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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

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。

3. 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。

4. 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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