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公开(公告)号：US20170158304A1
公开(公告)日：2017-06-08
申请号：US15366126
申请日：2016-12-01
CPC分类号： B64C1/10 , B64C1/34 , B64C2001/0072
摘要： A pressure bulkhead for an aircraft comprising a fuselage. The pressure bulkhead comprises an inflatable element, suitable for being filled with air, which in turn comprises a cover which delimits an inner zone. The pressure bulkhead further comprises a seal suitable for providing an airtight seal between the cover and the fuselage of the aircraft.
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公开(公告)号：US08746620B1
公开(公告)日：2014-06-10
申请号：US13747626
申请日：2013-01-23
CPC分类号： B64C1/34 , B64C3/30 , B64C3/46 , B64C39/024 , B64C2201/021 , B64C2201/105 , B64C2201/122 , B64D2211/00 , H01L31/0543 , H02S10/40 , H02S20/32 , Y02E10/52 , Y02T50/14
摘要： Methods and apparatus for an adaptable solar airframe are provided herein. In some embodiments, an adaptable solar airframe includes a solar PV system having at least one solar tracking system and being able to follow the sun position in order to increase sunlight collection and power output; and an expandable body having an aerodynamic cross-section that minimizes parasitic air drag at any given thickness of the body, further being at least partially transparent to sunlight, further enclosing the solar PV system, and further being able to change its shape in response to changes in the positions of the solar PV system.
摘要翻译： 本文提供了适用于太阳能机身的方法和装置。 在一些实施例中，适应性太阳能机身包括具有至少一个太阳能跟踪系统并且能够跟随太阳位置以增加阳光收集和功率输出的太阳能PV系统; 以及具有空气动力学横截面的可膨胀体，该空气动力学横截面最小化在本体的任何给定厚度的寄生空气阻力，进一步包围太阳能光伏系统，并进一步包围太阳能光伏系统，并且还能够响应于 太阳能光伏系统的位置变化。
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公开(公告)号：US20050077426A1
公开(公告)日：2005-04-14
申请号：US10961801
申请日：2004-10-08
申请人： Martin Simard
发明人： Martin Simard
CPC分类号： B64D25/18
摘要： An emergency flotation device for crashed small airplanes which can be retrofited on most small airplanes as well as come preinstalled on new small airplanes, is self contained in a small container; has several independent triggering means; and has a visual as well as an RF beacon system integrated within to call for rescue.
摘要翻译： 在小型飞机上安装了可以在大多数小型飞机上进行改装的坠毁的小型飞机的紧急浮选装置，它们装在小型集装箱中; 有几个独立的触发手段; 并具有视觉以及集成在其中的RF信标系统，以求救援。
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公开(公告)号：US5425515A
公开(公告)日：1995-06-20
申请号：US205200
申请日：1994-03-03
申请人： Tokuzo Hirose
发明人： Tokuzo Hirose
摘要： The object of the invention is to provide an aircraft which is capable of being enhanced in speed and preventing a crash even when a propeller does not operate to provide thrust to the aircraft. A wing which is an envelope made of a flexible material is comprised on an upper side of a aircraft body, and is filled with a gas with a specific gravity less than that of air. Moreover, the aircraft body is provided with a propeller.
摘要翻译： 本发明的目的是提供一种能够提高速度并且即使当螺旋桨不操作以向飞行器提供推力时也防止碰撞的飞机。 作为由柔性材料制成的信封的机翼包括在飞行器主体的上侧，并且填充比重小于空气的比重的气体。 此外，飞机主体设有螺旋桨。
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公开(公告)号：US4843992A
公开(公告)日：1989-07-04
申请号：US70821
申请日：1987-07-02
申请人： Sarkis S. Babikian
发明人： Sarkis S. Babikian
摘要： The cylindrical shape tube consists of a pressure valve and a safety valve. Whether the tube's contents be made of metal, expandable or non-stretchable materials, it has the ability to retain low air pressure. For safety purposes, any excess air pressure is released through the safety valve when the belts are made of metal content, the lengthwise belts have flares and grooves, the crosswise belts have oblong holes. When the belts are made of expandable or non-stretchable materials, snap head and grooves are cast within the lengthwise belts, the crosswise belts have round holes. The metal crosswise belts with their oblong holes can be engaged onto both the snap heads of the expandable lengthwise belts and flares of metal lengthwise belts. The expandable crosswise belts with their round holes can be snapped onto the snap heads of the expandable lengthwise belts and flares of the metal lengthwise belts. When a number of the completed air tubes protected by belts are interlocked, whether cross mannered or layered, it increases the potential of the lifting capacity for any load.
摘要翻译： 圆柱形管由压力阀和安全阀组成。 管的内容物是否由金属，可膨胀或不可拉伸材料制成，具有保持低气压的能力。 为了安全起见，当皮带由金属成分制成时，通过安全阀释放任何过量的空气压力，纵向带有喇叭口和槽，横向带具有长方形孔。 当皮带由可膨胀或不可拉伸的材料制成时，卡扣头和凹槽在纵向皮带内铸造，横向皮带有圆孔。 具有长方形孔的金属横向带可以接合到可伸缩长度带的卡扣头和金属纵向带的弹簧上。 具有圆形孔的可膨胀横向带可以卡扣在可伸缩长度带的卡扣头和金属纵向带上。 当一些由皮带保护的完成的空气管是互锁的，无论是交叉的还是分层的，它增加了任何负载的起重能力的潜力。
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56.发明授权Mechanism for automatically actuating a rescue device upon opening of an exit door 失效在打开出口门时自动启动救援装置的机构
公开(公告)号：US4715562A
公开(公告)日：1987-12-29
申请号：US821259
申请日：1986-01-22
申请人： Jean Bokalot
发明人： Jean Bokalot
CPC分类号： B64C1/143 , B64C1/1407 , B64D25/14 , Y10S244/905
摘要： This invention relates to a mechanism for automatically actuating a rescue device upon opening of a panel obturating an exit and bearing said rescue device, mechanism comprising a control bar connected to said rescue device and adapted, under the action of a voluntary actuating member, to be rendered fast either with said panel or with the periphery of said exit, with the result that opening of said panel does not bring about, or brings about, respectively, actuation of said rescue device via said control bar. According to the invention, this mechanism is characterized in that said control bar is fast in displacement with a mobile system controlled by said voluntary actuating member in order to subject said bar to a movement of translation parallel to itself, of direction at least substantially at right angles to said panel. The invention is more particularly applicable to the automatic control of escape slides, slide/rafts or the like in the event of an emergency.
摘要翻译： 本发明涉及一种用于在打开一个堵塞出口并承载所述救援装置的面板时自动启动救援装置的机构，该机构包括连接到所述救援装置的控制杆，并且在自愿致动构件的作用下适应 通过所述面板或与所述出口的周边快速地呈现，结果是所述面板的打开不会分别导致所述救援装置经由所述控制杆的启动或带来。 根据本发明，该机构的特征在于，所述控制杆具有由所述自愿致动构件控制的移动系统的位移快速，以便使所述杆平行于自身的平移运动，至少基本上在右侧的方向 与所述面板的角度。 本发明更特别适用于在紧急情况下自动控制逃生滑梯，滑板/筏等。
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57.发明授权
公开(公告)号：US3907218A
公开(公告)日：1975-09-23
申请号：US46641874
申请日：1974-05-02
申请人： MILLER RALPH H
发明人： MILLER RALPH H
CPC分类号： B64C1/34 , B64B2201/00 , B64C39/04
摘要： Improvements in heavier-than-air freight aircraft having forward thrust engines, wings, a rear fin and rudder, and a lighter-thanair gas lift mechanism for enhancing the aerodynamic lift provided by the forward thrust engines and wings, such improvement comprising respective forward and rear wings, three equally widthwise spaced apart gas compartments containing lighter-than-air gas disposed vertically above the forward wing, a freight compartment disposed vertically below the gas compartments, the forward and rear wings and the four compartments joined to each other to provide framing rigidity for the aircraft, the rear fin and rudder mounted upon the center one of the gas compartments so as to upstand vertically therefrom to obtain a clear aerodynamic cut into the air, a pilot compartment at the forward end of the center one of the gas compartments, each gas compartment of substantially uniform transverse crosssection, each compartment extending axially substantially full length of the aircraft, the rear wing being a substantially full width rear wing disposed vertically above the forward wing so as to have a substantially clear aerodynamic cut into the air, said forward wings comprising left and right forward partial-wing sections joined to the freight compartment.
摘要翻译： 具有前推力发动机，机翼，后排翼和方向舵的重型空中货运飞机的改进以及用于增强由前推力发动机和机翼提供的空气动力升力的轻型空气气举升降机构，其改进包括各自的 前翼和后翼，三个等宽度方向间隔开的气体舱，其包含垂直设置在前机翼上方的轻于空气的气体，垂直设置在气体隔间下方的货舱，前后翼和四个彼此连接的隔间 为飞机提供框架刚性，后鳍和方向舵安装在气体隔间的中心一个上，以便垂直地竖立，从而获得空气中明确的空气动力学切割，在中心的一端的前导舱 气体隔室，每个气室具有基本均匀的横截面，每个隔室沿轴向基本上全长延伸 飞行器，后翼是垂直设置在前翼上方的基本上全宽度的后翼，以便具有基本上清楚的空气动力学切入空气，所述前翼包括连接到货舱的左右前部分翼段。
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公开(公告)号：US3743440A
公开(公告)日：1973-07-03
申请号：US3743440D
申请日：1971-01-18
申请人： MOORE A
发明人： MOORE A
摘要： A helicopter, autogyro, windmill or other impeller, comprising blades, optionally resilient or substantially rigid, each having: a tip free of attachment to other blades and urged into extended position by centrifugal force; and blade-strengthening tubular members containing gaseous material, imbedded in foam plastic. Each tubular member may be: an elongated flat-ended tube or can; or a row of end-joined tubes or cans. The gaseous material may be: helium, air or other gas (preferably strongly pressurized); gas-cell-containing foam plastic; or other, gas-containing material. The preferably hinged form of the impeller comprises at least one aligned pair of blades (two pairs being shown), each pair comprising inflated tubes extending from one end of the blades to the other end, having walls of: thin ductile or resilient metal (preferably lead), optionally coated with rubberimpregnated fabric or with rubber or other resilient plastic; plastic-coated fabric; resilient plastic; glass; or the like. Each tube has flattened and sealed ends and a flattened middle portion clamped by a plate to the impeller shaft, providing flexible, integral hinges at this middle portion permitting tilting of the blades, balancing centrifugal and aerodynamic forces on each side of the rotary shaft. The flat-ended tubes are preferably flanked by blade-stiffening tubular members preferably rows of metal cans, end-joined by preferably resilient plastic. When the tubular members are of plastic or glass they optionally may be blow-molded or centrifugally molded.
摘要翻译： 直升机，自动扶梯，风车或其他叶轮，包括任选弹性或基本上刚性的叶片，每个叶片具有：与其它叶片无关的尖端，并通过离心力推动到延伸位置; 和含有气态材料的嵌入泡沫塑料的叶片加强管状构件。 每个管状构件可以是：细长的平端管或罐; 或一排端接管或罐。 气体材料可以是：氦气，空气或其他气体（优选强力加压）; 含气泡泡沫塑料; 或其他含气材料。 叶轮的优选铰接形式包括至少一对成对的叶片（示出两对），每对叶片包括从叶片的一端延伸到另一端的膨胀管，其具有：具有薄的延展性或弹性金属的壁 铅），任选地涂覆有橡胶浸渍的织物或与橡胶或其它弹性塑料; 塑胶面料; 弹性塑料; 玻璃; 或类似物。 每个管具有扁平和密封的端部以及由板夹持到叶轮轴的扁平的中间部分，在该中间部分处提供柔性的整体铰链，允许叶片倾斜，平衡离心力和空气动力在旋转轴的每一侧上。 平端管优选地侧翼为叶片加强的管状构件 - 优选地是通过优选弹性塑料端接的金属罐排。 当管状构件为塑料或玻璃时，它们可任选地被吹塑或离心模塑。
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公开(公告)号：US3559923A
公开(公告)日：1971-02-02
申请号：US3559923D
申请日：1969-05-06
申请人： MOORE ALVIN E
发明人： MOORE ALVIN EDWARD
摘要： A strong, slightly heavier than air helicopter or like vehicle having: hinged, resilient lifting-propeller blades comprising gas-inflated tubes; a substantially rigid cabin comprising gascontaining tubes and a strong skin means; a landing cushion of easily deformable material which maintains its outer shape in flight; a steering propeller supported in a doughnut-shaped tube that is housed in a strong, streamlined skin; and balloon means at the top of the craft for lightening its weight and stabilizing it against pitching and rolling. The cabin''s main, load-carrying part is cylindrical, or optionally oblong or barrel-shaped; and optionally its tubular members are in stavelike elements having strong, planar sides that are epoxy-glued together.
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公开(公告)号：US3285003A
公开(公告)日：1966-11-15
申请号：US42817065
申请日：1965-01-26
申请人： DUNLOP RUBBER CO
CPC分类号： B64C1/34 , B64C29/0058 , B64D33/02 , F02C7/042
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