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公开(公告)号：US08011613B2
公开(公告)日：2011-09-06
申请号：US12106485
申请日：2008-04-21
申请人： Mathieu Belleville
发明人： Mathieu Belleville
CPC分类号： B64D27/14 , B64D2027/005 , Y02T50/66
摘要： An aircraft includes a fuselage and at least one engine provided with at least one propeller and mounted at a rear part of the fuselage, on the back thereof, with the at least one engine having an axis substantially parallel to the longitudinal axis of the fuselage, where the at least one engine is mounted on the rear part of the fuselage so that the propeller lies forward of the tails, and provided at the rear part of the fuselage, symmetrically with respect to the fuselage, are removable noise masking surfaces configured to occupy either a deployed position in which the removable noise masking surfaces project laterally with respect to the rear part of the fuselage and are positioned plumb with the propeller, or a retracted position in which the removable noise masking surfaces are incorporated into the rear part of the fuselage.
摘要翻译： 飞机包括机身和至少一个设置有至少一个螺旋桨并且安装在机身的后部的后部的至少一个发动机，其中至少一个发动机具有基本上平行于机身的纵向轴线的轴线， 其中至少一个发动机安装在机身的后部，使得螺旋桨位于尾部的前方，并且相对于机身对称地设置在机身的后部，是被构造成占据 无论是展开位置，其中可移除的噪声掩蔽表面相对于机身的后部侧向突出并且与螺旋桨一起放置在铅垂处，或缩回位置，其中可移除的噪声掩蔽表面被结合到机身的后部 。
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公开(公告)号：US07819358B2
公开(公告)日：2010-10-26
申请号：US11691200
申请日：2007-03-26
申请人： Mathieu Belleville
发明人： Mathieu Belleville
IPC分类号： B64C15/00
CPC分类号： B64C11/001 , B64C15/02 , B64D27/20
摘要： According to the invention, said aircraft comprises at least one engine which has ducted propellers and is mounted on the back of the rear portion of the fuselage, the cowling being able to be oriented about the axis of said engine.
摘要翻译： 根据本发明，所述飞行器包括至少一个具有导管螺旋桨并且安装在机身后部后部的发动机，整流罩能够围绕所述发动机的轴线定向。
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公开(公告)号：US08336823B2
公开(公告)日：2012-12-25
申请号：US12520881
申请日：2007-12-21
IPC分类号： B64C1/00
CPC分类号： B64C1/0009 , B64C2001/0045 , B64D27/12
摘要： An aircraft fuselage including a front part including a cockpit, a central part, and a rear part. The central part of the fuselage includes a first zone located at the front part and that increases in width to a maximum width towards the rear of the aircraft, a second zone that decreases in width, and a third zone that has an essentially constant width and is located behind the second zone, width begin measured along the pitch axis.
摘要翻译： 飞机机身包括前部，包括驾驶舱，中央部分和后部。 机身的中央部分包括位于前部的第一区，并且宽度增加到飞行器后部的最大宽度，宽度减小的第二区和具有基本恒定宽度的第三区和 位于第二区后面，沿俯仰轴开始测量宽度。
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公开(公告)号：US20100032518A1
公开(公告)日：2010-02-11
申请号：US12520881
申请日：2007-12-21
CPC分类号： B64C1/0009 , B64C2001/0045 , B64D27/12
摘要： An aircraft fuselage including a front part including a cockpit, a central part, and a rear part. The central part of the fuselage includes a first zone located at the front part and that increases in width to a maximum width towards the rear of the aircraft, a second zone that decreases in width, and a third zone that has an essentially constant width and is located behind the second zone, width begin measured along the pitch axis.
摘要翻译： 飞机机身包括前部，包括驾驶舱，中央部分和后部。 机身的中央部分包括位于前部的第一区，并且宽度增加到飞行器后部的最大宽度，宽度减小的第二区和具有基本恒定宽度的第三区和 位于第二区后面，沿俯仰轴开始测量宽度。
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公开(公告)号：US08708275B2
公开(公告)日：2014-04-29
申请号：US12531980
申请日：2008-03-19
申请人： Mathieu Belleville
发明人： Mathieu Belleville
CPC分类号： B64C25/36 , B64C25/405 , B64D41/007 , Y02T50/44 , Y02T50/53 , Y02T50/823
摘要： In order to generate an efficient aerodynamic braking force, whatever the speed of a vehicle such as an airplane flying in the air, the method includes a step for the production of energy by the vehicle, a step of storage of the energy produced and a step of utilization of such energy to drive a propeller which generates a force opposing the forward motion of the vehicle. Energy is produced by using the displacement of the vehicle with respect to air using a propeller driving a generator, or using the displacement with respect to the ground, using wheels driving a generator, or using generators driven by motors of the vehicle. The energy can be stored in the pneumatic, electric or kinetic form and the generation and driving means are selected according to the technology used for the storage means.
摘要翻译： 为了产生高效的空气动力学制动力，无论诸如飞机在空中飞行的车辆的速度如何，该方法包括由车辆产生能量的步骤，存储所产生的能量的步骤和步骤 利用这种能量来驱动产生与车辆向前运动相反的力的螺旋桨。 通过使用驱动发电机的推进器使用车辆相对于空气的位移，或者使用相对于地面的位移，使用驱动发电机的车轮，或者使用由车辆的电动机驱动的发电机来产生能量。 能量可以以气动，电动或动力学形式存储，根据用于存储装置的技术选择发电和驱动装置。
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公开(公告)号：US20100170981A1
公开(公告)日：2010-07-08
申请号：US12531980
申请日：2008-03-19
申请人： Mathieu Belleville
发明人： Mathieu Belleville
CPC分类号： B64C25/36 , B64C25/405 , B64D41/007 , Y02T50/44 , Y02T50/53 , Y02T50/823
摘要： In order to generate an efficient aerodynamic braking force, whatever the speed of a vehicle such as an airplane flying in the air, the method includes a step for the production of energy by the vehicle, a step of storage of the energy produced and a step of utilisation of such energy to drive a propeller which generates a force opposing the forward motion of the vehicle. Energy is produced by using the displacement of the vehicle with respect to air using a propeller driving a generator, or using the displacement with respect to the ground, using wheels driving a generator, or using generators driven by motors of the vehicle. The energy can be stored in the pneumatic, electric or kinetic form and the generation and driving means are selected according to the technology used for the storage means.
摘要翻译： 为了产生高效的空气动力学制动力，无论诸如飞机在空中飞行的车辆的速度如何，该方法包括由车辆产生能量的步骤，存储所产生的能量的步骤和步骤 利用这种能量来驱动产生与车辆向前运动相反的力的螺旋桨。 通过使用驱动发电机的推进器使用车辆相对于空气的位移，或者使用相对于地面的位移，使用驱动发电机的车轮，或者使用由车辆的电动机驱动的发电机来产生能量。 能量可以以气动，电动或动力学形式存储，根据用于存储装置的技术选择发电和驱动装置。
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公开(公告)号：US20080105781A1
公开(公告)日：2008-05-08
申请号：US11691200
申请日：2007-03-26
申请人： Mathieu Belleville
发明人： Mathieu Belleville
CPC分类号： B64C11/001 , B64C15/02 , B64D27/20
摘要： Aircraft with reduced environmental impact.According to the invention, said aircraft comprises at least one engine which has ducted propellers and is mounted on the back of the rear portion of the fuselage, the cowling being able to be oriented about the axis of said engine.
摘要翻译： 降低环境影响的飞机。 根据本发明，所述飞行器包括至少一个具有导管螺旋桨并且安装在机身后部后部的发动机，整流罩能够围绕所述发动机的轴线定向。
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