公开(公告)号：US20100258672A1

公开(公告)日：2010-10-14

申请号：US11502453

申请日：2006-08-11

Applicant: Michael Grabmeier ,  Dieter Fasol

Inventor： Michael Grabmeier ,  Dieter Fasol

IPC: B64C7/00

CPC classification number: B64D1/04 ,  B64C39/024

Abstract: An aircraft, particularly an unmanned aircraft, has at least one weapons bay. At least one standardized equipment container can be inserted into the weapons bay.

Abstract translation: 一架飞机，特别是一架无人飞机，至少有一个武器舱。 至少一个标准化的设备容器可以插入武器舱。

公开(公告)号：US20080105112A1

公开(公告)日：2008-05-08

申请号：US11766343

申请日：2007-06-21

Applicant: Michael Grabmeier

Inventor： Michael Grabmeier

IPC: B64D1/12

CPC classification number: B64D1/12 ,  B64C2201/206

Abstract: A device for launching unmanned missiles from an aircraft with a pallet, on which at least one container is provided to receive a missile. The container has an upper container section that has a pylori for the suspended, detachable support of the missile. The container has a lower container section that is embodied as a support area for the missile.

Abstract translation: 用于从具有托盘的飞机发射无人导弹的装置，其上提供至少一个容器以接收导弹。 容器具有上部容器部分，其具有用于导弹的悬挂的可分离支撑件的幽门。 容器具有较低的容器部分，其被实施为导弹的支撑区域。

公开(公告)号：US08371535B2

公开(公告)日：2013-02-12

申请号：US12508793

申请日：2009-07-24

Applicant: Michael Grabmeier ,  Christine Stumpp

Inventor： Michael Grabmeier ,  Christine Stumpp

IPC: B64C13/02

CPC classification number: F41F3/0406 ,  B64D1/12 ,  B64D5/00 ,  F41G7/007

Abstract: Unmanned missile and method for releasing the unmanned missile from a carrier aircraft, in which the missile has an autonomous flight control device that acts on control devices of the missile. The method includes adjusting vertical rudders and elevators of the missile into a neutral position in which a respective rudder angle is 0°, separating electrical and mechanical connections between the missile and the carrier aircraft, and detecting, via sensors of the missile, that the separating has occurred. The method also includes activating the autonomous flight control device and automatically controlling the missile with the flight control device and the control devices based upon correction flight condition variables caused by a prevailing downwash between the missile and the carrier aircraft, and automatically controlling the missile with the flight control device and the control devices based on data stored in at least one storage device on the missile.

Abstract translation: 无人驾驶导弹和从载具飞机上释放无人导弹的方法，其中导弹具有作用于导弹的控制装置的自主飞行控制装置。 该方法包括将导弹的垂直方向舵和电梯调整到相应的舵角为0°的中立位置，分离导弹和载具飞机之间的电气和机械连接，以及通过导弹的传感器检测分离 已经发生了。 该方法还包括激活自主飞行控制装置，并根据飞弹控制装置和控制装置自动控制导弹，基于由导弹和载具飞机之间的主流下冲引起的校正飞行情况变量，并自动控制导弹 飞行控制装置和控制装置基于存储在导弹上的至少一个存储装置中的数据。

公开(公告)号：US20080035785A1

公开(公告)日：2008-02-14

申请号：US11705536

申请日：2007-02-13

Applicant: Michael Grabmeier

Inventor： Michael Grabmeier

IPC: F41G9/00

CPC classification number: F41G7/007 ,  F41G7/346

Abstract: An unmanned missile which may be uncoupled from a preferably propelled aircraft has a navigation and control device which has a receiver for position determination signals. The receiver is electrically connected to a first antenna, and receives signals collected by the first antenna and transmits same as position determination signals to the navigation and control device. The missile has an electrical signal input by which the missile is connected to the aircraft until it is uncoupled from the aircraft, and by which the missile is supplied with signals for position determination. The missile is provided with at least one additional antenna which is also electrically connected to the receiver.

Abstract translation: 可以从优选的推进飞机脱离的无人驾驶导弹具有导航和控制装置，其具有用于位置确定信号的接收器。 接收机电连接到第一天线，并且接收由第一天线收集的信号并将其作为位置确定信号发送到导航和控制装置。 导弹具有电信号输入，导弹连接到飞机，直到飞行器与飞机脱离，并且向导弹提供信号以进行位置确定。 该导弹设置有至少一个另外的天线，该天线也与接收器电连接。

公开(公告)号：US08387920B2

公开(公告)日：2013-03-05

申请号：US13034369

申请日：2011-02-24

Applicant: Michael Grabmeier

Inventor： Michael Grabmeier

IPC: B64D1/12

CPC classification number: B64D1/12 ,  B64C2201/206

Abstract: A device for launching unmanned missiles from an aircraft with a pallet, on which at least one container is provided to receive a missile. The container has an upper container section that has a pylon for the suspended, detachable support of the missile. The container has a lower container section that is embodied as a support area for the missile.

Abstract translation: 用于从具有托盘的飞机发射无人导弹的装置，其上提供至少一个容器以接收导弹。 容器具有一个上部容器部分，该部分具有用于导弹悬挂的可拆卸支撑件的塔架。 容器具有较低的容器部分，其被实施为导弹的支撑区域。

公开(公告)号：US07960675B2

公开(公告)日：2011-06-14

申请号：US11705536

申请日：2007-02-13

Applicant: Michael Grabmeier

Inventor： Michael Grabmeier

IPC: F41G7/00 ,  F42B15/01 ,  F42B15/00 ,  G06G7/80

CPC classification number: F41G7/007 ,  F41G7/346

Abstract: An unmanned missile which may be uncoupled from a preferably propelled aircraft has a navigation and control device which has a receiver for position determination signals. The receiver is electrically connected to a first antenna, and receives signals collected by the first antenna and transmits same as position determination signals to the navigation and control device. The missile has an electrical signal input by which the missile is connected to the aircraft until it is uncoupled from the aircraft, and by which the missile is supplied with signals for position determination. The missile is provided with at least one additional antenna which is also electrically connected to the receiver.

Abstract translation: 可以从优选的推进飞机脱离的无人驾驶导弹具有导航和控制装置，其具有用于位置确定信号的接收器。 接收机电连接到第一天线，并且接收由第一天线收集的信号并将其作为位置确定信号发送到导航和控制装置。 导弹具有电信号输入，导弹连接到飞机，直到飞行器与飞机脱离，并且向导弹提供信号以进行位置确定。 该导弹设置有至少一个另外的天线，该天线也与接收器电连接。

公开(公告)号：US07926764B2

公开(公告)日：2011-04-19

申请号：US11766343

申请日：2007-06-21

Applicant: Michael Grabmeier

Inventor： Michael Grabmeier

IPC: B64D1/12

CPC classification number: B64D1/12 ,  B64C2201/206

Abstract: A device for launching unmanned missiles from an aircraft with a pallet, on which at least one container is provided to receive a missile. The container has an upper container section that has a pylon for the suspended, detachable support of the missile. The container has a lower container section that is embodied as a support area for the missile.

Abstract translation: 用于从具有托盘的飞机发射无人导弹的装置，其上提供至少一个容器以接收导弹。 容器具有一个上部容器部分，该部分具有用于导弹悬挂的可拆卸支撑件的挂钩。 容器具有较低的容器部分，其被实施为导弹的支撑区域。