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    • 83. 发明授权
    • Fluidic thermoelectric generator
    • 流体热电发生器
    • US3839094A
    • 1974-10-01
    • US26773972
    • 1972-06-30
    • US ARMY
    • CAMPAGNUOLO C
    • F42C11/00F42C14/00F42C15/285F42C15/29F42C15/40H02N11/00H02N3/00
    • H02N11/002F42C11/008F42C14/00F42C15/285F42C15/29F42C15/40
    • A thermoelectric generator that utilizes the high temperature generated by fluid compression waves within a resonant tube that is subject to a supersonic air stream. The resonant tube, which may take any one of a number of forms, is located in a nose cone of the projectile that has a nozzle formed at the ogive for directing the fluid flow created while the projectile is in flight onto the open end of the resonant tube. This fluid flow sets up complex cyclical compression waves within the resonant tube which subsequently causes heating of the fluid therein due primarily to the friction within the tube and to the nonisentropic compression of the fluid interacting with the shock waves therein. The heating of the fluid and the high amplitude fluctuations cause a thermoelectric crystal placed near the closed end of the resonant tube to emit an electrical output. The electrical output may be utilized as a power source for any of a number of electrical devices within the projectile.
    • 一种热电发电机,其利用受到超音速气流影响的谐振管内由流体压缩波产生的高温。 可以采取多种形式的任何一种的共振管位于射弹的鼻锥中,其具有形成在喷嘴处的喷嘴,用于将抛射体飞行时产生的流体流引导到飞行器的开口端 谐振管。 该流体流在谐振管内设置复杂的周期性压缩波,其随后由于管内的摩擦和与其中的冲击波相互作用的非等熵压缩而导致其中的流体的加热。 流体的加热和高幅度波动导致放置在谐振管的封闭端附近的热电晶体发射电输出。 电输出可以用作射弹内的多个电气装置中的任何一个的电源。
    • 85. 发明授权
    • Miniaturized transmission line top loaded monopole antenna
    • MINIATURIZED传输线顶部负载单极天线
    • US3838429A
    • 1974-09-24
    • US38538273
    • 1973-08-03
    • US ARMY
    • REGGIA F
    • H01Q9/36H01Q9/00
    • H01Q9/36
    • A miniaturized antenna having high radiation efficiency consists essentially of an open circuit transmission line top-loading a short monopole over a metal ground plane. The currents in the two sides of the transmission line, being oppositely directed, tend to cancel each other''s effect in the distant field. Thus, only the short vertical monopole contributes to the distant field radiation. The omnidirectional monopole is a constant current radiating element operating at near RF ground potential (high current, low impedance).
    • 具有高辐射效率的小型化天线基本上由在金属接地平面上加载短单极子​​的开路传输线组成。 传输线两侧的相反方向的电流倾向于抵消在远处的影响。 因此,只有短的垂直单极子有助于远距离的场辐射。 全向单极子是在近RF地电位(大电流,低阻抗)下工作的恒流辐射元件。
    • 86. 发明授权
    • Liquid fuel-fired grille
    • 液体燃料盘
    • US3837329A
    • 1974-09-24
    • US37666273
    • 1973-07-05
    • US ARMY
    • MUTCHLER P
    • A47J37/06F24C3/00F24C3/06
    • F24C3/008A47J37/067Y02B40/166
    • A cooking surface or grille heated uniformly by the products of combustion from a liquid fuel-fired burner, wherein the products of combustion are caused to flow beneath the cooking surface of the grille through inverted V-shaped channels which define gastight passageways that extend from the back to the front of the grille and in the opposite direction through adjacent V-shaped gas-tight channels alternating with the inverted V-shaped channels to provide an efficient and uniform transfer of heat energy from the combustion gases to the cooking surface of the grille.
    • 通过来自液体燃料燃烧式燃烧器的燃烧产物均匀地加热的烹饪表面或格栅,其中燃烧产物通过形成气密通道的V形通道形成在格栅的烹饪表面下方, 从格栅的后部到前部,并且通过与倒V形通道交替的相邻V形气密通道在相反方向上提供从燃烧气体到烹饪表面的热能的有效且均匀的转移 格栅。
    • 87. 发明授权
    • Method and apparatus for rapid subsurface exploration
    • 用于快速表面勘探的方法和装置
    • US3836952A
    • 1974-09-17
    • US23176072
    • 1972-03-03
    • US ARMY
    • JOHNSON R
    • G01V1/00
    • G01V1/00
    • Exploring a selected zone of the earth to a shallow depth for a tunnel excavation, hollow, or other anomaly, without digging, which includes the use of a transmitter electro-seismic transducer and at least one receiver electro-seismic transducer for causing seismic energy to transmit from transmitter transducer to receiver transducer, through the ground in the selected zone, and examining for any unusual deviation in the phase angle difference between energy at the emitting transducer and energy at the receiving transducer as the span between transducers is displaced or as the span length is changed.
    • 探索地球的选定区域为浅层深度,用于隧道掘进,中空或其他异常,而不需要挖掘,其中包括使用变送器电 - 地震换能器和至少一个接收器电 - 地震换能器来使地震能量 从发射机传感器传输到接收机传感器,通过选定区域中的地面,并检查发射换能器的能量与传感器之间的能量之间的相位角差异中任何异常偏差,因为传感器之间的距离被移位或跨度 长度改变
    • 88. 发明授权
    • Supersonic chemical transfer laser
    • 超声波化学转移激光
    • US3832650A
    • 1974-08-27
    • US42156973
    • 1973-12-04
    • US ARMY
    • ROBERTS T
    • H01S3/0953H01S3/09H01S3/22
    • H01S3/0953
    • A laser having a gas generating section that delivers a flow of high pressure high temperature gas which contains a large concentration of active fluorine atoms (F) to a nozzle. This gas is expanded through a nozzle to achieve low pressure low temperature supersonic flow which still contains the large concentration of the active atoms. The nozzle includes one set of injection ports positioned so as to inject cold carbon dioxide gas (CO2) into the flow at a point in the nozzle where the flow is supersonic, just downstream of the throat; and another set positioned so as to inject deuterium (D2) into the flow after the CO2 has mixed with the fluorine containing flow, just at the nozzle exit plane. All gases exhaust from the nozzle into a lasing chamber wherein the energy of F + D2 reaction which initially appears as vibrational energy in the product DF molecule is transferred in collisions to the CO2 molecule. Thus producing a total inversion in the CO2 which allows the energy to be extracted as a laser beam from the flow.
    • 一种具有气体发生部分的激光器,其向喷嘴输送含有大量活性氟原子(F)的高压高温气体流。 该气体通过喷嘴膨胀以实现仍然含有大量活性原子的低压低温超音速流。 所述喷嘴包括一组注射口,所述注入口定位成将冷二氧化碳气体(CO 2)注入所述喷嘴中的流动超音速的点处,恰好在所述喉部的下游; 另一组定位成在CO 2与含氟流体混合之后恰好在喷嘴出口平面处,将氘(D2)注入流中。 所有气体从喷嘴排出到激光室,其中最初在产物DF分子中作为振动能产生的F + D2反应的能量以碰撞方式转移到CO 2分子。 因此在CO 2中产生总反转,其允许能量从流中作为激光束提取。
    • 89. 发明授权
    • Insulation application
    • 绝缘应用
    • US3830666A
    • 1974-08-20
    • US36932173
    • 1973-06-12
    • US ARMY
    • SCHNEIDER F
    • B29C63/00B64G1/58B32B31/26
    • B32B27/12B29C63/00B32B27/322B32B2262/101B32B2307/304B64G1/58Y10T428/31522Y10T442/138
    • Disclosed is a method for applying and curing thermo insulation to an aluminum substructure, and particularly, to an elliptical cone shaped aluminum substructure. The method comprises curing and bonding a thin covering of insulation to the aluminum substructure by a one step curing procedure. The insulation thickness is in the range of about 0.0600 inches. The insulation which is comprised of epoxy-phenolic film adhesive and silica fabric-phenolic resin is cured under a predetermined amount of heat and pressure for a predetermined amount of time to yield a cured and bonded insulation capable of withstanding extreme temperature and aerodynamic shear environment.
    • 公开了一种将热绝缘施加和固化到铝底层结构的方法,特别是涉及一种椭圆锥形铝底层结构。 该方法包括通过一步固化程序固化并将薄的绝缘覆盖物粘合到铝基底上。 绝缘厚度在约0.0600英寸的范围内。 由环氧 - 酚醛膜粘合剂和二氧化硅织物 - 酚醛树脂组成的绝缘体在预定量的热和压力下固化预定量的时间,以产生耐受极端温度和空气动力学剪切环境的固化和粘合的绝缘体。
    • 90. 发明授权
    • Settable pneumatic altitude detection equipment
    • 可设置的气动高度检测设备
    • US3827361A
    • 1974-08-06
    • US39752673
    • 1973-09-17
    • US ARMY
    • BARBIERI JCHANG NZECHNOWITZ AXENAKIS J
    • F42C5/02F42C9/16F42C5/00G01C19/30G01C21/00
    • F42C9/16F42C5/02Y10T74/12Y10T74/1239
    • A settable pneumatic altitude detection device provides an electrical signal to a missile or projectile for arming and destructing the missile or projectile at preset altitudes. The present invention''s main structural elements are a pair of sphere supports which hold therein a rotatable sphere assembly. The sphere support structure has two spherically shaped gas bearing pads which are separated and fixedly held to a circularly shaped collar. Two separate gas supplies are operatively positioned in the sphere support structure and in the rotatable sphere. An electrical initiating signal causes a gas release mechanism and a time delay valve, for each gas supply, to controllably release gas therefrom. Gas is forced through peripherally positioned jet nozzles on the sphere, and through operatively positioned venting ports and calibrated orifices in the sphere support structure. After the missile is fired, the sphere is pneumatically uncaged from its polar supporting structure so that it can freely spin on a nearly frictionless gas cushion. A pneumatically controlled distance meter operatively located in the sphere activates pressure operated switches on the ascent and the descent of the missile trajectory. The aforesaid switches provide an electrical signal which arms the missile on ascent and causes the missile to self-destruct on descent.
    • 可设置的气动高度检测装置为导弹或射弹提供电信号,用于在预设高度下布防和破坏导弹或射弹。 本发明的主要结构元件是一对球形支撑件,其中保持有可旋转的球体组件。 球体支撑结构具有两个球形的气体支承垫,它们被分离并固定地保持在圆形的套环上。 两个单独的气体供应器可操作地定位在球体支撑结构中并且在可旋转的球体中。 电启动信号使气体释放机构和每个气体供应的时间延迟阀可控制地从其中释放气体。 气体被迫通过球体上的外围定位的喷嘴,并且通过可操作地定位的排气口和球体支撑结构中的校准孔。 在导弹发射后,球体从其极性支撑结构中气动地开启,从而可以在几乎无摩擦的气垫上自由旋转。 可操作地位于球体中的气动控制距离计在导弹轨迹的上升和下降时激活压力操纵的开关。 上述开关提供一个电气信号,使导弹上升并使导弹在下降时自毁。