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1. 发明申请

WO2009023114A2 LENTICULAR AIRSHIP AND ASSOCIATED CONTROLS 审中-公开
标题翻译：航空和相关控制
公开(公告)号：WO2009023114A2
公开(公告)日：2009-02-19
申请号：PCT/US2008009453
申请日：2008-08-07
申请人： LTA CORP , BALASKOVIC PIERRE
发明人： BALASKOVIC PIERRE
IPC分类号： B64B1/36 , B64B1/34
CPC分类号： B64B1/00 , B64B1/34 , B64B1/36 , B64C13/04 , B64D43/00 , Y02T50/44
摘要： A system for controlling yaw associated with an airship may include one or more vertical control surfaces associated with the airship, a first power source and a second power source, each configured to provide a thrust associated with the airship, and a yaw control configured to receive an input indicative of a desired yaw angle. The system may further include a controller communicatively connected to the yaw control, the one or more vertical control surfaces, and the first and second power sources. The controller may be configured to receive an output signal from the yaw control corresponding to the desired yaw angle and to generate a control signal configured to modify a state associated with at least one of the one or more vertical control surfaces, the first power source, and the second power source, such that the airship substantially attains the desired yaw angle.
摘要翻译：用于控制与飞艇相关联的偏航的系统可以包括与飞艇相关联的一个或多个垂直控制表面，第一电源和第二电源，每个被配置为提供与飞艇相关联的推力，以及偏航控制，被配置为接收指示期望的偏航角的输入。系统还可以包括通信地连接到偏航控制器，一个或多个垂直控制表面以及第一和第二电源的控制器。控制器可以被配置为从对应于期望的偏航角的偏航控制接收输出信号，并且产生控制信号，该控制信号被配置为修改与一个或多个垂直控制表面，第一电源，和第二动力源，使得飞艇基本上达到所需的偏航角。

2. 发明申请

WO2012012275A3 SYSTEM AND METHOD FOR SOLAR-POWERED AIRSHIP 审中-公开
标题翻译： SOLAR-POWERED AIRSHIP的系统和方法
公开(公告)号：WO2012012275A3
公开(公告)日：2012-04-19
申请号：PCT/US2011044102
申请日：2011-07-15
申请人： LTA CORP , GOELET JOHN
发明人： GOELET JOHN
IPC分类号： B64B1/00 , B64B1/08 , B64B1/10 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/34 , B64B1/58
CPC分类号： B64B1/06 , B64B1/005 , B64B1/08 , B64B1/10 , B64B1/16 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/30 , B64B1/58 , B64D9/00
摘要： A solar-powered airship with a hull configured to contain a gas and at least one propulsion assembly with a propulsion device and electric motors configured to drive the propulsion device. The airship may also include a power supply system including solar panels operatively coupled to the electric motors and configured to supply power to the electric motors. The power supply system may also include batteries operatively coupled to the solar panels and configured to receive and store electrical energy supplied by the solar panels, the batteries being further operatively coupled to the electric motors and configured to supply power to the electric motors. The batteries may each be located within an outer envelope of the airship defined by the hull of the airship in a position selected to provide ballast. The solar-powered airship may also include a cargo system configured to contain passengers or freight.
摘要翻译：具有被配置为容纳气体的船体的太阳能飞艇以及具有推进装置和配置成驱动推进装置的电动机的至少一个推进组件。飞艇还可以包括电力供应系统，该电力供应系统包括可操作地耦合到电动机并且被配置为向电动机供电的太阳能面板。电源系统还可以包括可操作地连接到太阳能电池板并配置为接收和存储由太阳能电池板供应的电能的电池，电池进一步可操作地连接到电动机并且配置为向电动机供电。每个电池可以位于由飞艇的船体限定的飞艇的外壳内，其位置被选择为提供压载物。太阳能飞艇还可以包括配置为容纳乘客或货物的货物系统。

3. 发明申请

WO2015108607A3 CARGO AIRSHIP 审中-公开
标题翻译：货运航空
公开(公告)号：WO2015108607A3
公开(公告)日：2015-11-26
申请号：PCT/US2014063675
申请日：2014-11-03
申请人： LTA CORP
发明人： GOELET JOHN , KAPITAN LOGINN , HOCHSTETLER RON
IPC分类号： B64B1/22 , B64D1/22 , B64D9/00
CPC分类号： B64B1/08 , B64B1/10 , B64B1/20 , B64B1/22 , B64B1/32 , B64B1/34 , B64B1/58 , B64B1/70 , B64D1/02 , B64D1/22 , B64D9/003 , Y02T50/46
摘要： A cargo airship (10) is disclosed. The cargo airship may include a hull (12) configured to contain a gas and at least one propulsion assembly (16) coupled to the airship and including a propulsion device. The cargo airship may further include a payload bay (64) comprising an external cargo area (66) located outside of the hull. The cargo airship may also include a cargo handling system including at least one hoisting mechanism (82) configured to lift cargo into the external cargo area while the airship is hovering.
摘要翻译：披露了一艘货船（10艘）。货物飞艇可以包括构造成容纳气体的船体（12）和联接到飞艇并且包括推进装置的至少一个推进组件（16）。货物飞艇还可以包括有效载荷舱（64），其包括位于船体外部的外部货物区域（66）。货物飞艇还可以包括货物处理系统，其包括至少一个提升机构（82），其构造成在飞艇盘旋时将货物提升到外部货物区域。

4. 发明申请

WO2012135117A2 AIRSHIP INCLUDING AERODYNAMIC, FLOATATION, AND DEPLOYABLE STRUCTURES 审中-公开
标题翻译：航空包括航空，航行和可配置的结构
公开(公告)号：WO2012135117A2
公开(公告)日：2012-10-04
申请号：PCT/US2012030562
申请日：2012-03-26
申请人： LTA CORP , GOELET JOHN
发明人： GOELET JOHN
IPC分类号： B64B1/14
CPC分类号： B64B1/68 , B64B1/00 , B64B1/06 , B64B1/12 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/34 , B64B1/58 , B64B1/60 , B64B2201/00 , B64C25/32 , B64C25/56 , B64D2211/00
摘要： An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship.
摘要翻译：提供飞艇。飞艇包括构造成容纳气体的船体，耦合到船体的至少一个推进组件，并且包括推进装置，以及包括多个整流罩结构（包括一个或多个板条）的至少一个空气动力部件，其中至少一个空气动力学组件与船体相关联，并且被配置为引导飞艇周围的气流。

5. 发明申请

WO2015191812A3 AIRSHIPS FOR WEATHER MANIPULATION 审中-公开
公开(公告)号：WO2015191812A3
公开(公告)日：2016-02-11
申请号：PCT/US2015035261
申请日：2015-06-11
申请人： LTA CORP
发明人： GOELET JOHN
IPC分类号： B64B1/22 , A01G15/00
CPC分类号： A01G15/00 , B64B1/06 , B64B1/14 , B64B1/22
摘要： Airships for weather manipulation are disclosed. An airship may include a hull and a frame supporting the hull. The airship may also include a container configured to capture and transport a cloud. The airship may also include a sunlight reflecting system configured to block the sunlight over a destination area on ground. The airship may also include a nozzle configured to distribute a material to the cloud. The airship may also include a sensing system including at least one sensor configured to measure a parameter reflecting a condition of the cloud. The airship may further include at least one weather interference device configured to generate a wave or light and direct the wave or light toward the cloud. In some examples, two or more airships may be used to tow a parachute-style container deployable for capturing and transporting the cloud.
摘要翻译：披露了用于天气操纵的飞艇。飞艇可以包括船体和支撑船体的框架。飞艇还可以包括被配置为捕获和运输云的容器。飞艇还可以包括阳光反射系统，该系统被配置为阻挡地面上的目的地区域的太阳光。飞艇还可以包括被配置为将材料分配到云的喷嘴。飞艇还可以包括感测系统，其包括至少一个传感器，该传感器被配置成测量反映云的状况的参数。飞艇还可以包括至少一个天气干扰装置，其被配置为产生波或光并将波或光引向云。在一些示例中，可以使用两个或更多个飞艇来拖动可部署用于捕获和运输云的降落伞式容器。

6. 发明申请

WO2009023114A8 LENTICULAR AIRSHIP AND ASSOCIATED CONTROLS 审中-公开
标题翻译：独特的AIRSHIP和相关控制
公开(公告)号：WO2009023114A8
公开(公告)日：2009-05-22
申请号：PCT/US2008009453
申请日：2008-08-07
申请人： LTA CORP , BALASKOVIC PIERRE
发明人： BALASKOVIC PIERRE
IPC分类号： B64B1/36 , B64B1/34
CPC分类号： B64B1/00 , B64B1/34 , B64B1/36 , B64C13/04 , B64D43/00 , Y02T50/44
摘要： A system for controlling yaw associated with an airship may include one or more vertical control surfaces associated with the airship, a first power source and a second power source, each configured to provide a thrust associated with the airship, and a yaw control configured to receive an input indicative of a desired yaw angle. The system may further include a controller communicatively connected to the yaw control, the one or more vertical control surfaces, and the first and second power sources. The controller may be configured to receive an output signal from the yaw control corresponding to the desired yaw angle and to generate a control signal configured to modify a state associated with at least one of the one or more vertical control surfaces, the first power source, and the second power source, such that the airship substantially attains the desired yaw angle.
摘要翻译：用于控制与飞艇相关的偏航的系统可以包括与飞艇相关联的一个或多个垂直控制表面，第一动力源和第二动力源，每个构造成提供与飞艇相关联的推力，以及偏航控制器，配置为接收指示期望的偏航角的输入。该系统可以进一步包括通信地连接到偏航控制器，一个或多个竖直控制表面，以及第一和第二动力源的控制器。控制器可以被配置为从对应于期望偏航角的偏航控制接收输出信号并且生成控制信号，该控制信号被配置为修改与一个或多个垂直控制表面，第一动力源，和第二动力源，使得飞艇基本上达到期望的偏航角。

7. 发明申请

WO2008105851A9 LENTICULAR AIRSHIP 审中-公开
公开(公告)号：WO2008105851A9
公开(公告)日：2008-10-16
申请号：PCT/US2007021962
申请日：2007-10-15
申请人： LTA CORP , BALASKOVIC PIERRE
发明人： BALASKOVIC PIERRE
CPC分类号： B64B1/06 , B64B1/10 , B64B1/12 , B64B1/30 , B64B1/34 , B64B2201/00 , B64C2201/00
摘要： An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.
摘要翻译：飞艇可包括基本成形为扁球体的船体，限定支撑结构的一个或多个框架构件，其中支撑结构形成船体的至少部分支撑，至少一个水平稳定构件可操作地联接到船体的下表面飞艇和至少一个具有第一端和第二端的水平稳定件。该至少一个水平稳定构件可以限定一个五面体构型。飞艇还可以包括垂直稳定构件，该垂直稳定构件具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端部和至少一个水平稳定构件的第一端部可以可操作地彼此联接。

8. 发明申请

WO2008105851A2 LENTICULAR AIRSHIP 审中-公开
标题翻译：航空公司
公开(公告)号：WO2008105851A2
公开(公告)日：2008-09-04
申请号：PCT/US2007021962
申请日：2007-10-15
申请人： LTA CORP , BALASKOVIC PIERRE
发明人： BALASKOVIC PIERRE
CPC分类号： B64B1/06 , B64B1/10 , B64B1/12 , B64B1/30 , B64B1/34 , B64B2201/00 , B64C2201/00
摘要： An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.
摘要翻译：飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。所述至少一个水平稳定构件可以限定一个双面构型。飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

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