公开(公告)号：US5050477A

公开(公告)日：1991-09-24

申请号：US742079

申请日：1985-03-19

申请人： Roy L. Cowdery ,  James W. Schofield

发明人： Roy L. Cowdery ,  James W. Schofield

IPC分类号： B64D7/08

CPC分类号： B64D7/08

摘要： A helicopter includes missile storage means (29) adapted to store a plurality of missiles (26) laterally within a fuselage (28) and missile launcher means (40) located at the end of a lateral outrigger (27) for pivotal movement about a generally vertical axis (42) between a loading position generally laterally of the fuselage and a launch position generally parallel with a longitudinal centreline of the fuselage. In the illustrated embodiment, the launcher means comprises an elongated support beam (45) for selective engagement by a longitudinally extending tubular member (32) attached to each missile and includes transfer means (51, 52, 60, 61) for transferring a missile between the storage means and the launcher means when the latter is in said loading position.

摘要翻译： 直升机包括适于在机身（28）内横向存储多个导弹（26）的导弹存储装置（29）和位于外部支腿（27）的端部处的导弹发射装置（40），用于围绕一般的 在机身的大致横向的加载位置与大致平行于机身的纵向中心线的发射位置之间的垂直轴线（42）。 在所示实施例中，发射器装置包括细长的支撑梁（45），用于通过附接到每个导弹的纵向延伸的管状构件（32）进行选择性接合，并且包括用于在两个导弹之间传送导弹的传送装置（51,52,60,61） 当后者处于所述装载位置时，存储装置和发射器装置。

公开(公告)号：US4785710A

公开(公告)日：1988-11-22

申请号：US887532

申请日：1986-07-21

申请人： James W. Schofield

发明人： James W. Schofield

IPC分类号： B64C27/04 ,  F41A9/04 ,  F41F3/06 ,  F41F3/04

CPC分类号： B64D7/08 ,  F41A9/04 ,  F41F3/06 ,  B64C27/04

摘要： A helicopter (10) has a fuselage (11) provided with storage means (19, 20, 24) for storing a plurality of missiles (16) longitudinally of the fuselage, reloadable turret means (17) beneath the fuselage for movement in azimuth and elevation and transfer means (20b, 21) for transferring a missile from the storage means to the turret means. In the illustrated embodiment the missiles are stored externally of generally vertical side walls (13) and a lower generally horizontal wall (14) of the fuselage and fairings (39) are provided to protect the externally mounted missiles.

摘要翻译： 直升机（10）具有机身（11），其具有存储装置（19,20,24），用于在机身的纵向上存储多个导弹（16），机身下方的可重新加载的转塔装置（17）用于在方位角上移动， 用于将导弹从存储装置传送到转台装置的高度和转移装置（20b，21）。 在所示实施例中，导弹存储在大体上垂直的侧壁（13）的外部，机身和整流罩（39）的下部大致水平的壁（14）被设置以保护外部安装的导弹。

公开(公告)号：US4151234A

公开(公告)日：1979-04-24

申请号：US793417

申请日：1977-05-03

申请人： James W. Schofield

发明人： James W. Schofield

IPC分类号： C01B17/02 ,  B01J2/06

CPC分类号： C01B17/0237

摘要： A process for producing solid, irregular shaped sulfur nuggets from molten sulfur. The process includes the steps of: gravity flowing molten sulfur at a temperature preferably in the range of about 240.degree.-270.degree. F. to a distributor head positioned closely above or below the surface of a cooling liquid; discharging the molten sulfur from the distributor head in ribbon-shaped streams into a cooling liquid, preferably water, having a temperature in the range of about 170.degree.-190.degree. F.; passing the molten sulfur streams through the cooling liquid until the streams are subdivided and thereafter solidified into nuggets of irregular shape and size; and removing the solid sulfur nuggets from the cooling liquid. The apparatus in which the process is carried out includes a feed system having temperature control apparatus for maintaining the sulfur in a molten state, a reservoir tank for the cooling liquid, a distributor head having elongated discharge slots for flowing the molten sulfur in ribbon-shaped streams into the cooling liquid, and apparatus such as a conveyor belt in the reservoir tank under the distributor head for collecting and removing the solid sulfur nuggets from the cooling liquid.

摘要翻译： 从熔融硫生产固体，不规则形状的硫磺块的方法。 该方法包括以下步骤：将熔融硫在优选在约240°至270°F的温度范围内重力流入位于冷却液表面附近的分配器头; 将熔融的硫从带状流中的分配器头排出到具有约170°-190°范围内的温度的冷却液，优选水中; 使熔融的硫流通过冷却液，直到流被细分，然后固化成不规则形状和大小的矿块; 并从冷却液中除去固体硫块。 进行该过程的装置包括具有用于将硫保持在熔融状态的温度控制装置的进料系统，用于冷却液体的储存罐，分配器头部，其具有用于使熔融硫在带形状 流入冷却液，以及在分配器头下方的储存罐中的传送带等装置，用于从冷却液中收集和除去固体硫块。