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114 条记录 (耗时 0.014 秒)

    Tethered piston engine
    86.
    发明授权
    Tethered piston engine 有权

    公开(公告)号：US09964030B1

    公开(公告)日：2018-05-08

    申请号：US15261658

    申请日：2016-09-09

    申请人： Nolton C. Johnson, Jr.

    发明人： Nolton C. Johnson, Jr.

    IPC分类号： F02B69/00 ,  F02B61/06 ,  F02B75/18 ,  F16H19/06

    CPC分类号： F02B69/00 ,  F01B9/04 ,  F01B11/004 ,  F01B11/02 ,  F02B61/06 ,  F02B75/18 ,  F02B75/32 ,  F02B2075/1808 ,  F16H19/06 ,  F16H2019/0686

    摘要： A system including a combustion engine is disclosed. The combustion engine includes a first cylinder orientated along a first axis. The combustion engine also includes a first piston, fitted within the first cylinder, to move in reciprocating motion by alternately moving in a first linear direction along the first axis responsive to a first power stroke or a second linear direction along the first axis responsive to a second power stroke. The combustion engine includes a tensile band affixed to a first end and a second end of the first piston. The first piston is to exert a first tensile force on the tensile band in the first linear direction in response to the first power stroke. The first piston is to exert a second tensile force on the tensile band in the second linear direction in response to the second power stroke.

    PREFORMED ARTICLE FOR CYLINDER HEAD, CYLINDER HEAD, AND METHOD FOR MANUFACTURING CYLINDER HEAD
    87.
    发明申请
    PREFORMED ARTICLE FOR CYLINDER HEAD, CYLINDER HEAD, AND METHOD FOR MANUFACTURING CYLINDER HEAD 审中-公开
    气缸头，气缸头及其制造方法

    公开(公告)号：US20150322884A1

    公开(公告)日：2015-11-12

    申请号：US14649688

    申请日：2012-12-06

    申请人： Hideyuki NISHIDA

    发明人： Hideyuki NISHIDA

    IPC分类号： F02F1/24 ,  F02B69/00 ,  F02F1/42

    CPC分类号： F02F1/242 ,  F02B69/00 ,  F02B69/02 ,  F02F1/4235 ,  Y10T29/49272

    摘要： A preformed article for a cylinder head, includes: a first portion where a first through hole is to be formed from an upper wall portion to a central portion which is a portion, of a bottom wall portion, forming a combustion chamber of an internal combustion engine; and a second portion where a second through hole is to be formed to the central portion from an outer wall portion (for example, the upper wall portion) positioned above an intake port which opens to the central portion. The first portion and the second portion are portions where a cooling water passage is not formed.

    摘要翻译： 一种用于气缸盖的预制件，包括：第一部分，其第一通孔将由上壁部分形成为中心部分，该中心部分是底壁部分的形成内燃燃烧室的一部分 发动机; 以及第二部分，其中第二通孔将从位于通向中心部分的进气口上方的外壁部分（例如，上壁部分）形成到中心部分。 第一部分和第二部分是没有形成冷却水通道的部分。

    Split-cycle aircraft engine
    88.
    发明授权
    Split-cycle aircraft engine 失效
    分体式飞机发动机

    公开(公告)号：US07513224B2

    公开(公告)日：2009-04-07

    申请号：US11518828

    申请日：2006-09-11

    申请人： Clifford D. Heaton

    发明人： Clifford D. Heaton

    IPC分类号： F01B7/12

    CPC分类号： F01B17/025 ,  B64D27/24 ,  B64D2027/026 ,  F02B59/00 ,  F02B69/00 ,  Y02T50/44 ,  Y02T50/64

    摘要： A split-cycle aircraft engine includes a crankshaft rotatable about a crankshaft axis. A power piston is slidably received within a power cylinder and is operatively connected to the crankshaft such that the power piston reciprocates through an expansion stroke and an exhaust stroke during a single rotation of the crankshaft. A compression piston is slidably received within a compression cylinder and is operatively connected to the crankshaft such that the compression piston reciprocates through an intake stroke and a compression stroke during a single rotation of the crankshaft. A gas crossover passage operatively interconnects the compression cylinder and the power cylinder. An air reservoir is operatively connected to the gas crossover passage by a reservoir passage. The air reservoir is selectively operable to receive and deliver compressed air. The engine is mounted to an aircraft and the air reservoir is disposed within the aircraft.

    摘要翻译： 分体式飞机发动机包括可围绕曲轴轴线旋转的曲轴。 动力活塞可滑动地容纳在动力缸内并且可操作地连接到曲轴，使得动力活塞在曲轴的单次旋转期间通过膨胀冲程和排气冲程往复运动。 压缩活塞可滑动地容纳在压缩气缸内并且可操作地连接到曲轴，使得压缩活塞在曲轴的单次旋转期间通过进气冲程和压缩冲程往复运动。 气体交叉通道可操作地连接压缩气缸和动力气缸。 储气器通过储存器通道可操作地连接到气体交叉通道。 空气储存器可选择性地操作以接收和输送压缩空气。 发动机安装在飞行器上，空气储存器设置在飞行器内。

    SPLIT-CYCLE AIRCRAFT ENGINE
    89.
    发明申请
    SPLIT-CYCLE AIRCRAFT ENGINE 失效
    分体循环飞机发动机

    公开(公告)号：US20090050103A1

    公开(公告)日：2009-02-26

    申请号：US11518828

    申请日：2006-09-11

    申请人： Clifford D. Heaton

    发明人： Clifford D. Heaton

    IPC分类号： F02B19/18

    CPC分类号： F01B17/025 ,  B64D27/24 ,  B64D2027/026 ,  F02B59/00 ,  F02B69/00 ,  Y02T50/44 ,  Y02T50/64

    摘要： A split-cycle aircraft engine includes a crankshaft rotatable about a crankshaft axis. A power piston is slidably received within a power cylinder and is operatively connected to the crankshaft such that the power piston reciprocates through an expansion stroke and an exhaust stroke during a single rotation of the crankshaft. A compression piston is slidably received within a compression cylinder and is operatively connected to the crankshaft such that the compression piston reciprocates through an intake stroke and a compression stroke during a single rotation of the crankshaft. A gas crossover passage operatively interconnects the compression cylinder and the power cylinder. An air reservoir is operatively connected to the gas crossover passage by a reservoir passage. The air reservoir is selectively operable to receive and deliver compressed air. The engine is mounted to an aircraft and the air reservoir is disposed within the aircraft.

    摘要翻译： 分体式飞机发动机包括可围绕曲轴轴线旋转的曲轴。 动力活塞可滑动地容纳在动力缸内并且可操作地连接到曲轴，使得动力活塞在曲轴的单次旋转期间通过膨胀冲程和排气冲程往复运动。 压缩活塞可滑动地容纳在压缩气缸内并且可操作地连接到曲轴，使得压缩活塞在曲轴的单次旋转期间通过进气冲程和压缩冲程往复运动。 气体交叉通道可操作地连接压缩气缸和动力气缸。 储气器通过储存器通道可操作地连接到气体交叉通道。 空气储存器可选择性地操作以接收和输送压缩空气。 发动机安装在飞行器上，空气储存器设置在飞行器内。