会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 77. 发明授权
    • Device and method for generating light of a predetermined spectrum with at least four differently colored light sources
    • 用至少四种不同颜色的光源产生预定光谱的光的装置和方法
    • US09565723B2
    • 2017-02-07
    • US13972254
    • 2013-08-21
    • EADS Deutschland GmbH
    • Mario CappitelliSönke KlostermannDietmar VogtMichael Olbert
    • H05B33/08
    • H05B33/08H05B33/0851H05B33/0866H05B33/0869H05B37/0227
    • A lighting device and method with a lighting unit which includes several light sources having different color spectra, with a sensor for determining the spectral power distribution emitted by the lighting unit, with a control unit which, as a function of a predetermined spectral power distribution as well as of the spectral power distribution measured by the sensor, acts on a drive unit which individually energizes the light sources of the lighting unit, so that the emitted light has predetermined spectral power distribution, wherein the lighting unit includes at least four light sources, and the control unit uses an optimization algorithm which, as an optimization goal, maximizes a coefficient of weighted sensor values, the coefficient being calculable from individual drive data of the light sources. A secondary condition is met when error between the predetermined spectral power distribution and the measured spectral power distribution is smaller than a limit value.
    • 一种具有照明单元的照明装置和方法,该照明装置包括具有不同颜色光谱的多个光源,具有用于确定由照明单元发射的光谱功率分布的传感器,其具有作为预定光谱功率分布的函数的控制单元 以及由传感器测量的光谱功率分布,作用在单独激发照明单元的光源的驱动单元上,使得发射的光具有预定的光谱功率分布,其中照明单元包括至少四个光源, 并且控制单元使用优化算法,作为优化目标,最大化加权传感器值的系数,该系数可从光源的各个驱动数据计算。 当预定光谱功率分布和测量光谱功率分布之间的误差小于极限值时,满足次要条件。
    • 79. 发明授权
    • Aircraft fuselage structure
    • 飞机机身结构
    • US09487285B2
    • 2016-11-08
    • US14225562
    • 2014-03-26
    • Airbus Operations GmbHEADS Deutschland GmbH
    • Robert Alexander GoehlichAlexander GahnKai FinkAlexei Vichniakov
    • B64C1/18B64C1/06
    • B64C1/061B64C1/18
    • Provided is an aircraft fuselage structure having an outer skin, a support structure arrangement comprising a multiplicity of frame elements and a floor structure arrangement having a multiplicity of floor support struts. The aircraft fuselage structure provides a connection between the floor structure arrangement and the support structure arrangement which is as simple and quick to produce as possible, while not significantly increasing the weight or weakening the structure. Either the floor structure arrangement or the support structure arrangement can have at a connection there between a male connector element or a female connector element. The male connector element can have a peg which extends in the engagement direction and which has a circumferential outer surface which is provided with a multiplicity of circumferential projections. The female connector element can have a cavity, the inner surface of which is provided with a multiplicity of circumferential tabs.
    • 本发明提供一种具有外皮的飞行器机身结构,包括多个框架元件的支撑结构布置和具有多个地板支撑支柱的地板结构布置。 飞机机身结构提供地板结构布置和支撑结构布置之间的连接,其尽可能简单且快速地生产,同时不显着增加重量或减弱结构。 地板结构布置或支撑结构布置可以在阳连接器元件或阴连接器元件之间具有连接。 阳连接器元件可以具有沿接合方向延伸的钉,并且具有周向外表面,该周向外表面设置有多个周向突起。 阴连接器元件可以具有空腔,其内表面设置有多个周向突出部。