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1.发明申请公开(公告)号：US20050269454A1
公开(公告)日：2005-12-08
申请号：US11037125
申请日：2005-01-19
CPC分类号： F42B10/46 , F42B12/105
摘要： It is an object of the present invention to provide a flying object using a thin elongated nose cone with a small tip angle for reducing the air resistance during flying, wherein the maximum loading capacity can be increased without decreasing the volume efficiency of the flying object by limitations placed on the accommodation space, regardless of the structure thereof. In the flying object in accordance with the present invention, which comprises a nose cone in the tip portion, the nose cone portion has a compressed structure in the axial direction during accommodation and expands on the tip side in the axial direction during flying, due to an expandable nose cone structure such that a disk with a small diameter is disposed in the forward position and the disks with a successively increasing diameter are disposed in the axial direction. After separation, the nose cone expands in the axial direction, deep cavities are formed between the disks, and a fine elongated nose cone with a small tip angle is provided, whereby the air resistance is reduced.
摘要翻译： 本发明的目的是提供一种飞行物体，其使用具有小尖角的细长鼻锥，以减少飞行期间的空气阻力，其中可以增加最大承载能力，而不会降低飞行物体的体积效率 不管其结构如何，对住宿空间的限制。 在根据本发明的飞行物体中，其包括尖端部分中的鼻锥，鼻锥部在调节期间在轴向方向上具有压缩结构，并且在飞行期间在轴向方向上的尖端侧膨胀，由于 可扩展的鼻锥结构，使得具有小直径的盘被设置在向前位置，并且具有连续增加的直径的盘沿轴向设置。 分离后，鼻锥在轴向上膨胀，在圆盘之间形成深空腔，并提供具有小尖角的细长鼻锥，由此减小空气阻力。
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公开(公告)号：US07322179B2
公开(公告)日：2008-01-29
申请号：US10759014
申请日：2004-01-20
CPC分类号： F02C7/042 , B64D33/02 , B64D2033/026 , F05D2220/80 , F05D2250/141 , F05D2250/90 , Y10T137/0645
摘要： An air intake includes a spike and a cylindrical cowl. The spike is composed of a plurality of plates which are arranged axial symmetrically around a central axis thereof, and the cowl includes an inner wall parallel to the central axis and is formed so as to enclose a rear portion of the spike via a given space. The adjacent ones of the plates form respective aerodynamic compressive surfaces in spaces formed by the adjacent ones. The distances between the adjacent ones of the plates are variable, and the distance between the forefront of the spike along the central axis and the cowl is variable.
摘要翻译： 进气口包括一个钉和一个圆柱形的整流罩。 尖钉由围绕其中心轴线对称布置的多个板组成，并且整流罩包括平行于中心轴线的内壁，并且形成为经由给定空间包围尖峰的后部。 相邻的板在由相邻板形成的空间中形成相应的空气动力学压缩表面。 相邻板之间的距离是可变的，并且沿着中心轴和整流罩的尖峰的最前沿之间的距离是可变的。
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3.发明授权公开(公告)号：US07118072B2
公开(公告)日：2006-10-10
申请号：US11037125
申请日：2005-01-19
IPC分类号： B64C1/38
CPC分类号： F42B10/46 , F42B12/105
摘要： It is an object of the present invention to provide a flying object using a thin elongated nose cone with a small tip angle for reducing the air resistance during flying, wherein the maximum loading capacity can be increased without decreasing the volume efficiency of the flying object by limitations placed on the accommodation space, regardless of the structure thereof.In the flying object in accordance with the present invention, which comprises a nose cone in the tip portion, the nose cone portion has a compressed structure in the axial direction during accommodation and expands on the tip side in the axial direction during flying, due to an expandable nose cone structure such that a disk with a small diameter is disposed in the forward position and the disks with a successively increasing diameter are disposed in the axial direction. After separation, the nose cone expands in the axial direction, deep cavities are formed between the disks, and a fine elongated nose cone with a small tip angle is provided, whereby the air resistance is reduced.
摘要翻译： 本发明的目的是提供一种飞行物体，其使用具有小尖角的细长鼻锥，以减少飞行期间的空气阻力，其中可以增加最大承载能力，而不会降低飞行物体的体积效率 不管其结构如何，对住宿空间的限制。 在根据本发明的飞行物体中，其包括尖端部分中的鼻锥，鼻锥部在调节期间在轴向方向上具有压缩结构，并且在飞行期间在轴向方向上的尖端侧膨胀，由于 可扩展的鼻锥结构，使得具有小直径的盘被设置在向前位置，并且具有连续增加的直径的盘沿轴向设置。 分离后，鼻锥在轴向上膨胀，在圆盘之间形成深空腔，并提供具有小尖角的细长鼻锥，由此减小空气阻力。
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