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公开(公告)号：US11987400B2
公开(公告)日：2024-05-21
申请号：US17503233
申请日：2021-10-15
申请人： Insitu, Inc.
IPC分类号： B64U20/70 , B64C1/34 , B64U101/19
CPC分类号： B64U20/70 , B64C1/34 , B64U2101/19
摘要： Expandable decoy unmanned aerial vehicles (UAVs) are disclosed. A disclosed example decoy UAV includes an expandable body at least partially defining an exterior of the expandable decoy UAV, an expander to expand the expandable body to a desired footprint, and a propulsion device operatively coupled to the expandable body, the propulsion device to move the expandable decoy UAV.
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公开(公告)号：US20230271714A1
公开(公告)日：2023-08-31
申请号：US18311985
申请日：2023-05-04
发明人： Scott Alan Schimmels , Jeffrey Douglas Rambo , Thomas Kupiszewski , Paul Alexander Intemann , Robert Proctor
摘要： A vehicle is provided including a structure including a skin defining an outside surface exposed to ambient cooling flow and an inside surface. The structure includes a first structural member extending from the inside surface of the skin and a second structural member extending from the inside surface of the skin; and a thermal management system including a heat exchanger assembly positioned adjacent to, and in thermal communication with, the inside surface of the skin, the heat exchanger assembly positioned at least partially between the first and second structural members of the structure.
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公开(公告)号：US20170320559A1
公开(公告)日：2017-11-09
申请号：US15528109
申请日：2015-11-19
发明人： Amir GAT , Shai ELBAZ , Yoav MATIA
CPC分类号： B64C3/185 , B29L2031/3085 , B64C1/34 , B64C3/38
摘要： A pressurized, fluid-filled channel network embedded in an elastic structure, asymmetrically to the neutral plane, is used to create a deformation field within the structure by the pressurization of the embedded fluidic network, which can be applied in accordance with external forces acting on the structure. The deformation of the structure resulting from the liquid pressure and geometry of the network is related to a continuous deformation-field function. This enables the design of networks creating steady arbitrary deformation fields as well as to eliminate deformation created by external time varying forces, thus increasing the effective rigidity of the beam. By including the effects of the deformation created by the channel network on the beam inertia, the response of the beam to oscillating forces can be modified, enabling the design of channel networks which create pre-defined oscillating deformation patterns in response to external oscillating forces.
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公开(公告)号：US20150217848A1
公开(公告)日：2015-08-06
申请号：US14667068
申请日：2015-03-24
申请人： Kevin Arash Peyman , Nazmi Peyman
发明人： Kevin Arash Peyman , Nazmi Peyman
CPC分类号： B64G1/002 , B64B1/40 , B64B1/62 , B64C1/34 , B64C37/02 , B64G1/005 , B64G1/22 , B64G1/401 , B64G2001/224
摘要： An aerospace vehicle comprising an airplane or spacecraft, operatively coupled to an airship balloon containing lighter than air gas adapted to elevate the vehicle. A control system adapted to deflate the balloon upon reaching a specific altitude by directing the gas to a propulsion system and high pressure gas chambers for powering the vehicle at a greater speed or to a greater altitude. The balloon can be retracted into the vehicle to achieve a better aerodynamic shape and further re-inflated for decreasing the speed of the vehicle upon reaching a destination.
摘要翻译： 一种航空航天车辆，其包括飞行器或航天器，其可操作地联接到包含比适于提升车辆的空气气体更轻的飞艇气球。 一种控制系统，其适于通过将气体引导到推进系统达到特定高度而放气，并且高压气体室以更高的速度或更高的高度向车辆供电。 气囊可以缩回到车辆中以获得更好的空气动力学形状，并进一步重新充气以便在到达目的地时降低车辆的速度。
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公开(公告)号：US20120211598A1
公开(公告)日：2012-08-23
申请号：US13445708
申请日：2012-04-12
CPC分类号： B64C1/34 , B64C3/385 , B64C13/28 , B64C2201/105 , Y02T50/14
摘要： An apparatus may comprise an inflatable control surface for an aircraft and an end of the inflatable control surface configured for attachment to a fuselage of the aircraft. The end of the inflatable control surface may be configured to be rotated about an axis to control movement of the aircraft during flight.
摘要翻译： 装置可以包括用于飞行器的可充气控制表面和构造成附接到飞行器的机身的可充气控制表面的一端。 可充气控制表面的端部可以被构造为绕轴线旋转以控制飞行器在飞行过程中的运动。
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公开(公告)号：US20110127373A1
公开(公告)日：2011-06-02
申请号：US11217851
申请日：2005-09-01
CPC分类号： B64C1/34 , B64C3/185 , B64C3/34 , B64C39/024 , B64C2201/042 , B64C2201/105 , B64D27/24 , B64D37/04 , B64D37/06 , B64D37/30 , B64D41/00 , H01L35/30 , Y02T50/44 , Y02T50/53 , Y02T50/62
摘要： A vehicle including at least one bladder for containing a fuel as liquid and gas at a predetermined pressure, with a bladder outlet arranged to releasing fuel from the bladder and to maintain the fuel in the bladder at the predetermined pressure, the fuel provides thrust to the vehicle upon combustion, the fuel-filled bladder providing initial structural integrity of the vehicle. In an exemplary embodiment, the vehicle is an unmanned anal vehicle. A combustion chamber and thermoelectric conversion module can generate electricity for a propellor and battery from the fuel supply. Internal vapor pressure is maintained until the fuel bladder is empty.
摘要翻译： 一种车辆，包括用于将燃料作为液体和气体以预定压力容纳的至少一个气囊，其中气囊出口布置成从气囊释放燃料并将气体中的燃料保持在预定压力，燃料提供推力 燃料填充的气囊提供车辆的初始结构完整性。 在示例性实施例中，车辆是无人驾驶的肛门车辆。 燃烧室和热电转换模块可以从燃料供应器为推进器和电池发电。 保持内部蒸汽压力，直到燃料囊为空。
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公开(公告)号：US5881970A
公开(公告)日：1999-03-16
申请号：US434981
申请日：1995-05-04
摘要： An aircraft with automated means to transport. Spherical or one of its segments, without airfoils for lift or guidance. Means for flight are housed within the aircraft. The outer-most sureface is configured to disrupt the air-flow, over its surfaces, in flight. This, to reduce skin-friction and drag coefficients, and mollify heat build-up on the skins outer surfaces as speeds increase to and beyond mach 1. The weight of gas per unit volume, with temperature variations, is the means to reduce the gross-weight and adjust for temperature and weight changes during flight. Propulsion, within the propulsion component, is provided by turbojet engines. They are secured within an inner compression pod and an outer combustion pod. The compression pod and the attached vertical-air-duct, rotate through three hundred sixty degrees, as the means for directional guidance and direct thrust. Augmented power-thrust-tubes extend outward from the combustion pod to the mid-horizontal circumference of the aircraft. Control baffles, on each thrust-tube, check, deflect and regulate the engines' thrust to control the motivity of the aircraft. Struts retract for flight and are extended for landing. These electro-hydraulic struts, level, raise and lower the aircraft for direct ground level support operations. The aircraft has the means to maintain a horizontal flight attitude. For flight aptness the aircraft has an internal, mechanical and scientific means, for vertical ascent and vertical descent without horizontal motivity, to hover and maintain a position and altitude. And during horizontal flight, climb and descend, and perform heading changes. These flight means are all performed in the aircrafts' horizontal attitude.
摘要翻译： 一架具有自动化装置的飞机。 球形或其中一个段，没有用于升降或引导的翼型。 飞机的方式安置在飞机内。 最外面的表面配置为在飞行中破坏其表面上的空气流。 这是为了减少皮肤摩擦和阻力系数，并且随着速度增加到超过马赫1，在皮肤外表面上的热积累变得虚弱。每单位体积的气体重量与温度变化是减少毛重 重量，并适应飞行过程中的温度和重量变化。 在推进组件内的推进由涡轮喷气发动机提供。 它们固定在内部压缩舱和外部燃烧舱内。 压缩舱和连接的垂直风道，旋转三百六十度，作为定向导向和直接推力的手段。 增强的动力推力管从燃烧舱向外延伸到飞行器的中部水平周边。 控制挡板，在每个推力管上，检查，偏转和调节发动机的推力以控制飞机的动力。 Struts撤回飞行，并延长着陆。 这些电动液压支柱，水平，升高和降低飞机直接地面水平支持操作。 飞机有维持水平飞行姿态的手段。 对于飞行适应性，飞机具有内部，机械和科学的手段，用于垂直上升和垂直下降，没有水平动力，可以悬停并保持位置和高度。 在水平飞行中，爬升和下降，并执行航向变化。 这些飞行手段都是以飞机的横向姿态进行的。
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公开(公告)号：US3913871A
公开(公告)日：1975-10-21
申请号：US46641774
申请日：1974-05-02
申请人： MILLER RALPH H
发明人： MILLER RALPH H
CPC分类号： B64C39/00 , B64B2201/00 , B64C1/34
摘要： Improvement in heavier-than-air passenger aircraft having forward thrust engines, wings, a rear fin and rudder, and a lighter-than-air gas lift mechanism for enhancing the aerodynamic lift provided by the forward thrust engines and wings, such improvement comprising respective forward and rear wings, two equally widthwise spaced apart gas compartments containing lighter-than-air gas disposed vertically above the forward wing, a passenger compartment having a pilot compartment at the front end thereof, the passenger compartment disposed vertically above the forward wing and transversely centrally between the gas compartments, the forward and rear wings and the three compartments joined to each other to provide framing rigidity for said aircraft, the rear fin and rudder mounted upon the passenger compartment so as to upstand vertically therefrom to obtain a clear aerodynamic cut into the air, each compartment of substantially uniform transverse cross-section, each compartment extending axially substantially full length of said 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.
摘要翻译： 具有向前推力发动机，翼，后翼和方向舵的重型客机的改进，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于空气的气举升降机构，其改进包括各自的 前翼和后翼，两个等宽度方向间隔开的气室，其包含垂直设置在前翼上方的轻于空气的气室，在其前端具有先导舱的乘客舱，在前翼上方垂直设置的乘客舱 在气室之间的中央，前翼和后翼与三个隔间相互连接，为所述飞机提供框架刚性，后鳍和方向舵安装在乘客舱上，从而垂直向上竖立，以获得清晰的气动切割 空气，每个隔室的横截面基本均匀，每个隔室延伸一个 所述飞行器的基本上全长，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。
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9.发明申请公开(公告)号：US20180170579A1
公开(公告)日：2018-06-21
申请号：US15383267
申请日：2016-12-19
申请人： EMBRAER S.A.
发明人： Rogério Scafutto SCOTTON , Natália Vianna CORREIA , Luiz Fernando DOS SANTOS , Thomas WARING , Richard WARING
CPC分类号： B64C1/1407 , B05B12/32 , B05B13/041 , B05B13/0431 , B05B13/06 , B05B13/0618 , B05B13/069 , B05B15/60 , B05D1/02 , B05D7/22 , B25J5/005 , B25J11/0075 , B64C1/143 , B64C1/1438 , B64C1/1461 , B64C1/18 , B64C1/22 , B64C1/34 , B64F5/10 , Y10S901/01 , Y10S901/27
摘要： Systems and methods are provided by which a treatment fluid (e.g., a liquid corrosion inhibitor) may be applied onto the interior surfaces of an aircraft fuselage which employ an automated guided vehicle (AGV) comprising a carriage assembly and a robotic spray system carried by the carriage assembly supported by a support platform positioned laterally of an aircraft fuselage in alignment with the cabin door opening thereof. The AGV may thus be deployable through the cabin door opening of the fuselage to a deployed position within the interior of the fuselage so as to be moveable along a longitudinal axis of the fuselage to allow the robotic spray assembly to spray the treatment fluid onto interior surfaces of the fuselage. A sealing door assembly located rearwardly of the AGV which is moveable relative to a door opening in the fuselage may also be provided so as to sealingly close the door opening of the fuselage when the AGV is deployed within the interior of the fuselage.
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公开(公告)号：US20170008609A1
公开(公告)日：2017-01-12
申请号：US15270922
申请日：2016-09-20
申请人： Kevin Arash Peyman , Nazmi Peyman
发明人： Kevin Arash Peyman , Nazmi Peyman
CPC分类号： B64G1/002 , B64B1/40 , B64B1/62 , B64C1/34 , B64C37/02 , B64G1/005 , B64G1/22 , B64G1/401 , B64G2001/224
摘要： The present invention relates to an aerospace vehicle comprising an airplane or spacecraft, operatively coupled to an airship balloon containing lighter than air gas adapted to elevate the vehicle. A control system adapted to deflate the balloon upon reaching a predetermined altitude by directing the gas for powering the vehicle at greater speed. The balloon can be re-inflated for decreasing the speed of the vehicle upon reaching a destination and deflated in a controlled manner for landing the vehicle or disengaged from the vehicle upon transferring the gas from the balloon to a propulsion system of the vehicle.
摘要翻译： 本发明涉及一种航空航天车辆，其包括飞行器或航天器，其可操作地耦合到包含比适于提升车辆的空气气体更轻的飞艇气球。 一种控制系统，其适于通过引导用于以更高速度为车辆供电的气体达到预定高度而使气囊放气。 气囊可以被重新充气，以便在到达目的地时降低车辆的速度并且以可控的方式放气，以便在将气体从气囊转移到车辆的推进系统时将车辆着陆或脱离车辆。
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