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1. 发明专利

JP2012201133A Vehicle travel control method and device 审中-公开
标题翻译：车辆行驶控制方法和装置
公开(公告)号：JP2012201133A
公开(公告)日：2012-10-22
申请号：JP2011065085
申请日：2011-03-23
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： B60W30/16 , B60H1/00
摘要： PROBLEM TO BE SOLVED: To provide a vehicle travel control method and device for suppressing reduction in air flow rate to be introduced to a vehicle on the back side without greatly increasing the consumed energy during following travel of a vehicle.SOLUTION: In the vehicle travel control method and device, when one's own vehicle is substantially stored in a peeling region of the air flow at the back of the other vehicle and the inflow air flow rate blown into the own vehicle is smaller than the necessary air flow rate required by an object to be cooled by the air flow, the inflow air flow rate is increased by separating the part from which the air is introduced into the own vehicle from the peeling region of the air flow at the back of the other vehicle. Thus, in a state where the performance of a cooling system of the own vehicle is maintained, saving of the consumed energy and travel stability improvement by the air resistance reduction effect are achieved in both of the own vehicle and the other vehicle.
摘要翻译：解决的问题：提供一种车辆行驶控制方法和装置，用于抑制在后侧引入车辆的空气流量的减少，而不会大大增加车辆行驶中的消耗能量。解决方案：在车辆行驶控制方法和装置中，当自己的车辆基本上存储在另一车辆的后部的空气流的剥离区域并且吹入本车辆的流入空气流量小于通过空气流被冷却的物体所需的必要的空气流量，通过将从空气引入自身车辆的部分与背面的空气流的剥离区域分开来增加流入空气流量另一辆车。因此，在本车辆的冷却系统的性能得以维持的状态下，在本车辆和其他车辆两者中都能够实现消耗能量的降低和通过减少空气阻力的行驶稳定性的提高。版权所有（C）2013，JPO＆INPIT

2. 发明专利

JP2011225058A Movable body 有权
标题翻译：可移动身体
公开(公告)号：JP2011225058A
公开(公告)日：2011-11-10
申请号：JP2010095238
申请日：2010-04-16
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： B60F5/02 , B64C3/56 , B64C37/00
摘要： PROBLEM TO BE SOLVED: To provide a movable body that prevents overturn when receiving a side wind, concerning a movable body including a wing at the top of a body thereof.SOLUTION: The movable body is configured to fold down the wing 32 provided at the top of the body 20 of the movable body. The wing 32 is folded to the position where the wing overlaps the body 20 of the movable body in a side view, thereby reducing the influence of a side wind during traveling with the wing 32 folded. Accordingly, the movable body prevents overturn.
摘要翻译：要解决的问题：提供一种在接收侧风时防止翻倒的移动体，涉及包括其主体顶部的机翼的可移动体。解决方案：可移动体构造成折叠设置在可移动体的主体20的顶部的翼32。机翼32在侧视图中被折叠到翼与可移动体的主体20重叠的位置，从而减少了在翼32折叠的行进期间侧风的影响。因此，可移动体防止翻倒。版权所有（C）2012，JPO＆INPIT

3. 发明专利

JP2007055372A Vertical taking-off/landing flying device 有权
标题翻译：垂直起落/起落飞行装置
公开(公告)号：JP2007055372A
公开(公告)日：2007-03-08
申请号：JP2005241479
申请日：2005-08-23
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： B64C29/00 , B64C15/00
CPC分类号： G05D1/102
摘要： PROBLEM TO BE SOLVED: To provide a technology capable of keeping the stability of attitude control of a machine body, even if weight distribution in the machine body of a vertical taking-off/landing flying device varies.
SOLUTION: The moment of inertia about a predetermined shaft of the machine body of the vertical taking-off/landing flying device is timely derived (S105). In the attitude control of the machine body, trust to be generated by a plurality of thrust generating machines disposed on the machine body is adjusted based on the moment of inertia at the time of the attitude control (S117).
COPYRIGHT: (C)2007,JPO&INPIT
摘要翻译：要解决的问题：即使垂直起飞/着陆飞行装置的机体中的重量分布变化，提供能够保持机体的姿态控制的稳定性的技术。解决方案：及时导出关于垂直起飞/着陆飞行装置的机体的预定轴的惯性矩（S105）。在机体的姿态控制中，基于姿势控制时的惯性矩来调整由设置在机体上的多台推力发电机产生的信任（S117）。版权所有（C）2007，JPO＆INPIT

4. 发明专利

JP2006056364A Vertical take-off/landing aircraft 有权
标题翻译：垂直起飞/着陆飞机
公开(公告)号：JP2006056364A
公开(公告)日：2006-03-02
申请号：JP2004239645
申请日：2004-08-19
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： B64C29/00 , B64C27/10 , B64C27/20 , B64D27/02 , F02C1/02
CPC分类号： B64C27/20 , B64C29/0025 , B64C39/026
摘要： PROBLEM TO BE SOLVED: To suppress the generation of temperature distribution of a tip turbine fan in a vertical take-off/landing aircraft utilizing the tip turbine fan as a propulsion force source.
SOLUTION: In the vertical take-off/landing aircraft provided with the tip turbine fan 2 and performing vertical take-off/landing, the fan is rotated by blowing compression gas to the tip turbine mounted to the fan 10 in an annular turbine chamber 15 provided making a rotation shaft 17 of the fan 10 as a center. Three or more compression gas inlets 14 for feeding the compression gas to a turbine chamber 15 are arranged on a circumference of the turbine chamber 15 at equal intervals.
COPYRIGHT: (C)2006,JPO&NCIPI
摘要翻译：要解决的问题：为了抑制利用尖端涡轮风扇作为推进力源的垂直起飞/着陆飞机中的尖端涡轮风扇的温度分布的产生。解决方案：在设置有顶端涡轮风扇2并执行垂直起飞/着陆的垂直起飞/着陆飞机中，风扇通过将安装在风扇10上的尖端涡轮机的压缩气体吹向环形涡轮室15以风扇10的旋转轴17为中心。用于将压缩气体供给到涡轮室15的三个或更多个压缩气体入口14以等间隔布置在涡轮室15的圆周上。版权所有（C）2006，JPO＆NCIPI

5. 发明专利

JP2004306668A Vertical takeoff/landing device 有权
公开(公告)号：JP2004306668A
公开(公告)日：2004-11-04
申请号：JP2003099540
申请日：2003-04-02
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： B64C29/00 , B64C25/58 , B64C27/20 , B64C39/02 , B64D25/02
CPC分类号： B64C39/026 , B64C27/20
摘要： PROBLEM TO BE SOLVED: To provide a vertical takeoff/landing device excellent in maneuverability of a machine body and attitude stability, having a function protecting an operator from an impact in landing or the like, and capable of extremely stably flying when hovering near a building.
SOLUTION: The vertical takeoff/landing device is provided with the machine body 1 having a propulsion machine 2 which generates thrust force vertically upward and provided with a side wall surface 3 surrounding the propulsion machine 2, a plurality of air inlets 4 provided on the side wall surface 3 at equal intervals, duct portions 5 connecting this air inlet 4 to the propulsion machine 2, shutter portions 6 provided on the respective air inlets 4 and adjusting the air volume flowing in, and a control part 7 adjusting the opening level of these shutter portions 6. The machine body 1 can be moved in an arbitrary direction by giving instructions to the control part 7 by the operator. In comparison with conventional control of a machine body by weight shift, an attitude can be controlled more rapidly and maneuvering stability is improved.
COPYRIGHT: (C)2005,JPO&NCIPI

6. 发明专利

JP2014136463A Aerodynamic control device for vehicle or movable body and vehicle or movable body including aerodynamic control device 有权
标题翻译：用于车辆或可移动体和车辆或可移动体的空气动力学控制装置，包括气动控制装置
公开(公告)号：JP2014136463A
公开(公告)日：2014-07-28
申请号：JP2013004905
申请日：2013-01-15
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： B62D35/00 , B60R11/00 , B60R19/48
摘要： PROBLEM TO BE SOLVED: To provide an aerodynamic control device configured to be able to appropriately control a flow separation range of a flow around a vehicle body or a body of a vehicle such as a motor vehicle or other movable body even in a situation in which a non-stationary or transient flow phenomenon occurs in the flow around the vehicle body or the body.SOLUTION: An aerodynamic control device for a vehicle or other movable body of the present invention comprises: a rotating body constituted by at least two rotation member rotating around the same rotational axis at independent rotational velocities and cascaded in a direction of the rotational axis on a surface of a vehicle body or a surface of a body; and a rotation control unit controlling rotation of the at least two rotation members.
摘要翻译：要解决的问题：提供一种空气动力学控制装置，其被配置为能够适当地控制车体或机动车辆或其他可移动体等车辆的车体的流动分离范围，即使在本发明的车辆或其他可移动体的空气动力学控制装置包括：旋转体，其由至少两个旋转构件旋转构成，围绕相同的旋转轴线以独立的旋转速度围绕在车体或身体的表面上的旋转轴线的方向上级联; 以及旋转控制单元，其控制所述至少两个旋转构件的旋转。

7. 发明专利

JP2010211476A Risk determination device in aircraft 有权
标题翻译：飞机中的风险确定装置
公开(公告)号：JP2010211476A
公开(公告)日：2010-09-24
申请号：JP2009056439
申请日：2009-03-10
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： G08G5/00 , B64D45/00
摘要： PROBLEM TO BE SOLVED: To provide a risk determination device in an aircraft for properly determining the future risk of flight of the aircraft.
SOLUTION: A predicted altitude acquisition part 11 in a risk determination ECU 1 obtains a present altitude and a future altitude of the aircraft. A risk situation index calculation part 14 calculates a risk situation index based on the present altitude and the future altitude. A safe control command acquisition part 12 calculates and obtains a safe control command about the range where an airframe can be controlled safely. A pilot command acquisition part 13 obtains a pilot command about the operation of a control stick by an operator. A risk level determination index calculation part 15 calculates a risk level determination index based on the risk situation index calculated by the risk situation index calculation part 14, the safe control command obtained by the safe control command acquisition part 12, and the pilot command obtained by the pilot command acquisition part 13.
COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：提供飞机中的风险确定装置，以正确确定飞机未来的飞行风险。解决方案：风险确定ECU1中的预测高度获取部分11获得飞行器的当前高度和未来的高度。风险指标计算部14基于当前的高度和未来的高度来计算风险状况指标。安全控制指令获取部12计算并获得关于能够安全地控制机体的范围的安全控制指令。驾驶员命令获取部13获取操作者关于控制棒的操作的驾驶员指令。风险等级确定指标计算部15基于由风险状况指标计算部14计算出的风险状况指标，由安全控制指令获取部12得到的安全控制指令，以及由导航指令采集部分13.版权所有（C）2010，JPO＆INPIT

8. 发明专利

JP2008247123A Fan control device 有权
标题翻译：风扇控制装置
公开(公告)号：JP2008247123A
公开(公告)日：2008-10-16
申请号：JP2007089026
申请日：2007-03-29
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： B64D31/00 , B64C29/00
CPC分类号： F02C9/20 , F02C6/206 , F02K3/04 , F05D2220/329 , F05D2270/09 , F05D2270/093
摘要： PROBLEM TO BE SOLVED: To provide a fan control device capable of preventing a normal drive source from being brought into an overload state when part of a plurality of drive sources is broken.
SOLUTION: When an FADEC 10 detects an abnormality of either of an engine + compressor 11, 12, an FCC 3 controls an air quantity for fan drive so that it becomes lower than that before the abnormality is detected until the normal engine + compressor 11, 12 can supply air of a flow rate necessary for a fan 1 to generate a thrust force before the abnormality detection. Thus, this can prevent the overload state caused by a surge etc. generated in the normal engine + compressor 11, 12.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种风扇控制装置，其能够在多个驱动源的一部分被破坏时防止正常的驱动源进入过载状态。解决方案：当FADEC10检测到发动机+压缩机11,12中的任何一个异常时，FCC 3控制风扇驱动的空气量，使得其比检测到异常之前低，直到正常发动机+ 压缩机11,12可以提供风扇1所需的流量的空气，以产生异常检测之前的推力。因此，这可以防止由普通发动机+压缩机11,12产生的浪涌等引起的过载状态。版权所有：（C）2009，JPO＆INPIT

9. 发明专利

JP2005125976A Vertical taking off/landing flying device 有权
标题翻译：垂直起飞/着陆飞行装置
公开(公告)号：JP2005125976A
公开(公告)日：2005-05-19
申请号：JP2003365112
申请日：2003-10-24
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： B64C29/00 , B60F5/02
CPC分类号： B64C29/0025 , B60F5/02
摘要： PROBLEM TO BE SOLVED: To provide a compact vertical taking off/landing flying device capable of being simply and safely operated.
SOLUTION: Fans 2 are provided at a front part 1A of a vehicle body and a rear part 1C of the vehicle body respectively. An occupant seat 4 for seating an operator H is provided at a central part 1B of the vehicle body. A seating surface 4b of the occupant seat 4 is arranged at a lower position than a rotation surface of the fan 2. Further, at the central part 1B of the vehicle body, a driving source 3 for driving the fan 2 is arranged below the seating surface 4b of the occupant seat 4. According to such arrangement, the center of gravity of the flying device 1 is positioned at a position close to a lower part of the center of the vehicle body and is hung down from above by the thrust of the fans at the front and rear side of the vehicle body at flying. Accordingly, the stability of the vehicle body during flying is increased and the safety is enhanced.
COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：提供能够简单和安全地操作的紧凑型垂直起飞/着陆飞行装置。解决方案：风扇2分别设置在车体的前部1A和车体的后部1C。在车体的中央部1B设置有用于操作者H的乘员座椅4。乘员座椅4的座位表面4b布置在比风扇2的旋转表面更低的位置处。此外，在车体的中心部分1B处，用于驱动风扇2的驱动源3设置在座椅下方乘员座椅4的表面4b。根据这种布置，飞行装置1的重心定位在靠近车体中心下部的位置，并且从上方垂下车身正面和背面的风扇飞行。因此，飞行时车体的稳定性增加，安全性提高。版权所有（C）2005，JPO＆NCIPI

10. 发明专利

JP2004268640A Small flight apparatus 有权
公开(公告)号：JP2004268640A
公开(公告)日：2004-09-30
申请号：JP2003059125
申请日：2003-03-05
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： ISHIBA MASAJI
IPC分类号： B64C29/00 , F01K25/08 , F02C1/05
摘要： PROBLEM TO BE SOLVED: To provide a small flight apparatus which enhances fuel economy, also ensures safety and realizes application to a rescue work.
SOLUTION: The device 1 is detachably mounted to the back of a human body and is provided with a frame part 2 to be attached to the human body; and a driving force generator 3. The driving force generator 3 is provided with: a hydrogen peroxide tank 4; a pressurization gas tank 5; a catalyst 6 such as samarium silver; first and second gas turbines 7, 8 rotated by high pressure vapor generated by a reaction of hydrogen peroxide and the catalyst 6; a first variable pitch propeller 9 for hovering driven by the first gas turbine 7; a second variable pitch propeller 10 for propulsion driven by the second gas turbine 8; and a control part 11 for controlling a feed amount of the high pressure vapor and pitches of the first and second variable pitch propellers 9, 10. The high pressure vapor generated by the reaction of hydrogen peroxide and the catalyst 6 becomes thrust at the first and second variable pitch propellers 9, 10.
COPYRIGHT: (C)2004,JPO&NCIPI

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