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1.发明授权Dual-string dynamometer for measuring dental handpiece power at high speed and low torque 失效双弦测力计，用于在高速和低扭矩下测量牙科手机功率公开(公告)号：US07997131B2
公开(公告)日：2011-08-16
申请号：US12750778
申请日：2010-03-31
IPC分类号： G01L5/04
摘要： A dual-string tension dynamometer (1) utilizes two strings (10, 11) wrapped around approximately ninety degrees of a test wheel (12). The lateral forces (E, F) are balanced such that the total lateral force net value is zero. The results reflect purely torsional loading.
摘要翻译： 双弦张力测力计（1）利用围绕大约九十度的测试轮（12）缠绕的两根绳（10,11）。 横向力（E，F）是平衡的，使得总横向力净值为零。 结果反映纯粹的扭转载荷。
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2.发明申请Dual-string dynamometer for measuring dental handpiece power at high speed and low torque 审中-公开双弦测力计，用于在高速和低扭矩下测量牙科手机功率公开(公告)号：US20050103102A1
公开(公告)日：2005-05-19
申请号：US11022092
申请日：2004-12-22
申请人： Eugene Novak , Tom Papanek , Tadeusz Parafinczuk , Todd Fanciullo
发明人： Eugene Novak , Tom Papanek , Tadeusz Parafinczuk , Todd Fanciullo
摘要： A dual-string tension dynamometer (1) utilizes two strings (10, 11) wrapped around approximately ninety degrees of a test wheel (12). The lateral forces (E, F) are balanced such that the total lateral force net value is zero. The results reflect purely torsional loading.
摘要翻译： 双弦张力测力计（1）利用围绕大约九十度的测试轮（12）缠绕的两根绳（10,11）。 横向力（E，F）是平衡的，使得总横向力净值为零。 结果反映纯粹的扭转载荷。
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公开(公告)号：US20060253230A1
公开(公告)日：2006-11-09
申请号：US11120827
申请日：2005-05-03
申请人： Todd Fanciullo , Phillip Gold
发明人： Todd Fanciullo , Phillip Gold
IPC分类号： G06F17/00
CPC分类号： G05D1/0202 , G05D1/0808
摘要： A static longitudinal stability (SLS) system provides an unobtrusive airspeed hold function that reacts to the pilot control inputs into the flight control system and the measured states of the aircraft to engage and disengage smoothly without any explicit mode selection by the pilot. The SLS engages airspeed hold when the aircraft is close to trimmed, non-accelerating state. This logic allows the pilot to either fly close to a desired airspeed and let SLS engage, or trim the aircraft in an accelerating/decelerating maneuver and just wait for the SLS to capture a speed when longitudinal acceleration is small. The SLS is not dependant on the pilot specifically selecting this mode, but rather engages and disengages in response to flight control system status and how the aircraft is being maneuvered.
摘要翻译： 静态纵向稳定性（SLS）系统提供了一种不引人注意的空速保持功能，其对飞行控制系统的飞行员控制输入和飞行器的测量状态进行平滑地接合和分离，而飞行员没有任何明确的模式选择。 当飞机接近修剪，非加速状态时，SLS接合空速保持。 该逻辑允许飞行员飞行接近所需的空速，并使SLS接合，或者在加速/减速操作中修整飞行器，并且只需等待SLS在纵向加速度小时捕获速度。 SLS不依赖于具体选择该模式的飞行员，而是根据飞行控制系统状态和飞机如何被操纵而进行接合和脱离。
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