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公开(公告)号：US20060266204A1
公开(公告)日：2006-11-30
申请号：US11371541
申请日：2006-03-08
申请人： Richard Givens , Jerome Klein , Thomas Burky , James Reuther
发明人： Richard Givens , Jerome Klein , Thomas Burky , James Reuther
摘要： The present invention provides for cutting operations using linear thermite charges; the charges cut one dimensional or two dimensional geometric shapes; the invention is useful for structure entry or demolition.
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公开(公告)号：US20050126420A1
公开(公告)日：2005-06-16
申请号：US10938199
申请日：2004-09-10
申请人： Richard Givens , Michael Fisher , Thomas Burky , Jerome Klein , Graham Alexander , Jason Paugh
发明人： Richard Givens , Michael Fisher , Thomas Burky , Jerome Klein , Graham Alexander , Jason Paugh
摘要： Wall breaching apparatus and methods utilizing shaped charges for penetration of walls of buildings and other structures for rescue, escape, or military operations.
摘要翻译： 墙体破坏装置和方法利用成形装置对建筑物和其他结构的墙壁进行穿透以进行救援，逃生或军事行动。
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公开(公告)号：US09405295B2
公开(公告)日：2016-08-02
申请号：US12518361
申请日：2007-12-11
申请人： Alvaro Vitor Polati De Souza , Fabricio Reis Caldeira , Dagfinn Gangsaas , Jerome Klein , Lauro Rocha Borges , Reneu Luiz Andrioli, Jr. , Luciano Tury Pastorini , Marco Paulo Fonseca
发明人： Alvaro Vitor Polati De Souza , Fabricio Reis Caldeira , Dagfinn Gangsaas , Jerome Klein , Lauro Rocha Borges , Reneu Luiz Andrioli, Jr. , Luciano Tury Pastorini , Marco Paulo Fonseca
CPC分类号： G05D1/0676 , G05D1/08 , G05D1/0808
摘要： A flight control system commands drag devices such as flight spoilers according to pilot or autopilot longitudinal command. Furthermore, the flight control system monitors a set of flight parameters to determine whether the aircraft is operating inside the permitted safe envelope, hence, incorporating envelope automatic exceeding disengagement. This invention allows the aircraft to descend in a steeper glide path than the 3° used in the normal approach, while keeping speeds unchanged.
摘要翻译： 飞行控制系统根据飞行员或自动驾驶仪纵向命令来命令拖动装置，例如飞行扰流板。 此外，飞行控制系统监视一组飞行参数，以确定飞行器是否在允许的安全信封内操作，因此，将信封自动超出分离。 本发明允许飞行器以比正常进近中使用的3°更陡的滑行路径下降，同时保持速度不变。
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公开(公告)号：US20060140605A1
公开(公告)日：2006-06-29
申请号：US11286645
申请日：2005-11-25
申请人： Jerome Klein
发明人： Jerome Klein
IPC分类号： G03B17/00
CPC分类号： G03B17/14
摘要： A method and apparatus that allows a ring to be inserted into the primary devices lens element or adapter without changing the offset (i.e., the distance between the camera and the lens along the optical path). This can be at the ocular or recording end of lenses. The ring can be hand turned and gently tightened with a key similar to a spanner wrench. The ring will maintain it's place and location when the amount of pressure applied to the accessory is less then that applied to the ring. When the insertion ring is in place, the screw mount diameter of the primary device is smaller without adding additional unnecessary offset when mounting the accessory. The present application covers the usage, design and manufacture of insertion rings, insertion ring keys and any modifications to the primary device.
摘要翻译： 一种允许环在不改变偏移（即，照相机和透镜沿着光路的距离）的情况下将环插入主要装置透镜元件或适配器中的方法和装置。 这可以在镜头的眼睛或记录端。 手环可以手动转动并用类似扳手的扳手轻轻地拧紧。 当施加到附件的压力的量小于施加到环上时，环将保持其位置和位置。 当插入环就位时，主装置的螺丝安装直径较小，而在安装附件时不增加额外的不必要的偏移。 本申请涉及插入环，插入环键的使用，设计和制造以及对主要装置的任何修改。
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公开(公告)号：US20100217460A1
公开(公告)日：2010-08-26
申请号：US12518361
申请日：2007-12-11
申请人： Alvaro Vitor Polati De Souza , Fabricio Reis Caldeira , Dagfinn Gangsaas , Jerome Klein , Lauro Rocha Borges , Reneu Luiz Andrioli, JR. , Luciano Tury Pastorini , Marco Paulo Fonseca
发明人： Alvaro Vitor Polati De Souza , Fabricio Reis Caldeira , Dagfinn Gangsaas , Jerome Klein , Lauro Rocha Borges , Reneu Luiz Andrioli, JR. , Luciano Tury Pastorini , Marco Paulo Fonseca
CPC分类号： G05D1/0676 , G05D1/08 , G05D1/0808
摘要： A flight control system commands drag devices such as flight spoilers according to pilot or autopilot longitudinal command. Furthermore, the flight control system monitors a set of flight parameters to determine whether the aircraft is operating inside the permitted safe envelope, hence, incorporating envelope automatic exceeding disengagement. This invention allows the aircraft to descend in a steeper glide path than the 3° used in the normal approach, while keeping speeds unchanged.
摘要翻译： 飞行控制系统根据飞行员或自动驾驶仪纵向命令来命令拖动装置，例如飞行扰流板。 此外，飞行控制系统监视一组飞行参数，以确定飞行器是否在允许的安全信封内操作，因此，将信封自动超出分离。 本发明允许飞行器以比正常进近中使用的3°更陡的滑行路径下降，同时保持速度不变。
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