公开(公告)号：US20190061950A1

公开(公告)日：2019-02-28

申请号：US16117066

申请日：2018-08-30

Applicant: Driessen Aerospace Group N.V.

Inventor： Andreas Hoogeveen ,  Paul Cornelis Vlaming

IPC: B64D11/04

Abstract: Embodiments of the present disclosure relate generally to improved braking systems for slide extractors. Slide extractors are generally used in aircraft galleys in order to move containers forward. The disclosed slide extractor braking system provides cooperation between magnets and corresponding conductive material in order to manage and appropriately slow retraction of the slide extractor in use.

公开(公告)号：US20210122572A1

公开(公告)日：2021-04-29

申请号：US16626496

申请日：2019-07-17

Applicant: Driessen Aerospace Group N.V.

Inventor： Paul Cornelis Vlaming

IPC: B65G1/14 ,  B64D11/04

Abstract: A container extraction assembly that includes an extractor assembly and a retainer assembly. The extractor assembly includes a pull member and an extractor member. The extractor member is movable between a distal position and a proximal position and the pull member is movable between first, second third positions. Moving the pull member from the first position to the third position moves the extractor member from the distal to the proximal position. The retainer assembly includes a proximal leg member and a distal leg member that are hingedly connected to one another. The retainer assembly is movable between a deployed position, a folded position and a finish position. Moving the pull member from the first position to the second position moves the retainer assembly from the deployed to the folded position, and moving the pull member from the second position to the third position moves the retainer assembly from the folded to the finish position.

公开(公告)号：US20160221307A1

公开(公告)日：2016-08-04

申请号：US14993489

申请日：2016-01-12

Applicant: Driessen Aerospace Group N.V.

Inventor： Jochem Floris Wartena ,  Paul Cornelis Vlaming

IPC: B32B17/10 ,  B64D11/02 ,  B64D11/04

CPC classification number: B32B17/10 ,  B32B17/064 ,  B32B17/10137 ,  B32B2307/412 ,  B32B2439/00 ,  B32B2451/00 ,  B32B2457/208 ,  B32B2605/18 ,  B64D11/02 ,  B64D11/04

Abstract: Embodiments of the present invention provide a laminated glass surface for an aircraft or other passenger transportation vehicle surface. Specific features may include a glass substrate that is associated with an adhesive layer to form a laminated glass. The glass substrate may be an ultrathin glass substrate and/or a strengthened glass substrate. The laminated glass may then be secured to an aircraft surface.

Abstract translation: 本发明的实施例提供了一种用于飞行器或其他乘客运输车辆表面的夹层玻璃表面。 具体特征可以包括与粘合剂层相关联以形成夹层玻璃的玻璃基板。 玻璃基板可以是超薄玻璃基板和/或强化玻璃基板。 然后可以将夹层玻璃固定到飞行器表面。

公开(公告)号：US11167926B2

公开(公告)日：2021-11-09

申请号：US16626503

申请日：2019-07-17

Applicant: Driessen Aerospace Group N.V.

Inventor： Paul Cornelis Vlaming ,  Maxim Smulders

IPC: B65G1/14 ,  B64D11/04 ,  A47F1/12

Abstract: A retainment assembly that includes a proximal retainer member that is movable between a first retracted position, a second retracted position and a deployed position, a distal retainer member that is movable between a retracted position and a deployed position. When the proximal retainer member moves from the deployed position to the first retracted position the distal retainer member does not move, and when the proximal retainer member moves from the deployed position to the second retracted position the distal retainer member moves from the deployed position to the retracted position.

公开(公告)号：US20210122471A1

公开(公告)日：2021-04-29

申请号：US16626503

申请日：2019-07-17

Applicant: DRIESSEN AEROSPACE GROUP N.V.

Inventor： Paul Cornelis Vlaming ,  Maxim Smulders

IPC: B64D11/04 ,  A47F1/12

Abstract: A retainment assembly that includes a proximal retainer member that is movable between a first retracted position, a second retracted position and a deployed position, a distal retainer member that is movable between a retracted position and a deployed position. When the proximal retainer member moves from the deployed position to the first retracted position the distal retainer member does not move, and when the proximal retainer member moves from the deployed position to the second retracted position the distal retainer member moves from the deployed position to the retracted position.

公开(公告)号：US10974901B1

公开(公告)日：2021-04-13

申请号：US16626496

申请日：2019-07-17

Applicant: Driessen Aerospace Group N.V.

Inventor： Paul Cornelis Vlaming

IPC: B65G1/14 ,  B64D11/04 ,  B25J1/04

Abstract: A container extraction assembly that includes an extractor assembly and a retainer assembly. The extractor assembly includes a pull member and an extractor member. The extractor member is movable between a distal position and a proximal position and the pull member is movable between first, second third positions. Moving the pull member from the first position to the third position moves the extractor member from the distal to the proximal position. The retainer assembly includes a proximal leg member and a distal leg member that are hingedly connected to one another. The retainer assembly is movable between a deployed position, a folded position and a finish position. Moving the pull member from the first position to the second position moves the retainer assembly from the deployed to the folded position, and moving the pull member from the second position to the third position moves the retainer assembly from the folded to the finish position.