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公开(公告)号：US20100200689A1
公开(公告)日：2010-08-12
申请号：US12368559
申请日：2009-02-10
申请人： Robert Erik Grip
发明人： Robert Erik Grip
IPC分类号： B60F5/00
摘要： An aircraft comprising a fuselage, a vessel associated with the fuselage, a propulsion system associated with the fuselage, and a lift system. The vessel is capable of storing a pressurized gas compressed to a density that allows the aircraft to operate under water. The lift system is capable of providing the aircraft lift to fly in air.
摘要翻译： 一种飞机，包括机身，与机身相关的船只，与机身相关联的推进系统，以及升降机系统。 该容器能够储存被压缩到允许飞机在水下操作的密度的加压气体。 电梯系统能够提供飞机升降机在空中飞行。
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公开(公告)号：US08418968B2
公开(公告)日：2013-04-16
申请号：US13295988
申请日：2011-11-14
申请人： Robert Erik Grip
发明人： Robert Erik Grip
IPC分类号： B64C3/44
摘要： An apparatus comprises a structure having a first side, a second side substantially opposite to the first side, a flexible skin, and a plurality of deformable assemblies. The flexible skin is attached to the first side and the second side of the structure. The plurality of deformable assemblies is moveably connected to the structure, in which each deformable assembly in the plurality of deformable assemblies has a vertex and a base. The each deformable assembly in the plurality of deformable assemblies has a height that is capable of changing to change a shape of the structure and a shape of the flexible skin.
摘要翻译： 一种装置包括具有第一侧，与第一侧基本相反的第二侧，柔性表皮和多个可变形组件的结构。 柔性皮肤附接到结构的第一侧和第二侧。 多个可变形组件可移动地连接到结构，其中多个可变形组件中的每个可变形组件具有顶点和底座。 多个可变形组件中的每个可变形组件具有能够改变以改变结构的形状和柔性皮肤的形状的高度。
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公开(公告)号：US20120056038A1
公开(公告)日：2012-03-08
申请号：US13295988
申请日：2011-11-14
申请人： Robert Erik Grip
发明人： Robert Erik Grip
IPC分类号： B64C3/50 , B64C5/06 , B64C5/02 , B64C9/00 , B64C9/32 , B62D37/02 , B63G8/14 , B61D17/00 , B63B1/00 , F41H7/00 , B62D47/00 , B64C3/44 , F02K1/54
摘要： An apparatus comprises a structure having a first side, a second side substantially opposite to the first side, a flexible skin, and a plurality of deformable assemblies. The flexible skin is attached to the first side and the second side of the structure. The plurality of deformable assemblies is moveably connected to the structure, in which each deformable assembly in the plurality of deformable assemblies has a vertex and a base. The each deformable assembly in the plurality of deformable assemblies has a height that is capable of changing to change a shape of the structure and a shape of the flexible skin.
摘要翻译： 一种装置包括具有第一侧，与第一侧基本相反的第二侧，柔性表皮和多个可变形组件的结构。 柔性皮肤附接到结构的第一侧和第二侧。 多个可变形组件可移动地连接到结构，其中多个可变形组件中的每个可变形组件具有顶点和底座。 多个可变形组件中的每个可变形组件具有能够改变以改变结构的形状和柔性皮肤的形状的高度。
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公开(公告)号：US20130104966A1
公开(公告)日：2013-05-02
申请号：US13286202
申请日：2011-10-31
IPC分类号： H01L31/048 , H01L31/18
CPC分类号： H01L31/0422 , B64C2201/021 , B64C2201/042 , B64D2211/00 , H01L31/042 , H02S10/40 , H02S20/00 , Y02B10/20 , Y02E10/50
摘要： In an embodiment of the disclosure, there is provided a strain isolation layer assembly. The assembly has a rigid solar layer; a strain isolation layer having a discontinuous configuration, a vertical rigidity, and a horizontal shear flexibility; and an underlying substrate layer. The strain isolation layer is coupled between the rigid solar layer and the underlying substrate layer to form a strain isolation layer assembly, such that the strain isolation layer isolates the rigid solar layer to reduce one or more strains induced on the rigid solar layer.
摘要翻译： 在本公开的一个实施例中，提供了应变隔离层组件。 该组件具有刚性的太阳能层; 具有不连续构型，垂直刚性和水平剪切挠度的应变隔离层; 和底层基底层。 应变隔离层耦合在刚性太阳能层和下面的基底层之间以形成应变隔离层组件，使得应变隔离层隔离刚性太阳能层以减少在刚性太阳能层上诱发的一种或多种应变。
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公开(公告)号：US20130099063A1
公开(公告)日：2013-04-25
申请号：US13276750
申请日：2011-10-19
CPC分类号： B64D27/24 , B64C3/18 , B64C3/182 , B64C3/185 , B64C3/187 , B64C3/22 , B64C3/26 , B64D2211/00 , Y02T50/44 , Y02T50/62 , Y02T50/64 , Y10T156/10
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.
摘要翻译： 飞机机翼具有多个翼段，其通过接头安装在翼梁上，允许翼梁和翼段之间的相对运动。 采用热膨胀系数的调整来减少温度变化引起的应力。
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