公告)号：US20180194473A1

公开(公告)日：2018-07-12

申请号：US15405284

申请日：2017-01-12

Applicant: Bell Helicopter Textron Inc.

Inventor： Joshua Emrich ,  Ross D. Cosby ,  Carl A. May ,  Richard Theodore Perryman

IPC: B64D11/06 ,  B64D25/04 ,  B64C1/18 ,  B64C27/00

CPC classification number: B64D11/064 ,  B64C1/18 ,  B64C27/00 ,  B64C27/04 ,  B64D11/0601 ,  B64D11/0639 ,  B64D11/0696 ,  B64D25/04 ,  Y02T50/46

Abstract: In one embodiment, an apparatus may comprise: a floor panel for a rotorcraft; and a plurality of passenger seats coupled to the floor panel, wherein: the plurality of passenger seats is arranged into a plurality of seating rows; and the plurality of passenger seats comprises one or more foldover seats arranged to facilitate access to one or more exits of the rotorcraft.

公开(公告)号：US20200301463A1

公开(公告)日：2020-09-24

申请号：US16361345

申请日：2019-03-22

Applicant: Bell Helicopter Textron Inc.

Inventor： Joshua Rogers ,  Joshua Emrich

IPC: G05G9/047 ,  B64C13/04

Abstract: Embodiments are directed to a flight control stick support comprising a spherical bearing coupled to a flight control stick, a first plate having a first hole configured to receive a top portion of the spherical bearing, a second plate having a second hole configured to receive a bottom portion of the spherical bearing, and a clamping device configured to move the first plate relative to and the second plate to apply a variable force against the spherical bearing.

公开(公告)号：US10196151B2

公开(公告)日：2019-02-05

申请号：US15144179

申请日：2016-05-02

Applicant: Bell Helicopter Textron Inc.

Inventor： Martin Peryea ,  Michael Reaugh Smith ,  Douglas Hamelwright, Jr. ,  Albert G. Brand ,  Nicholas J. Plagianos ,  Joshua Emrich ,  Timothy Carr

IPC: B64D37/06 ,  B64D37/32 ,  B64C27/00 ,  B64D37/04 ,  B64C27/04

Abstract: A rotorcraft includes a fuselage having a fuel tank receiving assembly with a fuel tank positioned therein. The fuel tank including a plurality of interconnected fuel bags operable to contain liquid fuel. A network of straps is disposed about the fuel tank forming a restraint assembly. The network of straps includes at least one perimeter strap extending at least partially about at least two fuel bags and at least one surrounding strap extending at least partially about the at least two fuel bags. The at least one perimeter strap has at least two intersections with the at least one surrounding strap.

公开(公告)号：US20170313434A1

公开(公告)日：2017-11-02

申请号：US15144179

申请日：2016-05-02

Applicant: Bell Helicopter Textron Inc.

Inventor： Martin Peryea ,  Michael Reaugh Smith ,  Douglas Hamelwright, JR. ,  Albert G. Brand ,  Nicholas J. Plagianos ,  Joshua Emrich ,  Timothy Carr

IPC: B64D37/06 ,  B64D37/32 ,  B64C27/00

CPC classification number: B64D37/06 ,  B64C27/00 ,  B64C27/04 ,  B64D37/04 ,  B64D37/32

Abstract: A rotorcraft includes a fuselage having a fuel tank receiving assembly with a fuel tank positioned therein. The fuel tank including a plurality of interconnected fuel bags operable to contain liquid fuel. A network of straps is disposed about the fuel tank forming a restraint assembly. The network of straps includes at least one perimeter strap extending at least partially about at least two fuel bags and at least one surrounding strap extending at least partially about the at least two fuel bags. The at least one perimeter strap has at least two intersections with the at least one surrounding strap.