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1.发明授权Controlled explosive, hypervelocity self-contained round for a large caliber gun 失效大口径枪的控制爆炸，超高速独立圆
公开(公告)号：US5016537A
公开(公告)日：1991-05-21
申请号：US490378
申请日：1990-03-08
Applicant: George T. Pinson
Inventor： George T. Pinson
Abstract: A round for placement and firing in the barrel of a large caliber gun, the round comprising a cartridge case defining a cylindrical chamber having axially opposed open and closed ends, a plurality of axially-adjacent annualr explosive charges coaxially-disposed in the chamber, the charges defining a bore coaxial with said chamber and each charge being shaped to generate on detonation a predetermined shock wave in the case, a projectile disposed in the chamber proximate the closed end, the projectile having a trailing end shaped to convert shock waves generated by detonation of the annular charges to projectile acceleration, an explosive in the case for initially propelling the projectile axially through the bore toward the open, end, an electrical detonator for each annular charge responsive to an electrical signal, and a power source and circuit for generating the electrical signal in response to axial movement of the projectile in the bore.
Abstract translation: 一个用于在大口径枪的枪管中放置和击发的圆，该圆形包括限定具有轴向相对的开放和封闭端的圆柱形腔室的盒壳体，同轴地设置在腔室中的多个轴向相邻的年度炸药， 限定与所述室同轴的孔，并且每个电荷被成形为在爆炸时产生预定的冲击波，在该情况下，放置在靠近封闭端的小室中，抛射体具有成形为转换由爆炸产生的冲击波的后端 的环形电荷到弹丸加速度，在最初将射弹轴向推动通过孔朝向开放端的情况下的爆炸物，响应于电信号的每个环形电荷的电雷管，以及用于产生 响应于射弹在孔中的轴向运动的电信号。
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公开(公告)号：US5012991A
公开(公告)日：1991-05-07
申请号：US493821
申请日：1990-03-15
Applicant: George T. Pinson
Inventor： George T. Pinson
Abstract: A tube-launched projectile includes an airframe with an open aft end, an optical fiber dispensing bobbin, and an obturator having a rocket motor attached to a hard point in the aft end of the airframe. The obturator forms a pressure vessel with insulated inner walls which contain rocket propellant and an igniter. An ejectable plug located in the rocket nozzle is expelled upon motor ignition.
Abstract translation: 管发射的射弹包括具有开口后端的机身，光纤分配线轴和具有附接到机身后端的硬点的火箭发动机的闭孔器。 闭孔器形成具有绝热内壁的压力容器，其包含火箭推进剂和点火器。 位于火箭喷嘴中的可弹出式插头在电机点火时被排出。
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公开(公告)号：US4886562A
公开(公告)日：1989-12-12
申请号：US32242
申请日：1987-03-31
Applicant: George T. Pinson
Inventor： George T. Pinson
CPC classification number: G02B6/4432 , G02B6/4486 , Y10S118/18 , Y10S118/19 , Y10S118/22
Abstract: A method of manufacturing reinforced optical fiber including conveying optical fiber from a source; symmetrically, coaxially winding reinforcing fiber to a selected density per unit length around the optical fiber; forming an resin matrix among the reinforcing fibers; and coating the resin matrix with an external coating. Reinforcing a predetermined length of an elongated optical fiber comprises gradually reducing the thickness of the external coating and then gradually reducing the density of reinforcing fiber and the thickness of the resin matrix to form a transition from a reinforced fiber and a non-reinforced fiber.
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公开(公告)号：US4838502A
公开(公告)日：1989-06-13
申请号：US169223
申请日：1988-03-16
Applicant: George T. Pinson
Inventor： George T. Pinson
Abstract: A cavity in an airframe from which an airfoil is deployed is automatically closed to reduce aerodynamic drag by a fairing element hinged to the force and aft cavity edges and resiliently deformable from an unbent aerodynamic position outside the cavity to a bent position within the cavity. The non-deployed airfoil overlies the bent fairing element and retains the fairing in a bent position against the resilient force tending to restore it to the unbent position, until airfoil deployment.
Abstract translation: 翼面展开的机身中的空腔被自动关闭，以通过铰接到力腔和后缘边缘的整流元件来减小空气动力学阻力，并且能够从空腔外的空气动力学位置弹性变形到空腔内的弯曲位置。 未展开的翼型件覆盖弯曲的整流元件，并且将整流罩保持在弯曲位置，抵抗弹性力，以将其恢复到未弯曲的位置，直到机翼展开。
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公开(公告)号：US4735382A
公开(公告)日：1988-04-05
申请号：US819134
申请日：1986-01-15
Applicant: George T. Pinson
Inventor： George T. Pinson
IPC: B64G1/42
CPC classification number: B64G1/426 , Y10T74/2117
Abstract: A space craft cellular energy generating and storage device for generating electrical power in space and storing the power for extended periods of time. The space craft generating and storage device characterized by having a pair of annular rotating housings having a plurality of individual compartments therein. The compartments receiving material which is compartmentalized to accurately control the mass distribution during the rotation of the housing for maintaining speed as energy is withdrawn or generated.
Abstract translation: 一种用于在空间中产生电力并将电力长时间存储的太空工艺细胞能量产生和存储装置。 其特征在于具有一对在其中具有多个单独隔室的环形旋转壳体。 所述隔间接收材料，其被隔室以在壳体旋转期间精确地控制质量分布，以便在能量被抽出或产生时保持速度。
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Patent Agency Ranking
公开(公告)号：US4730154A
公开(公告)日：1988-03-08
申请号：US890928
申请日：1986-07-31
Applicant: George T. Pinson
Inventor： George T. Pinson
CPC classification number: H02J3/30 , H02J15/00 , H02K7/025 , Y02E60/16 , Y10T74/2117
Abstract: A variable inertia energy storage system for storing large amounts of mechanical energy for an extended period of time on land or on a mobile vehicle. The energy storage system can also be used for generating electrical power for use on demand by a subsystem or the like.
Abstract translation: 一种用于在陆地或移动车辆上长时间存储大量机械能的可变惯性能量存储系统。 能量存储系统还可用于产生由子系统等按需要使用的电力。
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公开(公告)号：US4725766A
公开(公告)日：1988-02-16
申请号：US891301
申请日：1986-07-31
Applicant: George T. Pinson
Inventor： George T. Pinson
CPC classification number: H02K7/025 , B64G1/426 , H02J15/00 , Y02E60/16 , Y10T74/2117
Abstract: A multiple spoke energy storage system used in a space environment for storing large amounts of mechanical energy for extended periods of time. The storage system also provides means for generating electrical power that can be used to meet subsystem demands.
Abstract translation: 一种在空间环境中使用的多辐射能量储存系统，用于长时间储存大量的机械能。 存储系统还提供用于产生可用于满足子系统需求的电力的装置。
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公开(公告)号：US4684080A
公开(公告)日：1987-08-04
申请号：US741856
申请日：1985-06-06
Applicant: George T. Pinson
Inventor： George T. Pinson
IPC: F17C7/04 , F42B10/64 , F42B15/033
CPC classification number: F17C7/04 , F42B10/64 , F42B10/663 , F17C2201/0109 , F17C2205/0338 , F17C2221/038 , F17C2223/0153 , F17C2223/036 , F17C2227/0304 , F17C2250/032 , F17C2270/0186
Abstract: A high pressure gas supply system used for storing and activating a fluid in a liquid form and converting the liquid to a high pressure gas when needed. The high pressure gas is used for the control and stability of missile fin actuators, canards, hot or cold gas thrusters and other applications on a missile.
Abstract translation: 一种高压气体供应系统，用于储存和激活液体形式的流体，并在需要时将液体转化为高压气体。 高压气体用于控制和稳定导弹翅片执行器，卡车，热或冷气体推进器和导弹上的其他应用。
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公开(公告)号：US4615496A
公开(公告)日：1986-10-07
申请号：US688532
申请日：1985-01-03
Applicant: George T. Pinson
Inventor： George T. Pinson
IPC: F41G7/22
CPC classification number: F41G7/2253 , F41G7/008 , F41G7/2213 , F41G7/2226 , F41G7/2293
Abstract: A hybrid semi-strapdown infrared seeker for mounting in a missile or the like. The seeker processing both imaged and non-imaged data available around a potential target area displayed on a vidicon and providing a level of target identification, target discrimination, target acquisition and attack at the target's controid or other selected points on the target.
Abstract translation: 用于安装在导弹等中的混合半架红外探测器。 寻求者处理在虚拟机上显示的潜在目标区域周围可用的成像和非成像数据，并且在目标的对象或目标的其他选择点上提供目标识别，目标识别，目标获取和攻击的级别。
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公开(公告)号：US4604592A
公开(公告)日：1986-08-05
申请号：US602207
申请日：1984-04-19
Applicant: George T. Pinson
Inventor： George T. Pinson
Abstract: An electrically controlled radio frequency tuner used in conjunction with an antenna. The antenna used both as a transmitter and a receiver. The tuner eliminating waveform reflection and circulator feedthrough of transmitted signals which heretofore reflected back into the receiver creating a noise threshold that decreased the sensitivity of the receiver.
Abstract translation: 与天线结合使用的电控射频调谐器。 天线既用作发射机又用于接收机。 消除了传输信号的波形反射和循环器馈通的调谐器，其以前反射回接收机，产生降低接收机的灵敏度的噪声阈值。
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