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公开(公告)号：US20050146160A1
公开(公告)日：2005-07-07
申请号：US11013942
申请日：2004-12-15
Applicant: Michael Beauchamp
Inventor： Michael Beauchamp
Abstract: A large utility sport passenger van featuring the passenger side sliding door, bottom mounted scuff plate, truck wheel wells, conical hood dash and windshield, all-terrain tires, occupant safety features, capable of high-speed performance, off-road, rough-terrain transport, low, high or level angle 360 degree picture-taking, surveillance-maneuvering, on-the-fly pick-up, and rescue.
Abstract translation: 一个大型实用运动客车，包括乘客侧滑动门，底部安装的刮板，卡车车轮井道，锥形罩仪表板和挡风玻璃，全地形轮胎，乘员安全功能，能够高速性能，越野， 地形运输，低，高或水平角度360度摄影，监视机动，即时接送和救援。
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公开(公告)号：US20070059171A1
公开(公告)日：2007-03-15
申请号：US11505462
申请日：2006-08-17
Applicant: Mark Simms , Michael Beauchamp
Inventor： Mark Simms , Michael Beauchamp
IPC: F01D5/18
CPC classification number: F01D5/18 , B22C9/10 , F05D2230/21 , F05D2240/81
Abstract: A method of forming a turbine nozzle guide vane 2 for a gas turbine engine, the guide vane 2 comprising an internal cavity 14 and having internal features 16, comprises investment casting metal around a core member 30 that defines the internal cavity 14 and internal features 16 of the guide vane, removing the core member 30, and machining the guide vane 2. The process of investment casting around the core member 30 includes the step of casting at least one feature 40 external to the guide vane 2. The external feature 40 is used as a reference point to indicate the location of the internal features 16 of the guide vane 2 during the machining of the guide vane 2.
Abstract translation: 一种形成用于燃气涡轮发动机的涡轮喷嘴引导叶片2的方法，包括内部空腔14并且具有内部特征16的导向叶片2包括围绕限定内部空腔14的芯构件30和内部特征16的熔模铸造金属 的导叶，去除芯构件30，并且对导向叶片2进行加工。 围绕芯构件30的熔模铸造的过程包括将导向叶片2外部的至少一个特征部40铸造的步骤。 外部特征40用作参考点，以指示在引导叶片2的加工期间导向叶片2的内部特征16的位置。
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公开(公告)号：US20050077429A1
公开(公告)日：2005-04-14
申请号：US10645044
申请日：2003-08-18
Applicant: Michael Beauchamp
Inventor： Michael Beauchamp
CPC classification number: B64D25/10 , B64D2201/00
Abstract: An aircraft occupancy, here a helicopter with a seat chassis mounted on a set of rails of any type, ideally as I have demonstrated on load bearing triple monorails with one hundred sixty-eight circumventing roller trucks attached to the inner rails, an outer track box movable along the inner tracks, and a monorail supporting track with eighty-four roller trucks. Shown here in a side view with partial delineation of the mesh end cover Any seat chassis attached to the outer track box is ejectable along a lateral trajectory, perpendicular to the horizontal longitudinal axis of an aircraft, and guided out of the path of a failed aircraft during ejection flight by two bottom positioned tail fins slotted within the ejection monorails launcher platform legs. The seat chassis is enabled to eject laterally since a conventional hinged door is operational within a greater sliding door panel which pneumatic rockets at the top and bottom of the sliding door transverse the greater emergency sliding door panel including the interior fixed conventional hinge operational door out of the path of the seat chassis or chassis', attached to the outer track box towards the rear of the aircraft where the sliding greater panel is prevented from recoiling by a common latch catches. Dual airbags for positioning the legs and torso of an occupant for a safe emergency exit ejection are embedded or attached to the structure directly fore of the seat chassis. A second set of airbags, head, neck and chest protector are connected on both sides of the seat chassis, mandatory for safe lateral equal access emergency exit ejection. Three compartments for altitude appropriate parachutes and sensor fuse box for opening said desired chute. Including an interior side mounted blast shield and monorails inner tracks support to which a couple of rocket catapults are fixed by seals at their ignition points, holding the outer track box and seat chassis stationary between the inner tracks and supporting track.
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