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    • 2. 发明授权
    • Content injection system and methodology
    • 内容注入系统和方法
    • US08381244B2
    • 2013-02-19
    • US11985143
    • 2007-11-13
    • Michael J. KingJohn W. Morris, IVBrian S. Bosworth
    • Michael J. KingJohn W. Morris, IVBrian S. Bosworth
    • H04N7/10H04N7/025
    • H04N21/23H04H20/103H04H20/24H04H60/06H04H60/76H04N21/23406H04N21/23424H04N21/812
    • A method, and an associated system, for sending to a first group of recipients only the content portions of a continuity source data-flow which takes the form of ordered, successive, alternating content and non-content segments. From a methodologic point of view, the invention involves, in a manner which utilizes content-segment material buffering, delivering fully, and in correct order, to the first recipient group the material in each content segment, via steps including (a) bridging each gap between next-adjacent content segments at least partially with transmitted injection material that differs from the non-content segment material in the gap, which injection material ends in time no sooner than the end of the gap, and (b) employing, as needed, and as a part of such full delivering of content-segment material, time-progressive, time-length-variable buffering, and subsequent, progressive buffer-delivering, of any content-segment material which overlaps in time with the transmission of injection material.
    • 一种方法和相关联的系统,用于仅向第一组接收者发送采用有序,连续,交替的内容和非内容段的形式的连续性源数据流的内容部分。 从方法学的角度来看,本发明以利用内容段材料缓冲的方式涉及以下步骤:通过步骤包括(a)桥接每个内容片段材料缓冲,并以正确的顺序向第一接收者组递送每个内容片段中的材料 至少部分地与传输的注入材料之间的间隙,所述传输的注入材料与间隙中的非内容段材料不同,所述注入材料在时间结束之后不迟于所述间隙的末端,以及(b)根据需要应用 ,并且作为与注入材料的传输时间重叠的任何内容段材料的内容片段材料,时间渐进式,时间长度可变缓冲以及随后的渐进缓冲递送的一部分, 。
    • 3. 发明申请
    • Content injection system and methodology
    • 内容注入系统和方法
    • US20080120638A1
    • 2008-05-22
    • US11985143
    • 2007-11-13
    • Michael J. KingJohn W. MorrisBrian S. Bosworth
    • Michael J. KingJohn W. MorrisBrian S. Bosworth
    • H04N7/025
    • H04N21/23H04H20/103H04H20/24H04H60/06H04H60/76H04N21/23406H04N21/23424H04N21/812
    • A method, and an associated system, for sending to a first group of recipients only the content portions of a continuity source data-flow which takes the form of ordered, successive, alternating content and non-content segments. From a methodologic point of view, the invention involves, in a manner which utilizes content-segment material buffering, delivering fully, and in correct order, to the first recipient group the material in each content segment, via steps including (a) bridging each gap between next-adjacent content segments at least partially with transmitted injection material that differs from the non-content segment material in the gap, which injection material ends in time no sooner than the end of the gap, and (b) employing, as needed, and as a part of such full delivering of content-segment material, time-progressive, time-length-variable buffering, and subsequent, progressive buffer-delivering, of any content-segment material which overlaps in time with the transmission of injection material.
    • 一种方法和相关联的系统,用于仅向第一组接收者发送采用有序,连续,交替的内容和非内容段的形式的连续性源数据流的内容部分。 从方法学的角度来看,本发明以利用内容段材料缓冲的方式涉及以下步骤:通过步骤包括(a)桥接每个内容片段材料缓冲,并以正确的顺序向第一接收者组递送每个内容片段中的材料 至少部分地与传输的注入材料之间的间隙,所述传输的注入材料与间隙中的非内容段材料不同,所述注入材料在时间结束之后不迟于所述间隙的末端,以及(b)根据需要应用 ,并且作为与注入材料的传输时间重叠的任何内容段材料的内容片段材料,时间渐进式,时间长度可变缓冲以及随后的渐进缓冲递送的一部分, 。
    • 4. 发明授权
    • Helmet blastometer
    • 头盔炮
    • US08984664B2
    • 2015-03-24
    • US12499740
    • 2009-07-08
    • William C. MossMichael J. King
    • William C. MossMichael J. King
    • A42B3/04G01P15/00
    • A42B3/046
    • A helmet blastometer for characterizing the direction, speed, magnitude, and duration of a blast event to determine the likelihood of blast-induced traumatic brain injury (biTBI). Time of arrival (TOA) gage sensors are mounted on a rigid outer shell of the helmet each producing a TOA signal in response to a fast rising blast induced positive pressure change above a predetermined threshold. A receiver analyzes the positive pressure changes from the gages to determine direction, speed, and magnitude of a blast. Other TOA gauge sensors can be used to produce a TOA signal in response to a negative pressure change below a predetermined threshold. The positive and negative pressure change TOA signals are used to determine blast duration. A second set of internal contact pressure sensors is connected to an inner liner of the helmet to detect contact pressure on a user's head to determine if biTBI has been sustained.
    • 用于表征爆发事件的方向,速度,幅度和持续时间以确定爆炸诱发的创伤性脑损伤(biTBI)的可能性的头盔测孔计。 到达时间(TOA)量具传感器安装在头盔的刚性外壳上,每个产生一个TOA信号,以响应于高于预定阈值的快速升高的爆炸引起的正压力变化。 接收机分析来自量具的正压变化,以确定爆炸的方向,速度和幅度。 可以使用其他TOA量规传感器来响应于低于预定阈值的负压力变化产生TOA信号。 正负压变化TOA信号用于确定爆炸持续时间。 第二组内部接触压力传感器连接到头盔的内衬,以检测用户头部的接触压力,以确定biTBI是否已被维持。
    • 6. 发明授权
    • Extendable joined wing system for a fluid-born body
    • 用于流体出生体的可扩展连接翼系统
    • US06986481B2
    • 2006-01-17
    • US10698580
    • 2003-10-31
    • Jerome P. FanucciMichael J. KingDavid P. MaassPavel Bystricky
    • Jerome P. FanucciMichael J. KingDavid P. MaassPavel Bystricky
    • F42B10/12
    • B64C3/40B63B1/30B64C3/56B64C39/068Y02T50/14
    • An extendable wing system for a fluid-born body has a forward wing and an aft wing pivotably coupled together at a location outward of their wing roots. A linkage mechanism mounted on the body provides both pivoting of the wing roots about a pivot point and translation of the wing roots and their pivot points to extend the joined wings from a stowed position to a deployed position. Translation of the forward wing root pivot point allows the stowed wing system to occupy additional space toward the nose of the body, thereby allowing use of wings having a longer wingspan and greater aspect ratio. The linkage mechanism can also be used to incorporate flight control, such as roll and pitch control, directly into the wing system. In another embodiment, the wings can incorporate actuator elements on or within the wings to effect flight control by deformation of the wing structure.
    • 用于流体出身体的可延伸的翼系统具有前翼和后翼,它们在其翼根的外侧的位置处可枢转地联接在一起。 安装在主体上的连杆机构提供了机翼根部围绕枢轴点的枢转以及机翼根部及其枢转点的平移,以将结合的机翼从收起位置延伸到展开位置。 前翼根枢轴点的翻译允许收起的翼系统占据身体鼻部的额外空间,从而允许使用具有较长翼展和更大纵横比的翼。 连杆机构也可用于将飞行控制,如滚转和俯仰控制,直接融入机翼系统。 在另一个实施例中,翼可以将致动器元件结合在翼上或翅膀内,以通过翼结构的变形来实现飞行控制。