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    • 3. 发明授权
    • Pulse detonation engine and valve
    • 脉冲爆震发动机和阀门
    • US07251928B2
    • 2007-08-07
    • US11061546
    • 2005-02-18
    • Takayuki KojimaTetsuya SatoHiroaki Kobayashi
    • Takayuki KojimaTetsuya SatoHiroaki Kobayashi
    • F02K7/06F02K7/20
    • F02K9/805F02K7/06F23C15/00F23R7/00
    • Pressure and density of a gaseous mixture are increased in the process of introducing the gaseous mixture into the combustor of an air-breathing pulse detonation engine employing atmospheric oxygen as an oxidizer. The exit valve 20 able to be opened and closed is provided at the outlet of the combustor 15, an air cooler 12 is provided in the exit of the intake, and density is increased by exchange of heat of the air received at the intake with a coolant in the air cooler 12. Furthermore, by closing the exit valve 20 provided in the outlet of the combustor during the process of loading the gaseous mixture, transition to the detonation process is possible without expansion of the high-pressure high density air obtained by ram-compression at the intake.
    • 在将气体混合物引入使用大气氧气作为氧化剂的空气呼吸脉冲爆震引擎的燃烧器的过程中,气体混合物的压力和密度增加。 能够打开和关闭的出口阀20设置在燃烧器15的出口处,空气冷却器12设置在进气口的出口处,并且通过将在入口处接收的空气的热量与 空气冷却器12中的冷却剂。 此外,通过在装载气体混合物的过程中关闭设置在燃烧器的出口中的出口阀20,可以不引起在进气口处由压头压缩而获得的高压高密度空气的膨胀而过渡到爆震过程。
    • 4. 发明授权
    • Method for reducing resistance of flying object using expandable nose cone
    • 使用可伸缩鼻锥降低飞行物体阻力的方法
    • US07118072B2
    • 2006-10-10
    • US11037125
    • 2005-01-19
    • Hiroaki KobayashiNobuhiro TanatsuguTetsuya SatoMotoyuki HongoYusuke Maru
    • Hiroaki KobayashiNobuhiro TanatsuguTetsuya SatoMotoyuki HongoYusuke Maru
    • B64C1/38
    • F42B10/46F42B12/105
    • It is an object of the present invention to provide a flying object using a thin elongated nose cone with a small tip angle for reducing the air resistance during flying, wherein the maximum loading capacity can be increased without decreasing the volume efficiency of the flying object by limitations placed on the accommodation space, regardless of the structure thereof.In the flying object in accordance with the present invention, which comprises a nose cone in the tip portion, the nose cone portion has a compressed structure in the axial direction during accommodation and expands on the tip side in the axial direction during flying, due to an expandable nose cone structure such that a disk with a small diameter is disposed in the forward position and the disks with a successively increasing diameter are disposed in the axial direction. After separation, the nose cone expands in the axial direction, deep cavities are formed between the disks, and a fine elongated nose cone with a small tip angle is provided, whereby the air resistance is reduced.
    • 本发明的目的是提供一种飞行物体,其使用具有小尖角的细长鼻锥,以减少飞行期间的空气阻力,其中可以增加最大承载能力,而不会降低飞行物体的体积效率 不管其结构如何,对住宿空间的限制。 在根据本发明的飞行物体中,其包括尖端部分中的鼻锥,鼻锥部在调节期间在轴向方向上具有压缩结构,并且在飞行期间在轴向方向上的尖端侧膨胀,由于 可扩展的鼻锥结构,使得具有小直径的盘被设置在向前位置,并且具有连续增加的直径的盘沿轴向设置。 分离后,鼻锥在轴向上膨胀,在圆盘之间形成深空腔,并提供具有小尖角的细长鼻锥,由此减小空气阻力。
    • 5. 发明申请
    • Method for reducing resistance of flying object using expandable nose cone
    • 使用可伸缩鼻锥降低飞行物体阻力的方法
    • US20050269454A1
    • 2005-12-08
    • US11037125
    • 2005-01-19
    • Hiroaki KobayashiNobuhiro TanatsuguTetsuya SatoMotoyuki HongoYusuke Maru
    • Hiroaki KobayashiNobuhiro TanatsuguTetsuya SatoMotoyuki HongoYusuke Maru
    • F42B10/46F42B12/10B64C1/00
    • F42B10/46F42B12/105
    • It is an object of the present invention to provide a flying object using a thin elongated nose cone with a small tip angle for reducing the air resistance during flying, wherein the maximum loading capacity can be increased without decreasing the volume efficiency of the flying object by limitations placed on the accommodation space, regardless of the structure thereof. In the flying object in accordance with the present invention, which comprises a nose cone in the tip portion, the nose cone portion has a compressed structure in the axial direction during accommodation and expands on the tip side in the axial direction during flying, due to an expandable nose cone structure such that a disk with a small diameter is disposed in the forward position and the disks with a successively increasing diameter are disposed in the axial direction. After separation, the nose cone expands in the axial direction, deep cavities are formed between the disks, and a fine elongated nose cone with a small tip angle is provided, whereby the air resistance is reduced.
    • 本发明的目的是提供一种飞行物体,其使用具有小尖角的细长鼻锥,以减少飞行期间的空气阻力,其中可以增加最大承载能力,而不会降低飞行物体的体积效率 不管其结构如何,对住宿空间的限制。 在根据本发明的飞行物体中,其包括尖端部分中的鼻锥,鼻锥部在调节期间在轴向方向上具有压缩结构,并且在飞行期间在轴向方向上的尖端侧膨胀,由于 可扩展的鼻锥结构,使得具有小直径的盘被设置在向前位置,并且具有连续增加的直径的盘沿轴向设置。 分离后,鼻锥在轴向上膨胀,在圆盘之间形成深空腔,并提供具有小尖角的细长鼻锥,由此减小空气阻力。
    • 7. 发明申请
    • SHAFT SEAL APPARATUS
    • 轴封装置
    • US20140232070A1
    • 2014-08-21
    • US13983331
    • 2012-05-18
    • Yoshiaki TakigahiraYoji OshiiAtsushi KanekoTetsuya Sato
    • Yoshiaki TakigahiraYoji OshiiAtsushi KanekoTetsuya Sato
    • F16J15/34
    • F16J15/3404F16J15/3484F16J15/406
    • A pumping ring 46 producing an axial flow of sealed flow is secured to a rotary shaft 6 at an axial position different from a rotary ring 56 so that the sealed fluid positioned in the sealed space 33 flows along the axial direction of the rotary shaft 6. A discharge hole 14 is formed on an inner circumferential surface of a seal cover 8 positioned in the downstream side of the axial flow of the sealed fluid resulting from a rotation of the pumping ring 46. An inflow hole 15 is formed in the upstream side of the axial flow of the sealed fluid resulting from the rotation of the pumping ring 46, so that the sealed fluid discharged from the discharge hole 14 returns to the inside of the sealed space from the inflow hole 15. On the inner circumferential surface of the seal cover 8 provided with the discharge hole 14, a baffle member 18 is provided so that it protrudes radially inward in order to block the flow of the sealed fluid along the rotating direction of a retainer 52 and orient the sealed fluid toward the discharge hole 14.
    • 产生密封流动的轴向流动的泵送环46在不同于旋转环56的轴向位置处固定到旋转轴6,使得位于密封空间33中的密封流体沿着旋转轴6的轴向流动。 在位于密封流体的轴向流动的下游侧的密封盖8的内周面上形成有排出孔14,该密封流体由泵送环46的旋转而产生。在流入孔15的上游侧形成有流入孔15 密封流体由泵送环46的旋转引起的轴向流动,使得从排出孔14排出的密封流体从流入孔15返回到密封空间的内部。在密封件的内周面上 设置有排放孔14的盖8设置有挡板构件18,以便径向向内突出,以阻挡密封流体沿着保持器52的旋转方向的流动, 密封流体朝向排出孔14。
    • 8. 发明授权
    • Information processing apparatus and method for transferring settings information
    • 用于传送设置信息的信息处理设备和方法
    • US08760686B2
    • 2014-06-24
    • US12703060
    • 2010-02-09
    • Tetsuya Sato
    • Tetsuya Sato
    • G06F3/12
    • G06F3/1285G06F3/1204G06F3/1205G06F3/1209G06F3/1225G06F3/1257G06F3/1286
    • A situation can occur in which the seating location of a user is moved due to personnel changes within a division or the like, and the user has to use a different nearby image forming apparatus. In such a case, with conventional technology, it is not possible to efficiently transfer the settings information used in an image forming apparatus used before the personnel change to the new nearby image forming apparatus. According to the present invention, when an instruction to register an image forming apparatus is made in an application by the user, settings information set by the user is searched for in the image forming apparatuses that are registered in the application and the image forming apparatuses that were deleted from the application in the past, and they are presented as transfer candidates.
    • 可能发生用户的座位位置由于分区等内的人员变化而移动的情况,并且用户必须使用不同的附近图像形成装置。 在这种情况下,利用传统技术,不可能将在人员改变之前使用的图像形成装置中使用的设置信息有效地传送到新的附近图像形成装置。 根据本发明,当在用户的应用中进行注册图像形成装置的指示时,在登记在应用程序中的图像形成装置和图像形成装置中搜索由用户设置的设置信息, 从过去的应用程序中删除,并将其作为转移候选者。