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公开(公告)号:US20190241271A1
公开(公告)日:2019-08-08
申请号:US15890249
申请日:2018-02-06
Applicant: Bell Helicopter Textron Inc.
Inventor: Chad Richard Haugeberg , Timothy Carr , Michael Stephen Deslatte
Abstract: An embodiment rotorcraft structure includes a step disposed at an exterior of the rotorcraft, and an emergency kit installed into the recess of the step. The step is faired into a skin on the exterior of the rotorcraft. The emergency kit includes a container and a life raft. The container includes a container body that has a storage cavity, a container panel, and a first attachment element. The container body is disposed in the recess of the step, attached to the step, and has a storage cavity. The container panel is disposed at a bottom of the storage cavity, and the life raft is disposed in the storage cavity. The first attachment element releasably couples a first edge of the container panel to the container body, and encloses the life raft in the container under the step.
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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
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.
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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
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.
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