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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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2.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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3.发明申请SYSTEM, A METHOD AND A COMPUTER PROGRAM PRODUCT FOR MANEUVERING OF AN AIR VEHICLE WITH TILTABLE PROPULSION UNIT 有权系统，方法和计算机程序产品，用于使用可倾斜的推进装置运行空中的车辆公开(公告)号：US20140339372A1
公开(公告)日：2014-11-20
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 Volvoick
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.
Abstract translation: 一种被配置为控制包括至少一个可倾斜推进单元的至少一个可倾斜推进单元的空中交通工具的减速过程的控制系统，所述至少一个可倾斜推进单元中的每一个可倾斜以提供其方向至少在一般的垂直推力矢量方向 和相对于空中车辆的总纵向推力向量方向。
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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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