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1. 发明授权

US09180977B2 Supplementary power supply apparatus for a vehicle, in particular a flying machine 有权
标题翻译：用于车辆的补充电源装置，特别是飞行器
公开(公告)号：US09180977B2
公开(公告)日：2015-11-10
申请号：US13464002
申请日：2012-05-04
申请人： Sten Gatzke
发明人： Sten Gatzke
IPC分类号： B64D41/00 , H01L31/05 , H01L31/042 , H02S40/36 , H02S10/40
CPC分类号： B64D41/00 , B64D2211/00 , H01L31/05 , H02S10/40 , H02S20/00 , H02S40/36 , Y02E10/50
摘要： A supplementary power supply apparatus for electric onboard consumers of a vehicle, in particular flying machines. The apparatus includes openly disposed visible solar surfaces of several solar cells that are arranged in areas on the surface of an outer skin of the vehicle or integrated in the latter in the manner of a layer. Each of the solar cells includes at least two electric terminals by means of which the solar cells may be interconnected to form a solar generator, and several ones of the electric terminals are configured as generator terminals of the solar generator for one or several predetermined voltages between two respective ones of these generator terminals.
摘要翻译：一种用于车辆的电动车载消费者的辅助电源装置，特别是飞行器。该装置包括布置在车辆外皮表面上的区域中的多个太阳能电池的露天可见的太阳能表面，或以一层的方式集成在其中。每个太阳能电池包括至少两个电端子，太阳能电池可以互连以形成太阳能发电机，并且几个电端子被配置为太阳能发电机的发生器端子，用于一个或多个预定电压这些发电机端子中的两个相应的。

2. 发明授权

US08342443B2 Wing-engine combination, an aircraft, and a wing section of an aircraft comprising an engine bleed-air duct arrangement 失效
标题翻译：翼型发动机组合，飞机和飞机的翼部，包括发动机排气管道装置
公开(公告)号：US08342443B2
公开(公告)日：2013-01-01
申请号：US12863495
申请日：2009-01-30
申请人： Sten Gatzke
发明人： Sten Gatzke
IPC分类号： B64D15/02
CPC分类号： B64D13/08 , B64D33/02 , B64D2013/0618 , F28D7/026 , F28D7/106 , Y02T50/56
摘要： A wing-engine combination includes: a wing with a main wing and an engine with a premixing chamber, a combustion chamber and a hot-air space, which includes: an engine bleed-air duct, which extends along the wingspan direction and along the leading edge of the main wing, including an engine bleed-air inlet device that is coupled to an engine hot-air space, and including an engine bleed-air outlet device having a discharge orifice on the main wing or a connecting part for coupling the engine bleed-air duct to a consumer of the engine bleed-air, an ambient-air duct, which extends along the engine bleed-air duct, including an ambient-air inlet device which is arranged on an aircraft component of the aircraft, which aircraft component faces the intended flow-around direction of the aircraft and includes an aperture for letting ambient air into the ambient-air duct, and including an ambient-air outlet device with a passage between the ambient-air duct and a premixing chamber of the engine so that the arrangement including the engine bleed-air duct and the ambient-air duct forms a heat exchanger device for cooling the air flowing in the engine bleed-air duct and so that the ambient air conveyed in the ambient-air duct is supplied for combustion in the engine; and an aircraft and a wing section of an aircraft including an engine bleed-air duct arrangement.
摘要翻译：翼型发动机组合包括：具有主翼的机翼和具有预混合室的发动机，燃烧室和热空气空间，其包括：沿着翼展方向延伸的发动机放气管道，主翼的前缘，包括联接到发动机热空气的发动机排气入口装置，并且包括在主翼上具有排放孔的发动机排气出口装置或连接部分，用于联接发动机排气管道发动机排气的使用者，沿着发动机排气管道延伸的环境空气管道，包括布置在飞行器的飞行器部件上的环境空气入口装置，其中飞行器部件面向飞行器的预期流动方向，并且包括用于使环境空气进入环境空气管道的孔，并且包括环境空气出口装置，该环境空气出口装置在环境空气管道和预混合室之间的通道引擎 o包括发动机排气管道和环境空气管道的布置形成用于冷却在发动机排气管道中流动的空气的热交换器装置，并且使得在环境空气管道中输送的环境空气被供应发动机燃烧; 以及包括发动机排气管道装置的飞行器和机翼部分。

3. 发明授权

US09318625B2 Supplementary power supply for vehicles, in particular aircraft 有权
标题翻译：车辆，特别是飞机的补充电源
公开(公告)号：US09318625B2
公开(公告)日：2016-04-19
申请号：US13536562
申请日：2012-06-28
申请人： Sten Gatzke
发明人： Sten Gatzke
IPC分类号： B60L1/00 , H01L31/02 , B64D41/00 , H02S10/40 , B60K16/00
CPC分类号： H01L31/02021 , B60K2016/003 , B64D41/00 , B64D2211/00 , H02S10/40 , Y02E10/50 , Y02T50/54
摘要： The invention relates to a supplementary power supply including a solar generator for ohmic consumers in a vehicle, in particular an aircraft, wherein a control circuit is electrically connected to a multiplicity of solar cells via generator terminals of the solar generator and includes at least one output terminal, and wherein the control circuit is configured to interconnect the at least one output terminal with the multiplicity of solar cells in accordance with an actual intensity of insolation of the solar cells such that a nominal voltage and/or a nominal current intensity is available at the at least one output terminal.
摘要翻译：本发明涉及一种辅助电源，其包括用于车辆中的欧姆消费者的太阳能发电机，特别是飞机，其中控制电路通过太阳能发电机的发电机端子电连接到多个太阳能电池，并且包括至少一个输出并且其中所述控制电路被配置为根据所述太阳能电池的日照的实际强度将所述至少一个输出端子与所述多个太阳能电池互连，使得在所述太阳能电池的额定电压和/或标称电流强度可用于所述至少一个输出端子。

4. 发明授权

US08745965B2 Flexible cable guide 失效
标题翻译：柔性电缆导轨
公开(公告)号：US08745965B2
公开(公告)日：2014-06-10
申请号：US13476189
申请日：2012-05-21
申请人： Detlef Tiegs , Sten Gatzke
发明人： Detlef Tiegs , Sten Gatzke
IPC分类号： F16G13/16
CPC分类号： F16G13/16
摘要： A flexible cable guide is provided that includes, but is not limited to a first chain link with a first longitudinal axis, a front region and a tubular first inner surface that extends in longitudinal direction, and a second chain link with a second longitudinal axis, a rear region and a tubular second inner surface that extends in longitudinal direction. The front region of the first chain link is connected to the rear region of the second chain link pivotably about a pivoting axis that extends perpendicular to the longitudinal axes of the chain links, such that it can be pivoted leftward and rightward referred to the first longitudinal axis up to a maximum pivoting angle.
摘要翻译：提供了柔性电缆引导件，其包括但不限于具有第一纵向轴线的第一链节，在纵向方向上延伸的前区域和管状第一内表面以及具有第二纵向轴线的第二链节，后部区域和沿纵向方向延伸的管状第二内表面。第一链节的前部区域围绕垂直于链节的纵向轴线延伸的枢转轴线可枢转地连接到第二链节的后部区域，使得其可以向左和向右枢转参考第一纵向轴至最大枢转角度。

5. 发明授权

US08967530B2 Signal strength dependent cover unlocking device for a duct housing a secondary power supply device in an aircraft fuselage 有权
标题翻译：信号强度相关的盖解锁装置，用于容纳飞机机身中的次级电源装置的管道
公开(公告)号：US08967530B2
公开(公告)日：2015-03-03
申请号：US13203055
申请日：2010-02-24
申请人： Sten Gatzke
发明人： Sten Gatzke
IPC分类号： B64D41/00 , F03D9/00
CPC分类号： F03D9/32 , B64D41/007 , B64D2241/00 , F03D1/04 , F03D9/00 , F03D9/25 , F03D17/00 , F05B2220/50 , F05B2240/921 , Y02E10/72
摘要： A power generation system for integration into an aircraft system, including a secondary power supply device having a generator turbine arranged in a duct running between a forward opening and a rearward opening on the fuselage of the aircraft. An electromagnetic unlocking device locks and unlocks a covering device on the forward opening, depending on a signal strength supplied to the unlocking device. The system also includes an actuation device that generates an opening or closing signal for an opening and closing device, and an opening function switching device that activates the unlocking device electrically with a signal strength that locks the covering device in an initial state, and on receipt of a power requirement signal from a power generation monitoring device, activates the unlocking device with a second signal strength that unlocks the covering device.
摘要翻译：一种用于集成到飞行器系统中的发电系统，包括具有发电机涡轮机的二次供电装置，发电机涡轮机布置在运行在飞行器的机身上的前开口和后开口之间的管道中。电磁解锁装置根据提供给解锁装置的信号强度来锁定和解锁正向开口上的覆盖装置。该系统还包括产生用于打开和关闭装置的打开或关闭信号的致动装置，以及打开功能切换装置，该打开功能切换装置利用在初始状态下锁定覆盖装置的信号强度以及接收时激活解锁装置来自发电监测装置的功率需求信号，以解锁覆盖装置的第二信号强度来激活解锁装置。

6. 发明申请

US20100288890A1 WING-ENGINE COMBINATION, AN AIRCRAFT, AND A WING SECTION OF AN AIRCRAFT COMPRISING AN ENGINE BLEED-AIR DUCT ARRANGEMENT 失效
标题翻译：发动机组合，飞机和包含发动机空气排水装置的飞机的一部分
公开(公告)号：US20100288890A1
公开(公告)日：2010-11-18
申请号：US12863495
申请日：2009-01-30
申请人： Sten Gatzke
发明人： Sten Gatzke
IPC分类号： B64D27/12 , F02C7/18 , B64D15/02 , B64D13/06 , B64C3/32
CPC分类号： B64D13/08 , B64D33/02 , B64D2013/0618 , F28D7/026 , F28D7/106 , Y02T50/56
摘要： A wing-engine combination includes: a wing with a main wing and an engine with a premixing chamber, a combustion chamber and a hot-air space, which includes: an engine bleed-air duct, which extends along the wingspan direction and along the leading edge of the main wing, including an engine bleed-air inlet device that is coupled to an engine hot-air space, and including an engine bleed-air outlet device having a discharge orifice on the main wing or a connecting part for coupling the engine bleed-air duct to a consumer of the engine bleed-air, an ambient-air duct, which extends along the engine bleed-air duct, including an ambient-air inlet device which is arranged on an aircraft component of the aircraft, which aircraft component faces the intended flow-around direction of the aircraft and includes an aperture for letting ambient air into the ambient-air duct, and including an ambient-air outlet device with a passage between the ambient-air duct and a premixing chamber of the engine so that the arrangement including the engine bleed-air duct and the ambient-air duct forms a heat exchanger device for cooling the air flowing in the engine bleed-air duct and so that the ambient air conveyed in the ambient-air duct is supplied for combustion in the engine; and an aircraft and a wing section of an aircraft including an engine bleed-air duct arrangement.
摘要翻译：翼型发动机组合包括：具有主翼的机翼和具有预混合室的发动机，燃烧室和热空气空间，其包括：沿着翼展方向延伸的发动机放气管道，主翼的前缘，包括联接到发动机热空气的发动机排气入口装置，并且包括在主翼上具有排放孔的发动机排气出口装置或连接部分，用于联接发动机排气管道发动机排气的使用者，沿着发动机排气管道延伸的环境空气管道，包括布置在飞行器的飞行器部件上的环境空气入口装置，其中飞行器部件面向飞行器的预期流动方向，并且包括用于使环境空气进入环境空气管道的孔，并且包括环境空气出口装置，该环境空气出口装置在环境空气管道和预混合室之间的通道引擎 o包括发动机排气管道和环境空气管道的布置形成用于冷却在发动机排气管道中流动的空气的热交换器装置，并且使得在环境空气管道中输送的环境空气被供应发动机燃烧; 以及包括发动机排气管道装置的飞行器和机翼部分。

7. 发明申请

US20130002015A1 SUPPLEMENTARY POWER SUPPLY FOR VEHICLES, IN PARTICULAR AIRCRAFT 有权
标题翻译：补充电动车，特别是飞机
公开(公告)号：US20130002015A1
公开(公告)日：2013-01-03
申请号：US13536562
申请日：2012-06-28
申请人： Sten Gatzke
发明人： Sten Gatzke
IPC分类号： B60L1/00
CPC分类号： H01L31/02021 , B60K2016/003 , B64D41/00 , B64D2211/00 , H02S10/40 , Y02E10/50 , Y02T50/54
摘要： The invention relates to a supplementary power supply including a solar generator for ohmic consumers in a vehicle, in particular an aircraft, wherein a control circuit is electrically connected to a multiplicity of solar cells via generator terminals of the solar generator and includes at least one output terminal, and wherein the control circuit is configured to interconnect the at least one output terminal with the multiplicity of solar cells in accordance with an actual intensity of insolation of the solar cells such that a nominal voltage and/or a nominal current intensity is available at the at least one output terminal.
摘要翻译：本发明涉及一种辅助电源，其包括用于车辆中的欧姆消费者的太阳能发电机，特别是飞机，其中控制电路通过太阳能发电机的发电机端子电连接到多个太阳能电池，并且包括至少一个输出并且其中所述控制电路被配置为根据所述太阳能电池的日照的实际强度将所述至少一个输出端子与所述多个太阳能电池互连，使得在所述太阳能电池的额定电压和/或标称电流强度可用于所述至少一个输出端子。

8. 发明申请

US20120318915A1 SUPPLEMENTARY POWER SUPPLY APPARATUS FOR A VEHICLE, IN PARTICULAR A FLYING MACHINE 有权
标题翻译：适用于特种飞机的车辆补充电源装置
公开(公告)号：US20120318915A1
公开(公告)日：2012-12-20
申请号：US13464002
申请日：2012-05-04
申请人： Sten Gatzke
发明人： Sten Gatzke
IPC分类号： H01L31/05 , B64D41/00
CPC分类号： B64D41/00 , B64D2211/00 , H01L31/05 , H02S10/40 , H02S20/00 , H02S40/36 , Y02E10/50
摘要： A supplementary power supply apparatus for electric onboard consumers of a vehicle, in particular flying machines. The apparatus includes openly disposed visible solar surfaces of several solar cells that are arranged in areas on the surface of an outer skin of the vehicle or integrated in the latter in the manner of a layer. Each of the solar cells includes at least two electric terminals by means of which the solar cells may be interconnected to form a solar generator, and several ones of the electric terminals are configured as generator terminals of the solar generator for one or several predetermined voltages between two respective ones of these generator terminals.
摘要翻译：一种用于车辆的电动车载消费者的辅助电源装置，特别是飞行器。该装置包括布置在车辆外皮表面上的区域中的多个太阳能电池的露天可见的太阳能表面，或以一层的方式集成在其中。每个太阳能电池包括至少两个电端子，太阳能电池可以互连以形成太阳能发电机，并且几个电端子被配置为太阳能发电机的发生器端子，用于一个或多个预定电压这些发电机端子中的两个相应的。

9. 发明申请

US20120006938A1 POWER GENERATING SYSTEM FOR INTEGRATION INTO AN AIRCRAFT SYSTEM 有权
标题翻译：用于集成到飞机系统中的发电系统
公开(公告)号：US20120006938A1
公开(公告)日：2012-01-12
申请号：US13203055
申请日：2010-02-24
申请人： Sten Gatzke
发明人： Sten Gatzke
IPC分类号： B64D41/00 , B64D33/02
CPC分类号： F03D9/32 , B64D41/007 , B64D2241/00 , F03D1/04 , F03D9/00 , F03D9/25 , F03D17/00 , F05B2220/50 , F05B2240/921 , Y02E10/72
摘要： A power generation system for integration into an aircraft system, including a secondary power supply device having a generator turbine arranged in a duct running between a forward opening and a rearward opening on the fuselage of the aircraft. An electromagnetic unlocking device locks and unlocks a covering device on the forward opening, depending on a signal strength supplied to the unlocking device. The system also includes an actuation device that generates an opening or closing signal for an opening and closing device, and an opening function switching device that activates the unlocking device electrically with a signal strength that locks the covering device in an initial state, and on receipt of a power requirement signal from a power generation monitoring device, activates the unlocking device with a second signal strength that unlocks the covering device.
摘要翻译：一种用于集成到飞行器系统中的发电系统，包括具有发电机涡轮机的二次供电装置，发电机涡轮机布置在运行在飞行器的机身上的前开口和后开口之间的管道中。电磁解锁装置根据提供给解锁装置的信号强度来锁定和解锁正向开口上的覆盖装置。该系统还包括产生用于打开和关闭装置的打开或关闭信号的致动装置，以及打开功能切换装置，该打开功能切换装置利用在初始状态下锁定覆盖装置的信号强度以及接收时激活解锁装置来自发电监测装置的功率需求信号，以解锁覆盖装置的第二信号强度来激活解锁装置。

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