公开(公告)号：US20130228652A1

公开(公告)日：2013-09-05

申请号：US13776912

申请日：2013-02-26

申请人： EUROCOPTER

发明人： Jean-Francois Joffre

IPC分类号： B64D11/06

CPC分类号： B64D11/0696 ,  B64D11/0619 ,  B64D11/0639 ,  B64D11/0689 ,  B64D11/0697 ,  B64D25/04 ,  Y02T50/46

摘要： A crashworthy bench (1) for an aircraft having a cabin that includes a floor (51), a ceiling (52), and substantially vertical partitions. Said bench (1) comprises a frame (2), at least one seat for a passenger, with each seat comprising a seat, a back, a retaining system (7) for retaining said passenger, and at least one energy absorber device (20). Said frame (2) is fastened to the inside of said cabin via one low connection point (8) for each seat and via at least one high connection point (9) for said bench (1). Two low connecting rods (11) and one leg (12) connect the frame (2) to each low connection point (8) on said floor (51). Two high connecting rods (15) connect the frame (2) to the high connection points (9) on said ceiling (52) or on a vertical partition of the cabin of the aircraft.

摘要翻译： 一种用于具有包括地板（51），天花板（52）和基本垂直隔板的舱室的飞机的耐撞台（1）。 所述台架（1）包括框架（2），至少一个用于乘客的座椅，每个座椅包括座椅，靠背，用于保持所述乘客的保持系统（7）和至少一个能量吸收器装置 ）。 所述框架（2）经由用于每个座椅的一个低连接点（8）并且经由用于所述工作台（1）的至少一个高连接点（9）而紧固到所述机舱的内部。 两个低连接杆（11）和一个支腿（12）将框架（2）连接到所述地板（51）上的每个低连接点（8）。 两个高连杆（15）将框架（2）连接到所述天花板（52）上的高连接点（9）或飞机机舱的垂直隔板上。

公开(公告)号：US20100102602A1

公开(公告)日：2010-04-29

申请号：US12523523

申请日：2008-01-09

申请人： Holger Hansen

发明人： Holger Hansen

IPC分类号： B60R22/00 ,  B64D11/06 ,  A62B35/00 ,  B60R21/00 ,  B60N2/42 ,  A47C15/00

CPC分类号： B60N2/307 ,  B60N2/24 ,  B60N2/3002 ,  B60N2/3065 ,  B60N2/4242 ,  B60N2/54 ,  B60N2/7011 ,  B60R22/26 ,  B60R2022/027 ,  B64D11/06 ,  B64D11/0619 ,  B64D11/062 ,  B64D11/0697 ,  B64D11/0698 ,  F41H7/046

摘要： A safety seat for vehicles, including a seat portion having a rear end supported against vertical support straps of a strap framework secured to a vehicle. Each of two supports laterally disposed on the seat portion as a first end secured to the set. From the first end, each support extends in an inclined path, below the seat portion, to the vertical support straps. Each support has a free end remote from the first end and suspended in a loop formed on the vertical support straps. To tensioning straps are disposed beneath the seat portion and extend along side edges thereof from a front securement and the seat portion to a connection with the vertical support straps. Each tensioning strap has a length less than the distance between the front securement and the rear end of the seat portion.

摘要翻译： 一种用于车辆的安全座椅，包括座椅部分，该座椅部分的后端支撑在固定在车辆上的绑带框架的垂直支撑带上。 两个支撑件中的每一个作为固定到该组件上的第一端侧向设置在座椅部分上。 从第一端部，每个支撑件在座椅部分下方的倾斜路径中延伸到垂直支撑带。 每个支撑件具有远离第一端的自由端并且悬挂在形成在垂直支撑带上的环中。 张紧带被布置在座部下方并且沿其侧边缘从前固定件和座部分延伸到与垂直支撑带的连接。 每个张紧带的长度小于前部固定件和座椅部分的后端之间的距离。

公开(公告)号：US20120325586A1

公开(公告)日：2012-12-27

申请号：US13166217

申请日：2011-06-22

申请人： Daniel Meggs ,  Don Blackman ,  Brian Ford ,  Justin Robinson

发明人： Daniel Meggs ,  Don Blackman ,  Brian Ford ,  Justin Robinson

IPC分类号： B60R22/48 ,  B60R22/343

CPC分类号： A62B35/0062 ,  A61G7/1042 ,  A62B35/0075 ,  B64D11/00155 ,  B64D11/0611 ,  B64D11/062 ,  B64D11/0624 ,  B64D11/0697 ,  B64D25/06

摘要： Disclosed is a restraint system for a vehicle, such as a wheeled vehicle, boat, or fixed or rotary winged aircraft. The system includes a control system integrated into the harness and strap of the restraint. This permits crewmembers to lock and unlock the restraint from a body worn control panel. Other auxiliary equipment also be operated from the control panel. In another embodiment, wiring for a communication system is integrated into the harness and strap.

摘要翻译： 公开了一种用于车辆的限制系统，例如轮式车辆，船，或固定或旋翼飞机。 该系统包括集成到束带和束带的控制系统。 这允许机组人员从身体磨损的控制面板上锁定和解锁约束。 其他辅助设备也可从控制面板进行操作。 在另一个实施例中，用于通信系统的布线被集成到线束和带中。

公开(公告)号：US2812146A

公开(公告)日：1957-11-05

申请号：US41532454

申请日：1954-03-10

申请人： FAIREY AVIAT CO LTD

发明人： EUGENE CHAPLIN HERBERT

IPC分类号： B64D11/06

CPC分类号： B64D11/0639 ,  B64D11/06 ,  B64D11/0649 ,  B64D11/0697

公开(公告)号：US20170320581A1

公开(公告)日：2017-11-09

申请号：US15144867

申请日：2016-05-03

申请人： The Boeing Company

发明人： Darren Carl McIntosh

IPC分类号： B64D11/06 ,  B64D11/02

CPC分类号： B64D11/0697 ,  B64D11/0691

摘要： A vehicle includes an interior cabin including a floor and a ceiling. A deployable seat assembly is moveably coupled to the ceiling. The deployable seat assembly is moveable between a stowed position in which at least a portion of the deployable seat assembly is stowed within a stowage space within the ceiling, and a deployed position in which the deployable seat assembly extends between the ceiling and the floor.

公开(公告)号：US20090295208A1

公开(公告)日：2009-12-03

申请号：US12473844

申请日：2009-05-28

申请人： Zohar ELHANATI ,  Yoash KACHTAN

发明人： Zohar ELHANATI ,  Yoash KACHTAN

IPC分类号： A63G9/14

CPC分类号： B60N2/24 ,  B60N2/0232 ,  B60N2/3011 ,  B60N2/3015 ,  B60N2/3031 ,  B60N2/3047 ,  B60N2/3065 ,  B60N2/4242 ,  B60N2/50 ,  B60N2002/905 ,  B64D11/0619 ,  B64D11/062 ,  B64D11/0696 ,  B64D11/0697 ,  F41H7/046 ,  Y02T50/46

摘要： A vehicle comprising lower and upper surfaces, an object and a suspension apparatus for holding the object in a suspended position in the vehicle. The object having opposite rear and front edges, and adjacent first and second halves extending between the rear and front edges. The suspension apparatus being adapted to anchor the object to the lower surface of the vehicle via elongated suspension elements, and comprising first and second elongated suspension elements. Each elongated suspension element comprising first and second ends and an intermediate portion therebetween. The first elongated suspension element is connected via the first end thereof to a first point on the object's first half, and is connected via the second end thereof to a first point on the vehicle's lower surface disposed closer to the objects second half than to the first half thereof. The second elongated suspension element is connected via the first end thereof to a second point on the object's second half, and is connected via the second end thereof to a second point on the vehicle's lower surface disposed closer to the object's first half than to the second half thereof.

摘要翻译： 包括下表面和上表面的车辆，物体和用于将物体保持在车辆中的悬挂位置的悬挂装置。 物体具有相对的后边缘和前边缘，以及在后边缘和前边缘之间延伸的相邻的第一和第二半部。 悬挂装置适于经由细长的悬挂元件将物体锚固到车辆的下表面，并且包括第一和第二细长悬挂元件。 每个细长的悬挂元件包括第一和第二端以及它们之间的中间部分。 第一细长悬挂元件经由其第一端连接到物体的前半部分上的第一点，并且经由其第二端连接到车辆下表面上的第一点，该第一点设置成比第二点靠近物体的第二点 一半。 第二细长悬挂元件经由其第一端连接到物体的第二半部的第二点，并且经由其第二端连接到车辆下表面上的第二点，该第二点设置为更接近物体的前半部，而不是第二点 一半。

公开(公告)号：US08801099B2

公开(公告)日：2014-08-12

申请号：US13395079

申请日：2010-09-03

申请人： Wolfram Ebel ,  Andrè Haberecht

发明人： Wolfram Ebel ,  Andrè Haberecht

IPC分类号： A47C3/00 ,  B63B29/06 ,  B60N2/24 ,  B63B29/04 ,  B60N2/42 ,  B64D11/06

CPC分类号： B60N2/24 ,  B60N2/4242 ,  B63B29/04 ,  B63B29/06 ,  B64D11/06 ,  B64D11/0619 ,  B64D11/062 ,  B64D11/0639 ,  B64D11/0696 ,  B64D11/0697

摘要： Safety seat for land vehicles, aircraft and watercraft, including a strap framework for holding a sitting portion and comprising vertically extending support straps anchored to a vehicle and embodied as loops stretching between vehicle-mounted anchors above and below the sitting portion, which is secured to a support frame provided with two braces oriented in the direction of extension of the support straps. For securement of the support frame to the strap framework, a front strap or rear strap of each support strap loop is divided into two strap sections, one extending between the support frame and an anchor disposed above the sitting portion, and the other extending between the support frame and an anchor disposed below the sitting portion. Ends of the strap sections associated with the support frame are retained at the braces of the support frame and hold the support frame under tension in a vertical orientation.

摘要翻译： 用于陆上车辆，飞机和船舶的安全座椅，包括用于保持座位部分的带框架，并且包括锚定到车辆的垂直延伸的支撑带，并且被实施为在坐着部分上方和下方的车载锚定件之间延伸的环， 支撑框架设置有沿着支撑带的延伸方向定向的两个支架。 为了将支撑框架固定到带框架，每个支撑带环的前带或后带被分成两个带部分，一个在支撑框架和设置在坐着部分上方的锚之间延伸，另一个延伸在 支撑框架和设置在坐着部分下方的锚固件。 与支撑框架相关联的带部分的端部保持在支撑框架的支架处，并且在竖直方向上将支撑框架保持在张力下。

公开(公告)号：US20120200136A1

公开(公告)日：2012-08-09

申请号：US13395079

申请日：2010-09-03

申请人： Wolfram Ebel ,  André Haberecht

发明人： Wolfram Ebel ,  André Haberecht

IPC分类号： B60N2/015 ,  B63B29/04 ,  B64D11/06

CPC分类号： B60N2/24 ,  B60N2/4242 ,  B63B29/04 ,  B63B29/06 ,  B64D11/06 ,  B64D11/0619 ,  B64D11/062 ,  B64D11/0639 ,  B64D11/0696 ,  B64D11/0697

摘要： Safety seat for land vehicles, aircraft and watercraft, including a strap framework for holding a sitting portion and comprising vertically extending support straps anchored to a vehicle and embodied as loops stretching between vehicle-mounted anchors above and below the sitting portion, which is secured to a support frame provided with two braces oriented in the direction of extension of the support straps. For securement of the support frame to the strap framework, a front strap or rear strap of each support strap loop is divided into two strap sections, one extending between the support frame and an anchor disposed above the sitting portion, and the other extending between the support frame and an anchor disposed below the sitting portion. Ends of the strap sections associated with the support frame are retained at the braces of the support frame and hold the support frame under tension in a vertical orientation.

摘要翻译： 用于陆上车辆，飞机和船舶的安全座椅，包括用于保持座位部分的带框架，并且包括锚定到车辆的垂直延伸的支撑带，并且被实施为在坐着部分上方和下方的车载锚定件之间延伸的环， 支撑框架设置有沿着支撑带的延伸方向定向的两个支架。 为了将支撑框架固定到带框架，每个支撑带环的前带或后带被分成两个带部分，一个在支撑框架和设置在坐着部分上方的锚之间延伸，另一个延伸在 支撑框架和设置在坐着部分下方的锚固件。 与支撑框架相关联的带部分的端部保持在支撑框架的支架处，并且在竖直方向上将支撑框架保持在张力下。

公开(公告)号：US20050183461A1

公开(公告)日：2005-08-25

申请号：US11063956

申请日：2005-02-22

申请人： Bodo Kuhn ,  Igor Radosevic ,  Bruno Uebbing

发明人： Bodo Kuhn ,  Igor Radosevic ,  Bruno Uebbing

IPC分类号： B60N2/24 ,  B60N2/30 ,  B63B29/06 ,  B64D11/06 ,  C03B37/018

CPC分类号： C21D1/30 ,  B60N2/24 ,  B60N2/30 ,  B63B29/06 ,  B64D11/0639 ,  B64D11/0696 ,  B64D11/0697 ,  C03C3/06 ,  C03C4/08

摘要： A method for producing an optical component for transmitting ultraviolet radiation of a wavelength of 250 nm and shorter, wherein the component is made from a cylindrical quartz glass blank having a mean OH content of more than 50 wt ppm, which is subjected to a first annealing treatment for eliminating stress birefringence, characterized in that the quartz glass blank is subjected to a second annealing treatment which comprises heating up and holding the quartz glass blank at a low annealing temperature ranging from 350° C. to 800° C. and for an annealing period of more than 1 hour, with the proviso that a quartz glass blank is used in which in a direction perpendicular to the cylindrical longitudinal axis the deviation from the mean OH content is not more than 20 wt ppm.

摘要翻译： 一种用于透射波长为250nm以下的紫外线辐射的光学部件的方法，其中所述部件由平均OH含量大于50重量ppm的圆柱形石英玻璃坯料制成，其经受第一次退火 用于消除应力双折射的处理，其特征在于对石英玻璃坯料进行第二退火处理，其包括在350℃至800℃的低退火温度下加热并保持石英玻璃坯料并进行退火 时间大于1小时，条件是使用石英玻璃坯料，其中在垂直于圆柱纵轴的方向上偏离平均OH含量不大于20重量ppm。

公开(公告)号：US09308999B2

公开(公告)日：2016-04-12

申请号：US13776912

申请日：2013-02-26

申请人： AIRBUS HELICOPTERS

发明人： Jean-Francois Joffre

IPC分类号： B64D11/06 ,  B64D25/04

CPC分类号： B64D11/0696 ,  B64D11/0619 ,  B64D11/0639 ,  B64D11/0689 ,  B64D11/0697 ,  B64D25/04 ,  Y02T50/46

摘要： A crashworthy bench (1) for an aircraft having a cabin that includes a floor (51), a ceiling (52), and substantially vertical partitions. Said bench (1) comprises a frame (2), at least one seat for a passenger, with each seat comprising a seat, a back, a retaining system (7) for retaining said passenger, and at least one energy absorber device (20). Said frame (2) is fastened to the inside of said cabin via one low connection point (8) for each seat and via at least one high connection point (9) for said bench (1). Two low connecting rods (11) and one leg (12) connect the frame (2) to each low connection point (8) on said floor (51). Two high connecting rods (15) connect the frame (2) to the high connection points (9) on said ceiling (52) or on a vertical partition of the cabin of the aircraft.

摘要翻译： 一种用于具有包括地板（51），天花板（52）和基本垂直隔板的舱室的飞机的耐撞台（1）。 所述台架（1）包括框架（2），至少一个用于乘客的座椅，每个座椅包括座椅，靠背，用于保持所述乘客的保持系统（7）和至少一个能量吸收器装置 ）。 所述框架（2）经由用于每个座椅的一个低连接点（8）并且经由用于所述工作台（1）的至少一个高连接点（9）而紧固到所述机舱的内部。 两个低连接杆（11）和一个支腿（12）将框架（2）连接到所述地板（51）上的每个低连接点（8）。 两个高连杆（15）将框架（2）连接到所述天花板（52）上的高连接点（9）或飞机机舱的垂直隔板上。