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81. 发明专利

JPH08159698A SPIN MISSILE 失效
公开(公告)号：JPH08159698A
公开(公告)日：1996-06-21
申请号：JP29955594
申请日：1994-12-02
申请人： MITSUBISHI ELECTRIC CORP
发明人： NAKANO EIICHI
IPC分类号： F42B10/04 , F42B10/26 , F42B10/64
摘要： PURPOSE: To provide a missile flying spinning longitudinally of a machine body capable of producing roll torque required for spinning the body with a small- sized and simplified structure. CONSTITUTION: In a spin missile 1, there are provided the trunk 2 of the missile 1, a steering wing 3 disposed peripherally of the trunk 2 and in front of the body, and a rear wing 5 disposed peripherally of the trunk 2 and having an anti-symmetrical cross section. The missile 1 flies spinning longitudinally of the body, and is turned by actuating the steering wing 3 only in a predetermined roll attitude angle. In a conventional technique, for obtaining roll torque for the spinning a large-sized wing is provided to produce the roll torque. The cross section of the rear wing 5 provided peripherally of the trunk 2 is made anti-symmetrical, and air pressure excerted on the rear wing 5 is unbalanced to produce the roll torque whereby air resistance of the missile is reduced and a flying distance is increased.

82. 发明专利

JPH05141899A LAUNCHING METHOD FOR LONG BULLET AND THE LONG BULLET 失效
公开(公告)号：JPH05141899A
公开(公告)日：1993-06-08
申请号：JP30490691
申请日：1991-11-20
申请人： JAPAN STEEL WORKS LTD
发明人： IKUTA KAZUNARI
IPC分类号： F41A1/04 , F42B10/26 , F42B10/40
摘要： PURPOSE:To accelerate a bullet core within a limiting speed by accelerating a bullet having an engine case containing fuel and the core in a gun to a limiting speed, and burning fuel out of the gun. CONSTITUTION:When a bullet 20 is charged in a gun, accelerated to about 2km/sec of a limiting speed in the gun, and then launched out of the gun, a bullet core 1 is allowed to largely forward project, and the core 1 is integrated with an engine case 10 by the engagement of a groove end 1Aa with a pawl 14. A low combustion propulsion gunpowder 13 is ignited, injection gas 40 is injected from an injection port 10c, and the bullet 20 itself is started to be additionally accelerated. Then, when propulsion gunpowders 12, 11 are sequentially ignited, the core 1 is accelerated to an ultrahigh speed (about 3km/sec as a time is elapsed. When the final propulsion gunpowder 11 is burned out, a pawl releasing unit 41 disposed at the rear of the pawl 14 is operated to damage the pawl 14. Thus, the core 1 is separated from the case 10 and gradually decelerated to collide with a target.

83. 发明专利

JPH05141898A LAUNCHING METHOD FOR LIQUID FUEL ROCKET BULLET AND THE LIQUID FUEL ROCKET BULLET 失效
公开(公告)号：JPH05141898A
公开(公告)日：1993-06-08
申请号：JP30490491
申请日：1991-11-20
申请人： JAPAN STEEL WORKS LTD
发明人： IKUTA KAZUNARI
IPC分类号： F41A1/04 , F42B10/26 , F42B10/40
摘要： PURPOSE:To launch a long bullet core with a structure having a relatively small diameter by using liquid fuel at an ultrahigh speed. CONSTITUTION:A method for launching a liquid fuel rocket bullet and the liquid fuel rocket bullet has the steps of rotating an engine case 1 on its own axis by injection gas obtained by burning liquid fuel 20 in the case 1, and adhering the fuel 20 to the inner wall 1A of the case 1.

84. 发明专利

JPH02161296A GUIDED MISSILE 失效
公开(公告)号：JPH02161296A
公开(公告)日：1990-06-21
申请号：JP31468288
申请日：1988-12-13
申请人： MITSUBISHI ELECTRIC CORP
发明人： KATAYAMA MASAYUKI
IPC分类号： F42B10/26 , F42B10/64 , F42B15/01
摘要： PURPOSE:To shorten a time required for controlling a rolling position at the time of banked turning by reducing an inertial moment of a part for controlling the rolling position by coupling a guide controller to a body via a bearing. CONSTITUTION:A guided missile is so composed to couple a guiding unit to a body 1 via a guide controller 4 having a front wing 3 of a steering wing and a driver 6 via a bearing 7 so that its rolling motion is free as to control the rolling position only by the guide controller 4. When the guided missile is turned, the rolling position for producing a maximum turning acceleration is controlled, but since the guide controller 4 is free with respect to the rolling motion with respect to the body 1, only the guide controller 4 can control the rolling position. Since the mass of the guide controller is smaller than the whole missile, its inertial moment is small that much. Accordingly, since a time required for controlling the rolling position is short, the delay of a control system can be reduced. As a result, the tracing characteristic for a target motion is improved to obtain higher aiming probability.

85. 实用新型

JPS632851U 失效
公开(公告)号：JPS632851U
公开(公告)日：1988-01-09
申请号：JP9855186
申请日：1986-06-24
IPC分类号： B64G1/40 , B64G1/26 , F02K9/80 , F02K9/97 , F42B10/26 , F42B15/047

86. 发明专利

JPS6136159B2 失效
公开(公告)号：JPS6136159B2
公开(公告)日：1986-08-16
申请号：JP50223980
申请日：1980-09-25
申请人： ANDAASUSOON KAATO , BAATARUSUSOON NIRUSU , BONDESUSOON SUTEIGU
发明人： ANDAASUSOON KAATO , BAATARUSUSOON NIRUSU , BONDESUSOON SUTEIGU
IPC分类号： F42B10/14 , F42B10/16 , F42B10/26

87. 发明专利

JPS527200A PROJECTILE SHOOTING ASSEMBLY 失效
公开(公告)号：JPS527200A
公开(公告)日：1977-01-20
申请号：JP7797376
申请日：1976-07-02
申请人： EUROP PROPULSION
发明人： EMIIRU SUTOUFU
IPC分类号： F41F3/04 , F41A1/08 , F42B5/05 , F42B5/10 , F42B10/26 , F41F3/00 , F42B13/28 , F42B15/00

88. 发明公开

KR1020160109295A 이탈피를 가지는 탄두 조립체를 포함하는 지능형 탄두 无效
标题翻译： SMART WARHEAD HAVING WARHEAD ASSEMBLY WITH SABOT
公开(公告)号：KR1020160109295A
公开(公告)日：2016-09-21
申请号：KR1020150033426
申请日：2015-03-10
申请人： 국방과학연구소
发明人： 최우천 , 김윤건 , 이효근 , 송호인 , 김인근 , 장쾌현
IPC分类号： F42B10/26 , F42B12/58 , F42B30/08
CPC分类号： F42B10/26 , F42B12/58 , F42B30/08
摘要： 본발명은지능형탄두에대한것으로, 표적을탐지하기위한센서를포함하는탄두및, 상기탄두와적어도하나의이탈피의결합체로구성되는탄두조립체와, 상기표적을탐지하여거리및 방위각을결정하고, 상기탐지된방위각및, 기설정된방출각에따라상기탄두조립체를회전시켜방출하는플랫폼조립체와, 상기방출된상기탄두조립체가목표방출거리로의비행에필요한추진력및 상기탄두조립체의회전에필요한회전력을제공하는방출장치조립체를포함하며, 상기탄두조립체는, 상기탄두가, 상기적어도하나의이탈피에의해기 설정된일정각도만큼기울어진상태로상기탄두조립체에고정되는것을특징으로한다.
摘要翻译：本发明涉及智能弹头。智能弹头包括：一个弹头组件，包括一个弹头，弹头具有用于检测目标的传感器和弹头和至少一个炮弹的组件; 检测目标以确定距离和方位的平台组件，并且根据检测到的方位角和待排出的预设方位角来旋转弹头组件; 以及排出装置组件，其将排出弹头组件的飞行所需的推进力提供到目标排放距离并提供旋转弹头组件所需的旋转力。提供了弹头组件，其中弹头被固定到弹头组件，同时以预定角度倾斜至少一个炮弹。

89. 发明公开

KR1020120043828A 제트베인 분리식 발사체의 방향 조종 장치 有权
标题翻译：喷气机可拆卸的行驶控制机构
公开(公告)号：KR1020120043828A
公开(公告)日：2012-05-07
申请号：KR1020100105057
申请日：2010-10-27
申请人： 최용준
发明人： 최용준 , 이종수 , 김형호 , 김종호
IPC分类号： F42B10/38 , F42B10/26 , F42B10/66
CPC分类号： F42B10/665 , F42B10/64
摘要： PURPOSE: A direction control device of a jet vane-separable projectile is provided to simplify a whole power transmitting structure because a vane unit is rotated in a rotational direction of a jet vane-separable projectile by connecting a connection gear, a separation gear, and a driving gear. CONSTITUTION: A direction control device of a jet vane-separable projectile comprises a jet vane body, a control vane unit(40), a gear unit, a vane unit(60), a separable gear(74), a connecting gear(76), and a link unit. The jet vane body is coupled to one end of a cylindrical body unit. The control vane unit rotates around a rotary shaft(42) perpendicularly installed in the outer side of the jet vane body. The gear unit transmits the power of a motor(30) to the control vane unit. The vane unit rotates around a rotary shaft(62) perpendicularly installed inside of the jet vane body. A gear teeth(74a) of a separable gear is interlocked with a gear teeth(72a) of the driving gear. The connection gear is interlocked with a gear teeth(74b) of the other side of separable gear. One side of the link unit is joined to a rotary plate(44) extended to the side of the rotary shaft by a hinge. The other end of the link unit is connected to the rotary shaft of the connection gear, thereby rotating to an opposite direction.
摘要翻译：目的：提供一种喷射叶片可分离射弹的方向控制装置，以简化整个动力传递结构，因为叶片单元通过连接齿轮，分离齿轮和连接齿轮而沿着喷射叶片可分离射弹的旋转方向旋转一个驱动装置构成：喷射叶片可分离射弹的方向控制装置包括喷射叶片体，控制叶片单元（40），齿轮单元，叶片单元（60），可分离齿轮（74），连接齿轮（76））和链接单元。喷射叶片主体联接到圆柱体单元的一端。控制叶片单元围绕垂直安装在喷射叶片体的外侧的旋转轴（42）旋转。减速器将马达（30）的动力传递到控制叶片单元。叶片单元围绕垂直安装在喷射叶片主体内部的旋转轴（62）旋转。可分离齿轮的齿轮齿（74a）与驱动齿轮的齿轮齿（72a）互锁。连接齿轮与可分离齿轮的另一侧的齿轮齿（74b）互锁。连杆单元的一侧通过铰链连接到延伸到旋转轴侧的旋转板（44）。连杆单元的另一端连接到连接齿轮的旋转轴，从而沿相反方向旋转。

90. 发明授权

KR101885644B1 다목적 유탄 발사체 有权
公开(公告)号：KR101885644B1
公开(公告)日：2018-08-07
申请号：KR1020170059287
申请日：2017-05-12
申请人： 휴먼스화공(주)
发明人： 송민규
IPC分类号： F42B12/46 , F42B12/72 , F42B10/26
CPC分类号： F42B12/46 , F42B10/26 , F42B12/72
摘要： 본발명은일측끝면은막혀있으며, 타측끝면은열려있고, 상기일측끝면의중심부에격발뇌관이관통장착되어있는탄피; 및상기탄피에내장되며, 상기탄피의일측끝면의내측에채워진추진체의추진력으로상기탄피로부터분리되어일정거리비행하는탄체를포함하며, 상기탄체는, 상기추진체측과인접하게배치되고, 상기추진체로부터추진력을전달받아발화하는지연신관이장착되는분리본체를포함하는분리발사어셈블리와, 상기분리발사어셈블리가일정탄도를유지하면서회전하여비행하도록상기분리본체의외주면에형성되는날개부와, 상기분리발사어셈블리에결합되고, 일정기능을수행하는약제가일정형상으로성형된내부성형체를포함하는내통체와, 상기분리발사어셈블리에결합되어상기내통체를수용하며, 탄성변형을허용하는재질로이루어지는외통체를포함하는것을특징으로하여, 장비탄약의휴대상경량화구현이가능하며, 신속하게발사하기위한다기능복합효과를구현할수 있도록한 다목적유탄발사체에관한것이다.

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