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1.发明授权公开(公告)号：US07896288B2
公开(公告)日：2011-03-01
申请号：US11720818
申请日：2005-12-05
Applicant: Frederic Sauvinet
Inventor： Frederic Sauvinet
IPC: B64C5/02
CPC classification number: B64C9/12
Abstract: A roll steering method subdivides the direction of an aircraft control surface into two elements and, during a roll control operation using ailerons, steers an upper element of the control surface in the roll direction and a lower element in the opposite direction.
Abstract translation: 滚动转向方法将飞行器控制面的方向分为两个部件，并且在使用副翼的滚动控制操作期间，沿着滚动方向转向控制表面的上部元件，并在相反方向上引导下部元件。
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2.发明申请公开(公告)号：US20060060699A1
公开(公告)日：2006-03-23
申请号：US11002216
申请日：2004-12-03
Applicant: Regis Boe , Frederic Sauvinet
Inventor： Regis Boe , Frederic Sauvinet
IPC: B64C9/00
Abstract: According to the invention, prior to the resource, the adjustable horizontal tailplane (2) is nose-up deflected and the elevators (4) are nose-down deflected.
Abstract translation: 根据本发明，在资源之前，可调节的水平尾翼（2）被鼻梁偏转并且电梯（4）被向下偏转。
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Patent Agency Ranking
3.发明申请公开(公告)号：US20100222946A1
公开(公告)日：2010-09-02
申请号：US12713895
申请日：2010-02-26
Applicant: Frederic Sauvinet
Inventor： Frederic Sauvinet
IPC: G05D1/00
CPC classification number: B64C9/32 , B64C13/16 , B64C27/008 , B64F5/60 , G05D1/0083 , Y02T50/32 , B64F5/0045
Abstract: A process and a device for automatically optimising on the ground the aerodynamic configuration of an aircraft.The device (1) includes means (7, 8, 10) for determining and applying to the spoilers (6) a command providing the aircraft with an optimum aerodynamic configuration.
Abstract translation: 一种用于在地面上自动优化飞机的空气动力学配置的过程和装置。 装置（1）包括用于确定并向扰流板（6）施加提供飞行器最佳空气动力学构造的命令的装置（7,8,10）。
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4.发明申请公开(公告)号：US20050178899A1
公开(公告)日：2005-08-18
申请号：US11002067
申请日：2004-12-03
Applicant: Regis Boe , Frederic Sauvinet
Inventor： Regis Boe , Frederic Sauvinet
IPC: B64C5/00 , B64C5/02 , B64C5/10 , B64C9/00 , B64C9/02 , B64C9/04 , B64C9/06 , B64C9/08 , B64C9/10 , B64C9/12 , B64C9/30 , B64C13/00 , B64C17/00
Abstract: Process for reducing the aerodynamic loads applied to the elevators of an aircraft during takeoff. According to the invention, prior to the rotation, the adjustable horizontal tailplane (2) is nose-up overdeflected and the elevators (4) are nose-down deflected.
Abstract translation: 起飞过程中降低飞机电梯的空气动力学负荷。 根据本发明，在旋转之前，可调节的水平尾翼（2）被鼻梁过度偏转并且电梯（4）被鼻下偏转。
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5.发明申请METHOD AND DEVICE FOR GENERATING AN OPTIMUM AERODYNAMIC CONFIGURATION OF AN AIRCRAFT DURING A FLIGHT 有权用于在飞行中产生飞机的最佳航空配置的方法和装置公开(公告)号：US20100219298A1
公开(公告)日：2010-09-02
申请号：US12713782
申请日：2010-02-26
Applicant: Frederic Sauvinet
Inventor： Frederic Sauvinet
Abstract: A process and device for the automatic flight optimisation of the aerodynamic configuration of an aircraft.The device (1) includes means (7, 8, 10) for determining and applying to the spoilers (6) of the aircraft commands for providing the aircraft with an optimum aerodynamic configuration.
Abstract translation: 用于飞行器空气动力学结构的自动飞行优化的过程和装置。 装置（1）包括用于确定和应用于用于为飞行器提供最佳空气动力学构造的飞行器命令的扰流板（6）的装置（7,8,10）。
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6.发明申请公开(公告)号：US20090250551A1
公开(公告)日：2009-10-08
申请号：US11720818
申请日：2005-12-05
Applicant: Frederic Sauvinet
Inventor： Frederic Sauvinet
IPC: B64C9/00
CPC classification number: B64C9/12
Abstract: The invention concerns a method which consists in subdividing the direction of the control surface into at least two elements (6I, 6S) and, during a roll control using the ailerons (5G, 5D), steering the upper element (6S) in the roll direction and the lower element (6I) in the opposite direction.
Abstract translation: 本发明涉及一种方法，该方法包括将控制表面的方向细分成至少两个元件（6I，6S），并且在使用副翼（5G，5D）进行滚动控制期间，将滚轮中的上部元件（6S） 方向和下部元件（6I）在相反方向。
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7.发明申请METHOD AND DEVICE FOR PILOTING AN AIRCRAFT OPTIMIZING THE CONTROL OF THE AILERONS IN AN ENHANCED-LIFT CONFIGURATION 有权用于提升飞机的方法和装置，优化在增强提升装置中控制艾滋病公开(公告)号：US20090230253A1
公开(公告)日：2009-09-17
申请号：US12294588
申请日：2007-05-21
Applicant: Franck Delaplace , Sophie Lambeaux , Frederic Sauvinet
Inventor： Franck Delaplace , Sophie Lambeaux , Frederic Sauvinet
CPC classification number: B64C9/06 , B64C13/16 , B64C13/503 , G05D1/0808
Abstract: In conformance with the invention, based on the incident conditions and velocity, the steering of the ailerons is weakly negative (b0) or corresponds either to the maximum sharpness of the aircraft (b1), or the optimal lift of the latter (b2).
Abstract translation: 根据本发明，基于事故状况和速度，副翼的转向是弱负的（b0），或对应于飞行器的最大锋度（b1），或对应于后者（b2）的最佳提升。
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