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公开(公告)号:US20090060287A1
公开(公告)日:2009-03-05
申请号:US11899606
申请日:2007-09-05
Applicant: Roderick A. Hyde , Muriel Y. Ishikawa , Jordin Kare , Eric C. Leuthardt , Royce A. Levien , Lowell L. Wood, JR. , Victoria Y.H. Wood , Dennis J. Rivet
Inventor: Roderick A. Hyde , Muriel Y. Ishikawa , Jordin Kare , Eric C. Leuthardt , Royce A. Levien , Lowell L. Wood, JR. , Victoria Y.H. Wood , Dennis J. Rivet
IPC: G06K9/00
CPC classification number: A61B5/0002 , A61B5/082 , A61B5/1112 , A61B5/16 , A61B5/6898 , A61B5/7435 , G06K9/00885 , G06K2209/05
Abstract: A device is configured for one or more of communication transfer and audio/video playback. The device includes a sensing system for measuring a physiological condition through manipulation of an output of the device and analysis of a user response.
Abstract translation: 一个设备配置为通信传输和音频/视频播放中的一个或多个。 该装置包括用于通过操纵装置的输出和用户响应的分析来测量生理状况的感测系统。
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公开(公告)号:US20140182265A1
公开(公告)日:2014-07-03
申请号:US13733502
申请日:2013-01-03
Applicant: Jordin Kare
Inventor: Jordin Kare
IPC: F02K1/28
CPC classification number: F02K9/44
Abstract: In an aspect of the invention, a system for rocket propulsion includes a heater operable to generate thermal energy from energy supplied from a non-chemical energy source, and to supply the thermal energy to a non-cryogenic fuel to thermally decompose the fuel into components that include at least a first component and a second component. The rocket propulsion system also includes a combustion chamber and a nozzle. The combustion chamber is operable to receive an oxidizer and at least a portion of the thermally decomposed fuel, and allow the two to combust. The nozzle generates thrust by directing the products of the combustion out of the system.
Abstract translation: 在本发明的一个方面,一种用于火箭推进的系统包括可操作以从由非化学能源供应的能量产生热能的加热器,以及将热能提供给非低温燃料以将燃料热分解成部件 其包括至少第一组分和第二组分。 火箭推进系统还包括燃烧室和喷嘴。 燃烧室可操作以接收氧化剂和至少一部分热分解燃料,并允许两者燃烧。 喷嘴通过将燃烧产物引导出系统来产生推力。
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公开(公告)号:US20130199155A1
公开(公告)日:2013-08-08
申请号:US13733100
申请日:2013-01-03
Applicant: Jordin Kare
Inventor: Jordin Kare
IPC: F02K9/00
Abstract: In an aspect of the invention, a system for rocket propulsion includes a heater operable to generate thermal energy from energy supplied from a non-chemical energy source, and to supply the thermal energy to a non-cryogenic fuel to thermally decompose the fuel into components that include at least a first component and a second component. The rocket propulsion system also includes a combustion chamber and a nozzle. The combustion chamber is operable to receive an oxidizer and at least a portion of the thermally decomposed fuel, and allow the two to combust. The nozzle generates thrust by directing the products of the combustion out of the system.
Abstract translation: 在本发明的一个方面,一种用于火箭推进的系统包括可操作以从由非化学能源供应的能量产生热能的加热器,以及将热能提供给非低温燃料以将燃料热分解成部件 其包括至少第一组分和第二组分。 火箭推进系统还包括燃烧室和喷嘴。 燃烧室可操作以接收氧化剂和至少一部分热分解燃料,并允许两者燃烧。 喷嘴通过将燃烧产物引导出系统来产生推力。
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公开(公告)号:US20130130067A2
公开(公告)日:2013-05-23
申请号:US12589323
申请日:2009-10-20
Applicant: Geoffrey Deane , Bran Ferren , William Gates , W. Daniel Hillis , Roderick Hyde , Muriel Ishikawa , Edward Jung , Jordin Kare , Nathan Myhrvold , Clarence Tegreene , David Tuckerman , Thomas Weaver , Charles Whitmer , Lowell Wood, Jr. , Victoria Wood
Inventor: Geoffrey Deane , Bran Ferren , William Gates , W. Daniel Hillis , Roderick Hyde , Muriel Ishikawa , Edward Jung , Jordin Kare , Nathan Myhrvold , Clarence Tegreene , David Tuckerman , Thomas Weaver , Charles Whitmer , Lowell Wood, Jr. , Victoria Wood
CPC classification number: H01M4/02 , H01M4/36 , H01M4/366 , H01M10/44 , H01M10/613 , H01M10/617 , H01M10/654 , H01M10/6567 , H01M2004/021 , Y10T29/49108
Abstract: An electrochemical device (such as a battery) includes at least one electrode having a fluid surface, which may employ a surface energy effect to maintain a position of the fluid surface and/or to modulate flow within the fluid. Fluid-directing structures may also modulate flow or retain fluid in a predetermined pattern. An electrolyte within the device may also include an ion-transport fluid, for example infiltrated into a porous solid support.
Abstract translation: 电化学装置(例如电池)包括具有流体表面的至少一个电极,其可以采用表面能量效应来维持流体表面的位置和/或调节流体内的流动。 流体引导结构还可以以预定模式调节流动或保持流体。 装置内的电解质还可以包括离子输送流体,例如渗透到多孔固体支持物中。
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