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1. 发明授权

US5826821A Drag control module for range correction of a spin stabil 失效
标题翻译：拖动控制模块进行自旋稳定的范围校正
公开(公告)号：US5826821A
公开(公告)日：1998-10-27
申请号：US912970
申请日：1997-08-04
申请人： Fred J. Brandon , Michael S. L. Hollis
发明人： Fred J. Brandon , Michael S. L. Hollis
IPC分类号： F42B10/50
CPC分类号： F42B10/50
摘要： A range correction module which is designed to fit onto a spin stabilized llistic projectile for correcting range error. The range correction module is a self-contained module within the fuze which screws into the forward portion of the projectile. The range correction module is designed such that changes are not required to the existing projectile. During the course correction phase, sixteen semi-circular plates will deploy from the module. The plates create a blunt cross-sectional area in front of the projectile, thus creating more drag and effectively slowing the projectile.
摘要翻译：一种距离校正模块，其设计用于适应自旋稳定的弹道射弹，用于校正距离误差。范围校正模块是引信中的独立模块，螺钉进入射弹的前部。范围校正模块的设计使得现有弹丸不需要进行更改。在校正阶段期间，将从模块部署十六个半圆形板。这些平板在射弹前面形成钝的横截面，从而产生更大的阻力并有效地使射弹减速。

2. 发明授权

US5762291A Drag control module for stabilized projectiles 失效
标题翻译：拖动控制模块，用于稳定的射弹
公开(公告)号：US5762291A
公开(公告)日：1998-06-09
申请号：US924515
申请日：1997-09-05
申请人： Michael S. L. Hollis , Fred J. Brandon
发明人： Michael S. L. Hollis , Fred J. Brandon
IPC分类号： F42B10/50 , F42B10/00
CPC分类号： F42B10/50
摘要： A trajectory (range) control device which is designed to fit behind the f of a fin stabilized ballistic projectile for correcting range error. The trajectory (range) control device is a self-contained, add-on module, which will screw into the forward portion of the projectile. The fuze will then screw into the trajectory (range) control module, which has a small through hole that will coincide with the center of the fuze and the center of the projectile. This through hole is intended to provide a channel in which the fuze can detonate the intended booster charge which will in turn ignite the high explosive payload or function the payload of the fin stabilized ballistic projectile. The trajectory control device will not make changes to the existing projectile or fuze. During the course correction phase, eight spring loaded flare tabs will deploy from the device. The flare tabs create a blunt cross-sectional area in front of the projectile, thus creating more drag and effectively slowing the projectile.
摘要翻译：一种轨迹（范围）控制装置，其设计用于配合用于校正射程误差的翅片稳定弹道射弹的引信。轨迹（范围）控制装置是一个独立的附加模块，它将拧入射弹的前部。然后，引信将拧入轨迹（范围）控制模块，该模块具有与引信中心和射弹中心重合的小通孔。该通孔旨在提供一种通道，其中引信可以引爆预期的增压装置，这将进而点燃高爆炸物有效载荷或起作用的翅片稳定的弹道射弹的有效载荷。轨迹控制装置不会改变现有的弹丸或引信。在校正阶段期间，将从设备部署八个弹簧加载的火炬片。火炬片在射弹前面形成一个钝的横截面，从而产生更大的阻力并有效地减慢了射弹的速度。

3. 发明授权

US5501155A Hollow training round 失效
标题翻译：空心训练
公开(公告)号：US5501155A
公开(公告)日：1996-03-26
申请号：US327770
申请日：1994-10-24
申请人： Michael S. L. Hollis , Fred J. Brandon , Edward W. Kennedy , Edward M. Schmidt
发明人： Michael S. L. Hollis , Fred J. Brandon , Edward W. Kennedy , Edward M. Schmidt
IPC分类号： F42B8/12 , F42B10/06
CPC分类号： F42B8/12 , F42B10/06
摘要： A fin stabilized kinetic energy tank training device comprising a project having a nose and having nose and end sections, and constructed of a low density material such as aluminum, and having a hollowed-out section to further reduce weight thereof, so as to minimizing penetration of an armor system on impact thereon.
摘要翻译：一种翅片稳定动能罐训练装置，包括具有鼻部并具有鼻部和端部的弹丸，并由诸如铝的低密度材料构成，并且具有中空部分以进一步减轻其重量，从而最小化穿透的装甲系统。

4. 发明授权

US06347764B1 Gun hardened, rotary winged, glide and descent device 失效
标题翻译：枪硬化，旋转翼，下滑和下降装置
公开(公告)号：US06347764B1
公开(公告)日：2002-02-19
申请号：US09710736
申请日：2000-11-13
申请人： Fred J. Brandon , Michael S. L. Hollis
发明人： Fred J. Brandon , Michael S. L. Hollis
IPC分类号： B64C2708
CPC分类号： F42B10/58
摘要： A payload carrying device which is inserted into a remote area of interest by means of a projectile carrier to obtain data, or the like, from the remote area. The device has counter rotating main blades as well as tail blades carried on a tail rotor. The particular payload is carried in a canister which may also include a power source, a command and control unit and a motor, if hover or lateral flight is desired. The pitch of the tail blades is variable as well as their orientation around an axis, the combination of which generates a thrust vector in a particular direction for controlled lateral flight.
摘要翻译：一种有效载荷承载装置，其通过射弹载体从远程区域插入到感兴趣的偏远地区以获得数据等。该装置具有相对旋转的主叶片以及承载在尾部转子上的尾叶。如果需要悬停或侧向飞行，特定有效载荷被携带在罐中，其也可以包括电源，命令和控制单元以及电动机。尾翼的桨距是可变的，并且它们围绕轴线的方向是可变的，其组合在特定方向上产生用于受控横向飞行的推力矢量。

5. 发明授权

US5816531A Range correction module for a spin stabilized projectile 失效
标题翻译：旋转稳定弹丸的范围校正模块
公开(公告)号：US5816531A
公开(公告)日：1998-10-06
申请号：US794789
申请日：1997-02-04
申请人： Michael S. L. Hollis , Fred J. Brandon
发明人： Michael S. L. Hollis , Fred J. Brandon
IPC分类号： F42B10/50 , F42B10/34
CPC分类号： F42B10/50
摘要： A range correction module which is designed to fit onto a spin stabilized ballistic projectile for correcting range error. The range correction module is a self-contained module within the fuze which screws into the forward portion of the projectile. The range correction module is designed such that changes are not required to the existing projectile. During the course correction phase, semi-circular plates will deploy from the module. The plates create a blunt cross-sectional area in front of the projectile, thus creating more drag and effectively slowing the projectile.
摘要翻译：一种距离校正模块，其设计用于适应自旋稳定的弹道射弹，用于校正距离误差。范围校正模块是引信中的独立模块，螺钉进入射弹的前部。范围校正模块的设计使得现有弹丸不需要进行更改。在校正阶段期间，半圆形板将从模块部署。这些平板在射弹前面形成钝的横截面，从而产生更大的阻力并有效地使射弹减速。

6. 发明授权

US5363766A Remjet powered, armor piercing, high explosive projectile 失效
标题翻译： Remjet动力，穿甲穿甲，高爆炸弹药
公开(公告)号：US5363766A
公开(公告)日：1994-11-15
申请号：US489932
申请日：1990-02-08
申请人： Fred J. Brandon , Miles L. Lampson , Fred I. Grace
发明人： Fred J. Brandon , Miles L. Lampson , Fred I. Grace
IPC分类号： F42B12/10 , F42B10/34
CPC分类号： F42B12/10
摘要： An armor piercing projectile having a ramjet engine located at the forwardnd such that the exhaust nozzles of the ramjet engine are located at or near the center of gravity of the projectile. A warhead is contained in the center portion of the projectile and is either a shaped charge device or a high explosive warhead. A tail boom with stabilizing fins is located at the rear of the projectile. In an alternate embodiment, the ramjet engine is attached by an extension sleeve to the warhead allowing it to telescope after launch and provide increased standoff for better penetration by the shaped charge. Another embodiment allows the ramjet motor to detach prior to impact at the target to better allow the warhead to penetrate. A further embodiment incorporates an armor piercing subprojectile located within the centerbody of the ramjet motor.
摘要翻译：具有位于前端的冲压喷气发动机的穿甲射弹，使得冲压式喷气发动机的排气喷嘴位于或接近射弹的重心。弹头包含在弹丸的中心部分，并且是成形装药装置或高爆炸弹头。具有稳定翅片的尾臂位于射弹的后部。在替代实施例中，冲压式喷气发动机通过延伸套筒连接到弹头，允许其在发射之后望远镜并且提供增加的间隙以通过成形电荷更好地穿透。另一个实施例允许冲压喷气发动机在撞击目标之前分离以更好地允许弹头穿透。另一实施例包括位于冲压式喷气发动机的中心体内的装甲穿刺子弹头。

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