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Patent Agency Ranking
1.发明授权System, a method and a computer program product for maneuvering of an air vehicle 有权用于机动车辆的系统，方法和计算机程序产品公开(公告)号：US09540100B2
公开(公告)日：2017-01-10
申请号：US14415433
申请日：2013-09-12
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Guy Dekel , Lior Zivan , Yoav Efraty , Amit Wolff , Avner Volovick
CPC classification number: B64C27/52 , B64C29/0033 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/086 , B64C2201/104 , B64C2201/162 , B64C2201/165 , B64C2201/187 , G05D1/042 , G05D1/0808 , G05D1/0858 , G05D1/102
Abstract: A control system configured to control an acceleration of an air vehicle which comprises a tiltable propulsion unit that is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle, the control system comprising: (a) an input interface for receiving information indicative of a monitored airspeed of the air vehicle; and (b) a control unit, configured to issue controlling commands to a controller of the tiltable propulsion unit for controlling the acceleration of the air vehicle.
Abstract translation: 一种被配置为控制空中交通工具的加速度的控制系统，该控制系统包括可倾斜的推进单元，该倾斜推进单元可倾斜以提供方向至少相对于空气在一般的垂直推力矢量方向和一般纵向推力向量方向之间变化的推力 车辆，所述控制系统包括：（a）输入接口，用于接收指示所述空中交通工具的监控空速的信息; 以及（b）控制单元，被配置为向所述可倾斜推进单元的控制器发出控制命令，以控制所述空中交通工具的加速度。
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公开(公告)号：US10474167B2
公开(公告)日：2019-11-12
申请号：US15675547
申请日：2017-08-11
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Guy Dekel , Lior Zivan , Yoav Efraty , Amit Wolff , Avner Volovick
Abstract: A control system configured to control a deceleration process of an air vehicle which comprises at least one tiltable propulsion unit, each of the at least one tiltable propulsion units is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle.
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公开(公告)号：US09731818B2
公开(公告)日：2017-08-15
申请号：US14372060
申请日：2013-01-10
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Guy Dekel , Lior Zivan , Yoav Efraty , Amit Wolff , Avner Volovick
CPC classification number: B64C27/26 , B64C19/00 , B64C29/00 , B64C29/0033 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/086 , B64C2201/104 , B64C2201/162 , B64C2201/165 , B64C2201/187 , G05D1/0676 , G05D1/0858
Abstract: A control system configured to control a deceleration process of an air vehicle which comprises at least one tiltable propulsion unit, each of the at least one tiltable propulsion units is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle.
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公开(公告)号：US11932386B2
公开(公告)日：2024-03-19
申请号：US17296427
申请日：2019-11-20
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Ehud Baharav , Avner Volovick
CPC classification number: B64C29/0033 , B64C29/0025 , B64C39/04
Abstract: An air vehicle has an airframe, aerodynamic lift-generating wings, and a propulsion system. The propulsion system provides propulsion to the air vehicle in powered aerodynamic flight mode and in vectored flight mode, and stability and control in vectored flight mode. The propulsion system includes a first set of non-pivotable first propulsion units, arranged in polygonal arrangement with respect to the airframe, enclosing the air vehicle center of gravity, providing a fixed vertical thrust vector and an aggregate vertical thrust sufficient for enabling vectored flight mode. The propulsion system includes a second set of pivotable second propulsion units, arranged in spaced relationship with respect to the center of gravity, and provide vectored control moments to the air vehicle in three rotational degrees of freedom. The second propulsion units enable angular displacement of the respective thrust vectors at least between a respective vertical position and a respective horizontal position, and provide at least an aggregate horizontal thrust sufficient for providing powered aerodynamic flight mode.
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5.发明申请SYSTEM, A METHOD AND A COMPUTER PROGRAM PRODUCT FOR MANEUVERING OF AN AIR VEHICLE 有权系统，方法和计算机程序产品用于航空飞行器公开(公告)号：US20150197335A1
公开(公告)日：2015-07-16
申请号：US14415433
申请日：2013-09-12
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Guy Dekel , Lior Zivan , Yoav Efraty , Amit Wolff , Avner Volovick
CPC classification number: B64C27/52 , B64C29/0033 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/086 , B64C2201/104 , B64C2201/162 , B64C2201/165 , B64C2201/187 , G05D1/042 , G05D1/0808 , G05D1/0858 , G05D1/102
Abstract: A control system configured to control an acceleration of an air vehicle which comprises a tiltable propulsion unit that is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle, the control system comprising: (a) an input interface for receiving information indicative of a monitored airspeed of the air vehicle; and (b) a control unit, configured to issue controlling commands to a controller of the tiltable propulsion unit for controlling the acceleration of the air vehicle.
Abstract translation: 一种被配置为控制空中交通工具的加速度的控制系统，该控制系统包括可倾斜的推进单元，该倾斜推进单元可倾斜以提供方向至少相对于空气在一般的垂直推力矢量方向和一般纵向推力向量方向之间变化的推力 车辆，所述控制系统包括：（a）输入接口，用于接收指示所述空中交通工具的监控空速的信息; 以及（b）控制单元，被配置为向所述可倾斜推进单元的控制器发出控制命令，以控制所述空中交通工具的加速度。
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