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1. 发明授权

US11254413B2 Spatially staggered jury strut system 有权
公开(公告)号：US11254413B2
公开(公告)日：2022-02-22
申请号：US16601245
申请日：2019-10-14
申请人： THE BOEING COMPANY
发明人： Robert Erik Grip , Max U. Kismarton
IPC分类号： B64C7/00 , B64C1/26
摘要： A strut system for a wing of an aircraft, includes a strut member extending from the wing and a first jury strut assembly associated with the wing. The first jury strut assembly includes a first jury strut, which has a first end connected to the strut member and a second jury strut, which has a first end connected to the strut member, wherein a second end of the first jury strut and a second end of the second jury strut are each connected to the wing spaced apart from one another in a direction of a chord.

2. 发明授权

US11091175B2 Vacuum transport tube vehicle, system, and method for evacuating a vacuum transport tube 有权
公开(公告)号：US11091175B2
公开(公告)日：2021-08-17
申请号：US16719919
申请日：2019-12-18
申请人： The Boeing Company
发明人： Robert Erik Grip , Mark A. DeHaan , John C. Vassberg , Ted K. Rothaupt
IPC分类号： B61B13/10 , B61B13/08 , B60L13/04 , F04B25/00 , B60L13/10
摘要： A vacuum transport tube vehicle for evacuating a vacuum transport tube has a first end, a second end, and a body comprising a piston head. The vehicle has a blade-actuator assembly, comprising a circumferential blade member sealed to the piston head and having a blade perimeter portion defining a first end outer surface forming an annular gap with an inner surface of the vacuum transport tube. The vehicle further includes a plurality of blade segment actuators arranged circumferentially around the piston perimeter portion and configured to actively adjust a radial position of the blade member at the corresponding blade circumferential locations in a manner accommodating non-uniformities in an inner surface profile of the vacuum transport tube, and maintaining the annular gap at a substantially constant and relatively short gap distance during movement of the vehicle through the vacuum transport tube.

3. 发明授权

US11040825B2 Cargo container 有权
公开(公告)号：US11040825B2
公开(公告)日：2021-06-22
申请号：US16386829
申请日：2019-04-17
申请人： THE BOEING COMPANY
发明人： Robert Erik Grip
IPC分类号： B65D90/00 , B65D88/12
摘要： Certain aspects of the present disclosure provide a container, including: a floor; a plurality of vertical walls coupled to the floor; a ceiling coupled to the plurality of vertical walls; a first horizontal gate coupled to a first vertical wall of the plurality of vertical walls and comprising a first plurality of foldable portions; a second horizontal gate coupled to a second vertical wall of the plurality of vertical walls and comprising a second plurality of foldable portions; a third horizontal gate coupled to a third vertical wall of the plurality of vertical walls and comprising a third plurality of foldable portions; and a first vertical gate coupled to the ceiling and comprising a fourth plurality of foldable portions, wherein, when extended, the first horizontal gate, the second horizontal gate, the third horizontal gate, and the first vertical gate form a plurality of separate cargo volumes.

4. 发明授权

US10974807B2 Segmented aircraft wing having solar arrays 有权
公开(公告)号：US10974807B2
公开(公告)日：2021-04-13
申请号：US15957909
申请日：2018-04-20
申请人： The Boeing Company
发明人： Robert Erik Grip , Blaine Knight Rawdon
IPC分类号： B64C3/26 , B64C3/18 , B64C3/22 , B64D27/24
摘要： An aircraft wing has a plurality of wing segments mounted on a wing spar by joints that allow relative movement between the spar and the wing segments. Tuning of coefficients of thermal expansion is employed to reduce induced stresses from changes in temperature.

5. 发明申请

US20210016868A1 MODULAR FUSELAGE ASSEMBLIES FOR AIRCRAFT, AIRCRAFT INCLUDING MODULAR FUSELAGE ASSEMBLIES, AND METHODS OF ASSEMBLING MODULAR FUSELAGE ASSEMBLIES 有权
公开(公告)号：US20210016868A1
公开(公告)日：2021-01-21
申请号：US16517420
申请日：2019-07-19
申请人： The Boeing Company
发明人： Robert Erik Grip , Joseph Paul Giesing
IPC分类号： B64C1/06 , B64C1/12 , B64C1/22
摘要： Modular fuselage assemblies for aircraft, aircraft including modular fuselage assemblies, and methods of assembling modular fuselage assemblies. A modular fuselage assembly includes a plurality of fuselage lobes that may extend along a longitudinal axis of the modular fuselage assembly. Each fuselage lobe includes a plurality of frame members and a lobe skin that is operatively attached to the plurality of frame members and defines an external surface of the fuselage lobe. The modular fuselage assembly also includes a plurality of longerons extending along a longitudinal axis of the modular fuselage assembly. At least two fuselage lobes are operatively attached to each longeron and the plurality of fuselage lobes and the plurality of longerons at least partially bound a cargo hold defined within the modular fuselage assembly. The methods include methods of assembling the modular fuselage assemblies.

6. 发明申请

US20190185022A1 SUPPORT SYSTEMS AND METHODS FOR A TRANSPORTATION SYSTEM 审中-公开
公开(公告)号：US20190185022A1
公开(公告)日：2019-06-20
申请号：US16284165
申请日：2019-02-25
申请人： THE BOEING COMPANY
发明人： Robert Erik Grip
IPC分类号： B61B13/10
CPC分类号： B61B13/10
摘要： A transportation system includes a tube defining an interior channel. A vehicle is configured to travel through the interior channel. At least one tension support couples the tube to ground. The tension support(s) exerts tension force into the tube. The tension force exerted into the tube reduces deflection of the tube when the vehicle travels through the interior channel over the tension support(s).

7. 发明申请

US20180022435A1 SPACE FRAME FUSELAGE WITH PRESSURE MEMBRANE 审中-公开
公开(公告)号：US20180022435A1
公开(公告)日：2018-01-25
申请号：US15604409
申请日：2017-05-24
申请人： The Boeing Company
发明人： Robert Erik Grip , Kevin John Sequeira
IPC分类号： B64C1/08 , B64C1/10
CPC分类号： B64C1/08 , B64C1/10 , B64C1/12
摘要： Disclosed are structures and features of a space frame aircraft. In particular, this disclosure relates to a space frame aircraft with a pressure membrane.

8. 发明申请

US20170309068A1 Two-Dimensional Model of Triangular Sectors for Use in Generating a Mesh for Finite Element Analysis 有权
公开(公告)号：US20170309068A1
公开(公告)日：2017-10-26
申请号：US15641172
申请日：2017-07-03
申请人： The Boeing Company
发明人： Robert Erik Grip
IPC分类号： G06T17/20 , G06F17/50
CPC分类号： G06T17/20 , G06F17/5018
摘要： A method and apparatus for analyzing a joint. The apparatus comprises a graph generator and a model generator. The graph generator forms a first graph based on a plurality of points within a region. The plurality of points represent a plurality of locations relative to a structure for a plurality of fastener devices configured to be installed in the structure to form a joint. The graph generator is configured to identify primary points and secondary points based on the first graph. The graph generator is further configured to form a second graph using the primary points, the secondary points, and the first graph. The model generator is configured to generate a two-dimensional model comprised of triangular sectors using vertices of the second graph. The two-dimensional model is configured for use in forming a mesh for use in performing finite element analysis for the joint.

9. 发明授权

US09132908B1 Expandable nose cone 有权
标题翻译：可扩展鼻锥
公开(公告)号：US09132908B1
公开(公告)日：2015-09-15
申请号：US13834296
申请日：2013-03-15
申请人： The Boeing Company
发明人： Robert Erik Grip , John Joseph Brown
IPC分类号： B64C1/30 , B64C23/00 , B64G1/00 , B64C30/00 , B64C37/02 , F42B10/46
CPC分类号： B64C1/30 , B64C23/005 , B64C30/00 , B64C37/02 , B64D5/00 , B64G1/005 , F42B10/46
摘要： A method and apparatus for operating a nose cone. In one illustrative example, an apparatus comprises a plurality of segments and a movement system associated with the plurality of segments. The plurality of segments forms the nose cone. Each of the plurality of segments comprises a segment outer surface that forms a portion of an outer surface of the nose cone. The movement system is used to move at least one of the plurality of segments to move the nose cone between a retracted state and an expanded state.
摘要翻译：一种用于操作鼻锥的方法和装置。在一个说明性示例中，装置包括多个段和与多个段相关联的移动系统。多个段形成鼻锥。多个节段中的每一个包括形成鼻锥的外表面的一部分的节段外表面。移动系统用于移动多个区段中的至少一个以在缩回状态和展开状态之间移动鼻锥。

10. 发明授权

US11312398B2 Active control deflection neutralizer 有权
公开(公告)号：US11312398B2
公开(公告)日：2022-04-26
申请号：US16262642
申请日：2019-01-30
申请人： The Boeing Company
发明人： Robert Erik Grip , Steven Fulton Griffin
IPC分类号： B61B13/08 , E01B35/12 , B61B5/00
摘要： Neutralizing deflection in a transportation system comprising connecting a number of support structures to ground. A tube is coupled to the support structures via a number of actuators, wherein the tube defines an interior enclosure through which a vehicle can travel. Utilizing a number of sensors, directional displacement of the support structures can be sensed, and the actuators are controller to counter the sensed displacement of the support structures by producing a directionally-opposite displacement of the tube relative to the support structures.

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