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1. 发明授权

US3927740A Brake disk with tapered key way 失效
标题翻译：制动盘采用锥形键方式
公开(公告)号：US3927740A
公开(公告)日：1975-12-23
申请号：US48441174
申请日：1974-07-01
申请人： GOODYEAR AEROSPACE CORP
发明人： ZAREMBKA ROBERT L
IPC分类号： B64C25/44 , F16D65/12
CPC分类号： F16D65/126
摘要： Disclosed is a brake disk and associated reinforcement clip wherein the brake disk contains a plurality of trapezoidal key slots spaced about a peripheral edge thereof for making engagement with a similar plurality of trapezoidal keys. Metallic reinforcement clips having trapezoidal key slots therein are utilized for reinforcing the key slots of the brake disk when the disk is composed of carbon or other material of low force resistance. The clip includes caps interconnecting the sides thereof along the entire length of the clip but for the key slot area so as to substantially encapsulate the peripheral edge of the disk.
摘要翻译：公开了一种制动盘和相关联的加强夹，其中制动盘包括围绕其周边边缘间隔开的多个梯形钥匙槽，用于与相似的多个梯形钥匙接合。金属加强夹具有梯形钥匙槽，用于加强制动盘的键槽，当盘由碳或其他低力阻力的材料组成时。该夹子包括沿着剪辑的整个长度互连其侧面的盖，但是用于键槽区域，以便基本上封装盘的周边边缘。

2. 发明授权

US3907076A Key slot segments for driving brake discs 失效
标题翻译：用于驱动制动盘的钥匙槽段
公开(公告)号：US3907076A
公开(公告)日：1975-09-23
申请号：US39553073
申请日：1973-09-10
申请人： GOODYEAR AEROSPACE CORP
发明人： CROSSMAN RICHARD L , COOK ALBERT W , HAWLEY JESSE G
IPC分类号： F16D65/12
CPC分类号： F16D65/126 , F16D65/121 , F16D2065/1312
摘要： Annular brake discs are provided with metal key slot segments. The metal segments are fastened such as by rivets to the discs and the location of the fasteners are positioned to evenly distribute torque load through the metal segments to the discs. The discs may be either of single piece, multiple piece, or segmented construction. In the segmented construction the metal keyway segments also serve as links connecting the disc segments together. The method for mounting the segments to the discs is also covered.
摘要翻译：环形制动盘配有金属钥匙槽段。金属段通过铆钉固定到盘上，紧固件的位置被定位成将扭矩负载通过金属段均匀地分配到盘上。盘可以是单片，多片或分段结构。在分段结构中，金属键槽段还用作将盘段连接在一起的连接。还将覆盖用于将片段安装到盘的方法。

3. 发明授权

US3860138A Cargo container latch and door 失效
标题翻译：货物集装箱和门
公开(公告)号：US3860138A
公开(公告)日：1975-01-14
申请号：US43080374
申请日：1974-01-04
申请人： GOODYEAR AEROSPACE CORP
发明人： LOVICH JOHN W , MELLER OSCAR W , MORSE FRANK C
IPC分类号： B65D88/12 , B65D6/40 , B65D88/14 , B65D90/00 , B65D87/00
CPC分类号： B65D88/14 , B65D90/008
摘要： The invention relates to cargo containers and more particularly, to door and latch assemblies therefore. The invention comprises a dutch door having separate and independent upper and lower door portions interconnected by a unique latch-hinge assembly. The latch-hinge assembly allows the upper door to be disengaged from the lower door, rotated about an upper hinge, and be stored atop the cargo container on a slide thereon which engages with a track extruded in the upper door. The upper and lower doors may, as a unit, be opened by the folding of the lower door onto the upper door about the latch-hinge assembly and a subsequent storage of the two doors atop the cargo container may then be achieved by means of the slide-track engagement.
摘要翻译：本发明涉及货物集装箱，更具体地涉及门和闩锁组件。本发明包括一个具有独立且独立的上和下门部分的独立的闩锁铰链组合的荷叶门。闩锁 - 铰链组件允许上部门从下部门分离，围绕上部铰链旋转，并且被存储在货物集装箱顶部的滑动件上，该滑动件与在上部门中挤出的轨道接合。作为一个单元，上门和下门可以通过围绕闩锁铰链组件将下门折叠到上门上来打开，然后可以通过以下方式实现货物集装箱上方的两个门的后续存放滑轨参与。

4. 发明授权

US3743213A Guided missiles 失效
标题翻译：指导的MISSILES
公开(公告)号：US3743213A
公开(公告)日：1973-07-03
申请号：US27246452
申请日：1952-02-19
申请人： GOODYEAR AEROSPACE CORP
发明人： SUCHNER D
IPC分类号： F42B15/10 , F42B15/36 , F42B15/02 , F42B15/00 , F42B15/18
CPC分类号： F42B15/105 , F42B10/666 , F42B15/36
摘要： 3. In combination, an airframe having a fuselage and wings, a jet motor detachably mounted on the fuselage in substantially parallel relation thereto, the airframe having one center of gravity with the motor mounted thereon and a second center of gravity with the motor detached therefrom, a booster rocket disposed within and substantially parallel with said fuselage, a pair of rocket supporting tracks having their upper surface below the rocket center and adapted to support the rocket in one position or in a second position wherein the rocket is turned 180* about its longitudinal axis, driving lugs extending diametrically and transversely from the front end of the rocket and resting on said tracks, thrust abutment means on the fuselage for said driving lugs, a pair of vertically extending lugs on the rocket near the rocket rear portion, means on the fuselage for sideways holding said vertical lugs, latch means for longitudinally holding the rocket in place, and a rearwardly extending exhaust nozzle on the rocket, said nozzle being canted from the longitudinal center line of the rocket so that the nozzle center line in one position passes through one of said centers of gravity and when the rocket is turned 180* about its longitudinal center line the nozzle center passes through the other one of said centers of gravity.
摘要翻译：组合在一起，具有机身和机翼的机身，以与其大致平行的方式可拆卸地安装在机身上的喷射马达，具有安装在其上的马达的一个重心的机身，以及马达从其上拆下的第二重心，设置在机身内并基本上平行于机身的助推火箭，一对火箭支撑轨道，其上表面在火箭中心下方，并适于将火箭支撑在一个位置或第二位置，其中火箭围绕其旋转180度纵向轴线，从火箭的前端沿径向和横向延伸并且搁置在所述轨道上的驱动凸耳，用于所述驱动凸耳的机身上的推力抵靠装置，靠近火箭后部的火箭上的一对垂直延伸的凸耳，用于横向保持所述垂直凸耳的机身，用于将火箭纵向保持在适当位置的闩锁装置，以及向后延伸的 g火箭上的排气喷嘴，所述喷嘴从火箭的纵向中心线倾斜，使得一个位置的喷嘴中心线穿过所述重心之一，并且当火箭绕其纵向中心线转动180°时喷嘴中心通过另一个所述重心。

5. 发明授权

US3742495A Drone guidance system and method 失效
标题翻译：指导系统和方法
公开(公告)号：US3742495A
公开(公告)日：1973-06-26
申请号：US3742495D
申请日：1971-09-24
申请人： GOODYEAR AEROSPACE CORP
发明人： DIAMANTIDES N
IPC分类号： G01S5/00 , G01S7/04 , G06E3/00 , G06F15/50
CPC分类号： G06E3/003 , G01S5/0009 , G01S7/04 , G05D1/0016
摘要： A drone aircraft is guided over a desired flight path wherein line map correlation provides x and y offsets from the desired fixed point. The x, y offset signals are used to drive the actuators of the drone''s control surfaces and also provide positional information to a monitored display at the control station.
摘要翻译：无人驾驶飞机被引导到期望的飞行路径上，其中线图相关性提供与期望的固定点的x和y偏移。 x，y偏移信号用于驱动无人机控制面的执行器，并向控制站的监视显示器提供位置信息。

6. 发明授权

US3708619A Automatic focusing of optical systems 失效
标题翻译：光系统的自动聚焦
公开(公告)号：US3708619A
公开(公告)日：1973-01-02
申请号：US3708619D
申请日：1970-10-15
申请人： GOODYEAR AEROSPACE CORP
发明人： MARTIN G
IPC分类号： G02B7/34 , G02B27/40 , G03B3/00
CPC分类号： G02B27/40 , G02B7/343
摘要： Disclosed is a means to automatically focus an optical system. An error signal derived by sensing the image parallax with respect to an output focal plane is employed to focus the optical system by shifting an appropriate optical element so that the image parallax error is minimized.
摘要翻译：公开了一种自动聚焦光学系统的手段。采用通过感测相对于输出焦平面的图像视差导出的误差信号来通过移动适当的光学元件来聚焦光学系统，使得图像视差误差最小化。

7. 发明授权

US3681781A Storing and retrieval method 失效
标题翻译：存储和检索方法
公开(公告)号：US3681781A
公开(公告)日：1972-08-01
申请号：US3681781D
申请日：1970-09-04
申请人： GOODYEAR AEROSPACE CORP
发明人： BATCHER KENNETH E
IPC分类号： G06F17/30 , G06F9/00 , G06F15/34
CPC分类号： G06F17/30949
摘要： The invention relates to a technique for utilizing a general purpose computer controlled by an algorithm to store items from a multi-dimensional space in a store in such a way that retrieval of all items within a given tolerance of a search point can be effected rapidly. Basically, it is the use of unique algorithms in coordinating the function of the general purpose computer and correlator that enable the rapid processing to be achieved. In effect, it is a between limits hashing operation.
摘要翻译：本发明涉及一种用于利用由算法控制的通用计算机的技术，以便以这样的方式存储来自存储器中的多维空间的项目，使得可以快速地实现对搜索点的给定容限内的所有项目的检索。基本上，使用独特的算法来协调通用计算机和相关器的功能，从而实现快速处理。实际上，这是一个限制散列操作之间。

8. 发明授权

US3620486A Autostable circular tethered wing balloon 失效
标题翻译：自动圆形四边形气球
公开(公告)号：US3620486A
公开(公告)日：1971-11-16
申请号：US3620486D
申请日：1969-07-09
申请人： GOODYEAR AEROSPACE CORP
发明人： CHARPENTIER JEAN F , ROSS ROBERT S
IPC分类号： B64B1/40 , B64B1/50
CPC分类号： B64B1/40
摘要： This invention relates to an axisymmetrical-shaped, tethered wing balloon which is substantially autostable in the wind field and, particularly, to a wing balloon which, without performing any rotational motion, is able to keep relatively to the wind direction, a permanent consistent attitude irrespective of changes in wind velocity.

9. 发明授权

US3618073A Synchro angle converter 失效
标题翻译：同步角度转换器
公开(公告)号：US3618073A
公开(公告)日：1971-11-02
申请号：US3618073D
申请日：1970-03-23
申请人： GOODYEAR AEROSPACE CORP
发明人： DOMCHICK STEPHEN J , THOMAS HOWARD M
IPC分类号： H03M1/00 , H03K13/02
CPC分类号： H03M1/645
摘要： A synchro converter demodulates the stator signals, selects stator signal relationships indicative of a rotor-to-stator angular sector through logic switching, converts the selected signals in analog form to digital equivalents, and digitally processes the resultant signals to obtain an output representative of the synchro rotor-to-stator angular position.

10. 发明授权

US3569977A Hexagram antenna 失效
标题翻译： HEXAGRAM天线
公开(公告)号：US3569977A
公开(公告)日：1971-03-09
申请号：US3569977D
申请日：1968-12-26
申请人： GOODYEAR AEROSPACE CORP
发明人： KOLLER WILLIAM B
IPC分类号： H01Q11/08 , H01Q1/36 , H01Q1/48
CPC分类号： H01Q11/08
摘要： Two triangular radiating elements are interlaced in a helical winding about a common axis to form a single antenna structure. The elements are wound in opposite directions and are laterally separated, thus reducing the RF coupling between them and improving the circularity of each radiating pattern with one radiating element wound in one direction and the other in the opposite direction, a dual circularity is achieved from the same physical volume.

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