首页> 外国专利> Improvements in Gyroscopically Controlled Torpedoes and Launching-tubes therefor.

Improvements in Gyroscopically Controlled Torpedoes and Launching-tubes therefor.

机译:陀螺控制鱼雷及其发射管的改进。

摘要

17,895. Crucible Steel Co., [Assignees of Shonnard, H. W.]. April 3, [Convention date]. Gyroscopic apparatus. -Relates to automobile torpedoes provided with power - operated, e.g. electric, gyroscopes of the kind in which the spinning of the gyroscope is effected while the gyroscope is locked, the unlocking being under the control of the operator and taking place when the launching-tube is accurately trained on the target as described in Specification 11,459/12; the gyroscope motor is contained within the torpedo. According to the present invention, the passage of current through the electricmotor gyroscope is controlled by means of a movable or sliding member capable of establishing or disestablishing electric connexions directly with conductors on the electric - motor gyroscope. The sliding member may also lock and unlock the gyroscope. In the construction shown in Figs. 3 and 5, a gyroscope of any known type, e.g. as described in Specification 101,225 is employed, comprising a three-phase alternating-current induction motor, in which the stator 1 is the motor inductor and the rotor 4, 5 is the gyroscope fly-wheel. By means of a spider 2 the stator 1 is secured to a housing 3 forming the inner gimbal; the rotor is mounted in bearings, 6, 6a; and the housing 3 is exhausted of air by means of a check valve 75. Current is led to the stator through three conductors 7, which are connected to contacts 8. The locking and unlocking of the gyroscope, and the making and breaking of the circuit, is effected by a single sliding member 10 carrying the locking-pin 13 and three spring-actuated conducting-rods 14 which are connected, by flexible conductors, binding-posts, busbars, &c. to three contacts in a disk 26 removably secured by a watertight joint to the torpedo shell. Springs 27 tend to move the slide 10 rearwards, to break the circuit and unlock the gyroscope, and by means of toothed gearing 29, 30 actuated by means of a shaft 28 and the usual angular wrench-cup, the slide is moved forwards. A spring detent 32 retains the slide in the forward position, the detent being withdrawn by mechanism 34, 35, 36 and a tripping- finger 37 in a recess in the torpedo shell. The finger 37 may be tripped by the initial movement of the torpedo in the tube, or by special means, such as a catch 40 and an electromagnet 38, 39, operated before launching. In a modification, the sliding member 10 is pasitivaly moved in both directions, and the conducting- rods 14 are not spring-actuated. The rearward movement of the slide is produced by means of a tripping-finger, corresponding to the finger 37, connected by links to a shaft geared to the slide, while the forward movement is produced from a shaft, corresponding to the shaft 28, connected by bevel-gearing to the shaft which is geared to the slide. The mechanism for completing the circuit from an outside source of supply through the launching-tube to the contacts 25 is described in Specification 17,897/15, and comprises a casing 41 on the launching-tube fitted with a spring-pressed piston 42 having three contact-rods 44 to which the conductors of a multiple cable 49 are attached. The piston may be moved outwards, to break the circuit, by means of handles 50, or by compressed air admitted through the conduit 51 before, or simultaneously with, the launching of the torpedo. A spring catch 54 retains the piston in the outward position. In the construction shown in Fig. 1, the means for controlling the spinning of the gyroscope and the launching of the torpedo are controlled by the sighting officer. The director 55 is adjusted, in known manner, to close an electric circuit when the target being sighted arrives at a predetermined point, and, in the construction shown, the circuit is utilized to control the admission of air to launch the torpedo and to unlock the gyroscope. The usual storage reservoir 58 is mounted on the tube 57 and communicates therewith by a valve 59 operated by a rod 60, bell-crank lever 61, and spring-actuated rod 62. A projection 63 on the lever 61 engages a lever 64 connected to the armature 65 of an electro-magnet 66. The conduit 51 is connected to the passage from the reservoir 58 to the tube 57. A switch 69 is provided to control the circuits 67, 68 for spinning the gyroscope. The electro-magnets 38 and 66 are placed in series and are provided with current from the supply conductor 67. The gyroscope may thus be spun at any time by operating the switch 67, and the torpedo is launched and the gyroscope unlocked when the director 55 closes the circuit 70 ,71, 71a.
机译:17,895。 Crucible Steel Co。,[Shhonard,H.W。的受让人]。 [公约日期] 4月3日。陀螺仪。 -与配备动力的汽车鱼雷有关-例如电动陀螺仪,在陀螺仪锁定时进行陀螺仪旋转,解锁是在操作员的控制下进行的,并且如规范11459 / 12;鱼雷内装有陀螺仪马达。根据本发明,电流通过电动陀螺仪的通过是通过可动或滑动构件来控制的,该可动或滑动构件能够直接与电动陀螺仪上的导体建立或消除电连接。滑动构件还可锁定和解锁陀螺仪。在图1和图2所示的结构中。参照图3和图5,任何已知类型的陀螺仪,例如陀螺仪。如在规格101,225中所描述的那样,其使用包括三相交流感应电动机,其中定子1是电动机电感器,转子4、5是陀螺仪飞轮。定子1通过星形轮2固定到形成内部万向接头的壳体3上;定子3固定在壳体3上。转子安装在轴承6、6 中;外壳3通过单向阀75排出空气。电流通过连接到触点8的三个导体7流向定子。陀螺仪的锁定和解锁以及电路的接通和断开通过一个带有锁定销13的单滑动件10和三个由弹簧操纵的导电杆14来实现图3所示的滑动,该导电杆通过柔性导体,接线柱,母线等连接。圆盘26中的三个触点通过水密接头可移动地固定到鱼雷壳上。弹簧27趋于使滑块10向后移动,以断开电路并使陀螺仪解锁,并且借助于由轴28和通常的角形扳手杯致动的齿轮装置29、30,滑块向前移动。弹簧止动件32将滑动件保持在向前位置,该止动件由机构34、35、36和脱扣指状物37收回在鱼雷壳的凹部中。指状物37可通过鱼雷在管中的初始运动或通过在发射之前操作的特殊装置(例如卡扣40和电磁体38、39)而被绊倒。在一个变型中,滑动构件10沿两个方向临时移动,并且导电杆14不被弹簧致动。滑块的向后运动是通过一个与手指37相对应的脱扣手指产生的,该手指通过连杆连接到与滑块相联的轴上,而向前的运动是由一个与轴28相对应的轴产生的通过斜齿轮连接到与滑动装置相连的轴上。在规格17,897 / 15中描述了用于完成从外部电源通过发射管到触点25的电路的机构,该机构包括在发射管上的壳体41,该壳体上装有具有三个触点的弹簧活塞42 -多根电缆49的导体附接到其上的杆44。在发射鱼雷之前或同时,可以通过手柄50或通过导管51吸入的压缩空气使活塞向外移动,以中断回路。弹簧扣54将活塞保持在向外位置。在图1所示的结构中,用于控制陀螺仪旋转和鱼雷发射的装置由瞄准人员控制。导向器55以已知的方式被调节以在被瞄准的目标到达预定点时闭合电路,并且在所示的结构中,该电路用于控制空气的进入以发射鱼雷并解锁陀螺仪。普通的储存容器58安装在管57上,并通过由杆60,曲柄杆61和弹簧致动的杆62操作的阀59与管59连通。杆61上的突出部63接合连接至与之连接的杆64。导管51连接到从容器58到管57的通道。提供开关69以控制用于旋转陀螺仪的电路67、68。电磁体38和66串联放置并从供电导体67提供电流。因此,陀螺仪可以在任何时候通过操作开关67旋转,并且当导向器55时,鱼雷被发射并且陀螺仪被解锁。闭合电路70、71、71

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