-
公开(公告)号：US20100320314A1
公开(公告)日：2010-12-23
申请号：US12222355
申请日：2008-08-07
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
Abstract: 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.
Abstract translation: 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。
-
公开(公告)号：US20120160959A1
公开(公告)日：2012-06-28
申请号：US13342373
申请日：2012-01-03
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
IPC: B64B1/00
CPC classification number: B64B1/06 , B64B1/10 , B64B1/12 , B64B1/30 , B64B1/34 , B64B2201/00 , B64C2201/00
Abstract: 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.
Abstract translation: 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。
-
公开(公告)号：US20080179454A1
公开(公告)日：2008-07-31
申请号：US11907883
申请日：2007-10-18
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
CPC classification number: B64B1/06 , B64B1/10 , B64B1/12 , B64B1/30 , B64B1/34 , B64B2201/00 , B64C2201/00
Abstract: 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.
Abstract translation: 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。
-
公开(公告)号：US20140070050A1
公开(公告)日：2014-03-13
申请号：US14080314
申请日：2013-11-14
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
IPC: B64B1/00
Abstract: 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.
Abstract translation: 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。
-
公开(公告)号：US08616503B2
公开(公告)日：2013-12-31
申请号：US13649177
申请日：2012-10-11
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
IPC: B64C13/18
Abstract: 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.
Abstract translation: 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。
-
Patent Agency Ranking
公开(公告)号：US08297550B2
公开(公告)日：2012-10-30
申请号：US12222355
申请日：2008-08-07
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
IPC: G01C21/00
Abstract: 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.
Abstract translation: 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。
-
公开(公告)号：US08109462B2
公开(公告)日：2012-02-07
申请号：US12957989
申请日：2010-12-01
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
CPC classification number: B64B1/06 , B64B1/10 , B64B1/12 , B64B1/30 , B64B1/34 , B64B2201/00 , B64C2201/00
Abstract: 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.
Abstract translation: 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。
-
公开(公告)号：US09840318B2
公开(公告)日：2017-12-12
申请号：US14080314
申请日：2013-11-14
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
Abstract: 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.
-
公开(公告)号：US08418952B2
公开(公告)日：2013-04-16
申请号：US13342373
申请日：2012-01-03
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
CPC classification number: B64B1/06 , B64B1/10 , B64B1/12 , B64B1/30 , B64B1/34 , B64B2201/00 , B64C2201/00
Abstract: 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.
Abstract translation: 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。
-
公开(公告)号：US20110163200A1
公开(公告)日：2011-07-07
申请号：US12957989
申请日：2010-12-01
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
CPC classification number: B64B1/06 , B64B1/10 , B64B1/12 , B64B1/30 , B64B1/34 , B64B2201/00 , B64C2201/00
Abstract: 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.
Abstract translation: 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。
-
-
-
-
-
-
-
-
-
Search Results
12
records
(took 0.022 seconds)
