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21.发明授权公开(公告)号：US10479281B2
公开(公告)日：2019-11-19
申请号：US15672742
申请日：2017-08-09
Applicant: Airbus Operations GmbH
Inventor： Hermann Benthien , Marcus Hinrichs , Michael Telkamp
Abstract: An equipment mounting device and an installation arrangement for mounting an equipment to two fittings. The mounting device comprises a longitudinal carrier configured to be coupled to the equipment, and sized to span a space between the two fittings. A first coupling is disposed at a first end of the longitudinal carrier. The first coupling is configured to be coupled with a first of the two fittings and, when coupled with the first fitting, to prevent movement of the carrier in a first direction different from a direction along a longitudinal axis of the longitudinal carrier. A second coupling is configured to detachably couple with a second of the two fittings by receiving a part of the second fitting and, when coupled with the second fitting, to prevent movement of the carrier at least in the first direction and the direction of the longitudinal axis of the carrier.
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公开(公告)号：US20190118926A1
公开(公告)日：2019-04-25
申请号：US16156582
申请日：2018-10-10
Applicant: Airbus Operations GmbH
Inventor： Memis Tiryaki , Hermann Benthien , Wolfgang Eilken
Abstract: A fuselage structure for an aircraft, comprising a fuselage vessel and a pressure bulkhead arranged in an end region of the fuselage vessel and having a central region extending in a planar manner and a connection region adjoining the central region in a radial direction and surrounding the central region and being secured to the fuselage vessel. The pressure bulkhead divides the fuselage vessel with respect to the longitudinal direction into a first region for subjecting to an internal pressure and a second region for subjecting to an external pressure which is lower than the internal pressure. The central region of the pressure bulkhead has an arching in the direction of the first region of the fuselage vessel.
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公开(公告)号：US20190061937A1
公开(公告)日：2019-02-28
申请号：US16114517
申请日：2018-08-28
Applicant: Airbus Operations GmbH
Inventor： Bastian Schäfer , Hermann Benthien , David Kaden , Danny Dicks
Abstract: A coupling device for coupling modules with each other, comprising: a coupling surface, a primary coupling member and at least two secondary coupling members. The primary coupling member is disposed on the coupling surface. A coupling axis disposed parallel to a direction of action of earth's gravitational acceleration extends through the primary coupling member. The at least two secondary coupling members are configured to be complementary to each other and are disposed on the coupling face, and respectively have a predetermined distance from the coupling axis.
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24.发明申请公开(公告)号：US20190048908A1
公开(公告)日：2019-02-14
申请号：US16100910
申请日：2018-08-10
Applicant: Airbus Operations GmbH
Inventor： Hermann Benthien , Danny Dicks , David Kaden , Bastian Schäfer
IPC: F16B5/00
Abstract: A coupling member for coupling modules with each other. The coupling member comprises a coupling portion, which in turn has a coupling rim and at least two hook members disposed on the coupling rim. The coupling portion substantially corresponds in its outer contour to a spherical segment of a sphere with a predetermined spherical radius, wherein the coupling rim represents a circular disk of the spherical segment. In this case, an outer radius of the coupling rim is smaller than or equal to the spherical radius. The at least two hook members, in a lateral view, at least partially follow the outer contour of the spherical cap of the spherical segment. The at least two hook members are engageable with the hook members of a coupling portion of a second coupling member.
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公开(公告)号：US20180065725A1
公开(公告)日：2018-03-08
申请号：US15689539
申请日：2017-08-29
Applicant: Airbus Operations GmbH
Inventor： Hermann Benthien , Matthias Hegenbart
CPC classification number: B64C1/061 , B29C70/56 , B64C2001/0072 , B64G1/10 , B64G1/22
Abstract: A structural member for an aircraft or spacecraft has at least one fiber plastic composite, the fiber plastic composite having at least one or a plurality of plies. The structural member also has at least one pre-stressing means providing internal stresses to the fiber plastic composite. The fiber plastic composite and the pre-stressing means are configured and arranged to form a balanced system the internal stresses of which are essentially balanced to zero in a cured state of the said system. The balanced system of the structural member is able to counteract loading stresses exerted to the airframe in service such, that a damage caused by the loading stress is easily detectable visually.
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Patent Agency Ranking
公开(公告)号：US20170173882A1
公开(公告)日：2017-06-22
申请号：US15375688
申请日：2016-12-12
Applicant: Airbus Operations GmbH
Inventor： Hermann Benthien , Andreas Poppe
CPC classification number: B33Y30/00 , B29C64/153 , B29C64/20 , B33Y10/00
Abstract: A device for building a three-dimensional structure in layers includes at least one supply unit, at least one laser unit and one table, wherein the table comprises a circular surface and is adapted for rotating the circular surface around a central axis. The supply unit is adapted for applying a powdery material in layers on the circular surface of the table. The laser unit at the same time can partly or completely melt powdery material already applied by the supply unit while the circular surface is rotating.
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公开(公告)号：US20170080536A1
公开(公告)日：2017-03-23
申请号：US15269317
申请日：2016-09-19
Applicant: Airbus Operations GmbH
Inventor： Hermann Benthien , Andreas Poppe
CPC classification number: B23P19/04 , B64C1/06 , B64C1/403 , F16B39/101 , F16B39/12 , F16C7/06 , F16C11/04 , F16D1/101 , F16D3/54 , F16D2001/102
Abstract: A connection system includes two connecting elements each having a respective connecting flange on which a plurality of coupling elements are arranged along a peripheral direction and which has a substantially round external profile; and a coupling belt, on which a plurality of opposing coupling elements are arranged which are configured to form a positive-locking connection with the coupling elements of the two connecting elements for the mutual rotation-proof fixing of the two connecting elements.
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28.发明申请公开(公告)号：US20160347464A1
公开(公告)日：2016-12-01
申请号：US14564216
申请日：2014-12-09
Applicant: Airbus Operations GmbH
Inventor： Oliver Seack , Matthias Hegenbart , Hermann Benthien , Markus Piesker , Jens Rohde , Sebastian Palm , Joern Clausen , Matthias Radny , Ulrich Knapp
CPC classification number: B64D27/26 , B22F3/1055 , B33Y80/00 , B60R13/0869 , B64C1/403 , B64D41/00 , B64D2027/262 , B64D2041/002 , C22C1/0408 , C22C1/045 , F28D2021/0021 , F28F1/40 , F28F1/422 , F28F13/14 , F28F13/185 , Y02P10/295 , Y02T50/44 , Y02T50/46
Abstract: A load bearing element for attachment of a heat generating unit to a heat sensitive supporting structure, wherein said load bearing element includes at least one body integrally formed by additive layer manufacturing, ALM. The body is adapted to provide a controlled heat transfer from said heat generating unit to said heat sensitive supporting structure.
Abstract translation: 一种用于将发热单元附接到热敏支撑结构的承载元件，其中所述承载元件包括由添加剂层制造（ALM）一体形成的至少一个主体。 本体适于提供从所述发热单元到所述热敏支撑结构的受控热传递。
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公开(公告)号：US20160025242A1
公开(公告)日：2016-01-28
申请号：US14804791
申请日：2015-07-21
Applicant: Airbus Operations GmbH
Inventor： Hermann Benthien , Andreas Poppe
CPC classification number: F16L3/1222 , F16B5/0628 , F16L3/1211 , F16L3/1236 , F16L3/13 , F16L3/137 , H02G3/32
Abstract: A fixing device for fixing an element, in particular a line, a cable, a pipe, a hose or the like in an aircraft or spacecraft, to a component, includes an LFS fixing structure, the latching body and/or the flange portion of the LFS fixing structure having a tolerance compensator for compensating thickness tolerances of the entire arrangement.
Abstract translation: 用于将飞机或航天器中的元件特别是线，电缆，管，软管等固定到部件的固定装置包括LFS固定结构，闩锁体和/或凸缘部分 LFS固定结构具有用于补偿整个布置的厚度公差的公差补偿器。
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公开(公告)号：US20140059813A1
公开(公告)日：2014-03-06
申请号：US14076423
申请日：2013-11-11
Applicant: Airbus Operations GmbH
Inventor： Axel Soeffker , Hermann Benthien
IPC: A44B18/00
CPC classification number: A44B18/0073 , B29C65/562 , B29C65/564 , B29C66/112 , B29C66/1122 , B29C66/131 , B29C66/1312 , B29C66/431 , B29C66/43441 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/72143 , B29C66/73941 , B29C70/543 , B29C70/68 , B29C70/882 , B29L2031/3076 , F16B5/07 , Y02T50/43 , Y10T24/2717 , Y10T29/49947 , Y10T29/49948 , Y10T29/4995 , Y10T29/49966 , Y10T29/49968 , B29K2307/04 , B29K2309/08 , B29K2063/00
Abstract: A connecting device for manufacturing a peeling-stress-resistant connection between two components. The connecting device includes a carrier, which has a first surface and a second surface opposing the first surface. The connecting device further includes a plurality of hook and loop elements which extend both from the first and the second surface of the carrier and each have at their free ends facing away from the first or the second surface of the carrier a hook and loop head, which is arranged to enter into a hook and loop connection with a component comprising a fiber-reinforced composite material.
Abstract translation: 一种用于在两个部件之间制造耐剥离 - 抗压连接的连接装置。 连接装置包括载体，其具有与第一表面相对的第一表面和第二表面。 连接装置还包括多个钩环元件，其从载体的第一表面和第二表面两者延伸，并且每个钩和环元件在其自由端处背离载体的第一或第二表面的钩和环头部， 其布置成与包括纤维增强复合材料的部件进行钩环连接。
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