公开(公告)号：US3332389A

公开(公告)日：1967-07-25

申请号：US56025766

申请日：1966-06-24

Applicant: VELDHUIZEN JOHN VAN ,  VELDHUIZEN EDNA M VAN

Inventor： VELDHUIZEN JOHN VAN ,  VELDHUIZEN EDNA M VAN

IPC: B60V1/00 ,  B60V1/04 ,  B63B1/38 ,  B63H7/00 ,  B63H11/12

CPC classification number: B60V1/046 ,  B63B1/38 ,  B63H7/00 ,  B63H11/12 ,  Y02T70/122

公开(公告)号：US3259097A

公开(公告)日：1966-07-05

申请号：US38169364

申请日：1964-07-10

Applicant: VELDHUIZEN JOHN VAN ,  VELDHUIZEN EDNA M VAN

Inventor： VELDHUIZEN JOHN VAN ,  VELDHUIZEN EDNA M VAN

IPC: B60V1/14 ,  B63H7/00 ,  B63H11/12

CPC classification number: B63H7/00 ,  B60V1/14 ,  B63B1/38 ,  Y02T70/122

公开(公告)号：US10967936B1

公开(公告)日：2021-04-06

申请号：US17002631

申请日：2020-08-25

Applicant: Borja Rodriguez Guevara

Inventor： Borja Rodriguez Guevara

IPC: B63B1/38 ,  B63B1/34 ,  B63H1/30 ,  B63B32/50 ,  B63B1/40 ,  B63H7/00

Abstract: A watercraft system including one or more air passageways and/or one or more water passageways is provided. The air passageways may extend from an upper surface of the watercraft, through the body of the watercraft, to an underneath surface of the watercraft. The water passageways may extend from an underneath forward or side portion on the watercraft, through the body of the watercraft, to a rear portion of the watercraft. The air and/or water passageways may be constricting from the inlets to the outlets so that the air and/or water is accelerated through the passageways during use of the craft. In this way, the release of the accelerated air and/or water decreases the craft's drag and provides the craft a forward thrust.

公开(公告)号：US10435129B1

公开(公告)日：2019-10-08

申请号：US16103142

申请日：2018-08-14

Applicant: John F. Corcoran

Inventor： John F. Corcoran

IPC: B63H21/16 ,  B63H16/08 ,  B63H7/00 ,  B63H21/165 ,  B63H1/14 ,  B63H19/00 ,  F15B1/26 ,  F01B23/04 ,  F04D25/06 ,  F04D25/08 ,  B63H21/21

Abstract: A watercraft comprising a compressed air propulsion system is shown and described. The watercraft includes at least one propeller operatively connected to an air motor. Storage tanks supply compressed air having a pressure of at least 2000 psi to a pressure regulator that reduces the pressure and supplies air to an air control valve. User controls adjust the air control valve to adjust the flow rate of air to the air motor which in turn adjusts the direction and/or speed of rotation of the propeller. An on-board air compressor energized by a plurality of lithium iron phosphate batteries provides air to the air storage tanks when the pressure falls below a specified value. In certain examples, the electric and air propulsion system is used to replace a fossil fuel engine in an existing watercraft and can remain at sea longer than the existing watercraft.

公开(公告)号：US10106234B2

公开(公告)日：2018-10-23

申请号：US15328037

申请日：2015-06-25

Applicant: Yu Lee Tan

Inventor： Yu Lee Tan

IPC: B63H7/02 ,  B63H7/00 ,  B63B1/18 ,  B63B1/32 ,  B63B3/48 ,  B63B7/00 ,  B63B17/00 ,  B63H25/38

Abstract: The invention is an air propelled boat that has a triangular shaped hydroplaning monohull which has surface adhesion characteristics by means of a concave bottom hull. The invention also has aircraft-like control surfaces (5,6) for safety and control at high speeds. The invention is the only monohull marine craft which produces aerodynamic lift without wings and has air based propulsion (4), air based control surfaces and a unique concave planing hull.

公开(公告)号：US09162736B2

公开(公告)日：2015-10-20

申请号：US14063591

申请日：2013-10-25

Applicant: Ronald J. Thibodaux

Inventor： Ronald J. Thibodaux

IPC: B63H7/00 ,  B63B35/44 ,  B66C23/61 ,  B63B35/00 ,  B63H7/02 ,  B66C23/60 ,  B66F11/04 ,  B60F3/00

CPC classification number: B63H7/02 ,  B60F3/0007 ,  B63B27/06 ,  B63B35/00 ,  B63B35/44 ,  B66C23/605 ,  B66F11/044 ,  Y02T70/121

Abstract: A wide, flat-bottom, buoyant, amphibious hull with a powered articulating member mounted on the deck. The hull has a shallow draft and distributes its weight over a large area and is propelled by at least one engine-driven propeller rotating above the hull. These features cooperatively provide a vehicle capable of performing overhead work, such as installing or servicing power transmission poles, towers, or other structures located in environmentally sensitive wetlands, swamps, marshes, shallow water, or terrain which is not efficiently accessible by other means.

Abstract translation: 一个宽阔的平底，浮力，两栖船体，安装在甲板上的动力铰接构件。 船体具有较浅的通风并在大面积上分配其重量，并且由至少一个在船体上方旋转的发动机驱动的螺旋桨推动。 这些特征协同地提供能够执行高架作业的车辆，例如安装或维修位于环境敏感的湿地，沼泽，沼泽，浅水或其他方式无法有效访问的地形中的输电杆，塔或其他结构。

公开(公告)号：US20150072578A1

公开(公告)日：2015-03-12

申请号：US14466100

申请日：2014-09-12

Applicant: Carl Stone ,  William Gremminger ,  Emil Hasl

Inventor： Carl Stone ,  William Gremminger ,  Emil Hasl

IPC: B63H21/36 ,  B63H21/30 ,  B63H7/00

CPC classification number: B63H21/36 ,  B63H7/00 ,  B63H21/30 ,  F16J3/042

Abstract: A bellows for protecting a U-joint in a marine stern drive includes a flexible, hollow body defining an interior space and open at opposite ends, the body formed of a thermoplastic elastomer material to be self-supporting, having a first mating end and a second mating end and being pleated therebetween, a first sealing cuff formed of an elastomeric material, softer than the thermoplastic elastomer material, bonded to the first mating end and, a second sealing cuff formed of an elastomeric material, softer than the thermoplastic elastomer material, bonded to the second mating end.

Abstract translation: 用于保护海底船尾驱动器中的U形接头的波纹管包括限定内部空间并在相对端开口的柔性空心体，所述主体由热塑性弹性体材料形成，以自支撑，具有第一配合端和 第二配合端并且在其间被打褶，由弹性体材料形成的第一密封箍，比热塑性弹性体材料柔软，结合到第一配合端，以及由弹性体材料形成的比热塑性弹性体材料柔软的第二密封箍， 结合到第二配合端。

公开(公告)号：US20130224031A1

公开(公告)日：2013-08-29

申请号：US13437476

申请日：2012-04-02

Applicant: Andrew Breeze-Stringfellow ,  Manampathy Gangadharan Giridharan ,  Syed Arif Khalid ,  Leroy H. Smith, JR.

Inventor： Andrew Breeze-Stringfellow ,  Manampathy Gangadharan Giridharan ,  Syed Arif Khalid ,  Leroy H. Smith, JR.

IPC: B63H7/00

CPC classification number: B64C11/18 ,  F01D5/141 ,  Y02T50/66

Abstract: An airfoil section of a propeller for a propulsion device includes a pressure surface and a suction surface, the pressure surface and suction surface intersecting at a leading edge and a trailing edge. The airfoil section has a meanline defined midway between the pressure surface and the suction surface and a meanline angle is defined as an angle between a tangent to the meanline and a centerline of the propeller. The blade has a meanline curvature defined as the slope of a meanline angle with respect to chord fraction along the meanline, and at least a portion of the meanline has a meanline curvature that increases from between approximately 0.1 chord fraction progressing toward the leading edge and at least a portion of the meanline has a meanline curvature that decreases from between approximately 0.1 chord fraction progressing toward the leading edge.

Abstract translation: 用于推进装置的推进器的翼型部分包括压力表面和吸力表面，压力表面和吸力表面在前缘和后缘相交。 翼型部分具有限定在压力表面和吸力表面之间的中间线的平均线，并且平均线角度被定义为在平均线的切线和螺旋桨的中心线之间的角度。 叶片的平均曲率被定义为相对于平均线的和弦分数的平均线角度的斜率，并且平均线的至少一部分具有从大约0.1个弦分数前进到前缘和 平均线的至少一部分具有从大约0.1个弦分数向前缘前进的平均曲率减小。

公开(公告)号：US08313298B2

公开(公告)日：2012-11-20

申请号：US12160333

申请日：2007-01-26

Applicant: Günter Berger ,  Gerhard Bauer

Inventor： Günter Berger ,  Gerhard Bauer

IPC: A47C7/74 ,  A47C21/04 ,  B63H1/00 ,  B63H3/00 ,  B63H5/00 ,  B63H7/00 ,  B63H13/00 ,  B63H15/00 ,  B64C11/00 ,  B64C27/00 ,  F01D25/00 ,  F03B3/12

CPC classification number: F03D15/10 ,  F03D15/00 ,  F03D80/00 ,  F03D80/70 ,  F05B2240/50 ,  Y02E10/72

Abstract: A drive train between a rotor and a transmission having a torque support for a wind turbine generator system, including a rotor shaft extending from the rotor and supported in this area by a first rotor shaft bearing and extending to the transmission for converting the rotor speed into a desired generator speed, wherein the rotor shaft is supported by a second rotor shaft bearing formed in the manner of a moment bearing which is arranged on the input side within the transmission in order to receive the partial rotor forces, moments and weight forces and to directly pass them on to the torque support.

Abstract translation: 一种转子和变速器之间的传动系，其具有用于风力涡轮发电机系统的转矩支撑，包括转子轴，该转子轴从转子延伸并由第一转子轴轴承支撑在该区域中并延伸到变速器，以将转子转速转换成 期望的发电机速度，其中转子轴由第二转子轴承支撑，该第二转子轴轴承以轴承的方式形成，所述转矩轴承布置在变速器内的输入侧，以便接收部分转子力，力矩和重力，并且 直接传递给转矩支持。

公开(公告)号：US08210824B1

公开(公告)日：2012-07-03

申请号：US12187967

申请日：2008-08-07

Applicant: John C. Bucher ,  Brian Keith Love

Inventor： John C. Bucher ,  Brian Keith Love

IPC: B63H7/00 ,  F04B53/00 ,  F04B39/00

CPC classification number: F04B33/00 ,  F04D19/002 ,  F04D29/646 ,  F04D29/703 ,  Y10T29/49815 ,  Y10T29/49819 ,  Y10T29/49947

Abstract: Methods, devices, systems and apparatus of fully knock-down drum fans that can be shipped completely unassembled so that the smallest packaging is used resulting in more units per container and a lower shipping cost per unit. This allows overseas manufacturers to be more competitive with local manufactures. This is achieved through a drum fan design that utilizes completely modular components that can be assembled quickly and easily either by the distributor of the drum fan or the final end user. A drum fan can include a plural identical shroud curved members, with the same number of pie shaped front grill members, and the same number of pie shaped rear grill members, as well as other modular components that are both easy to nest, pack, store and ship with one another. The knock-down fan will significantly reduce packaging size from approximately 50 to approximately 75% less than current drum fans. The knock-down fan is easy to re-assemble, because of modular components, and the knock-down fan size can be applied to any size drum fan from approximately 24″, 36″, and 42″ up to approximately 60″ in diameter.

Abstract translation: 完全敲击滚筒风扇的方法，设备，系统和设备，可以完全拆卸，以便使用最小的包装，导致每个集装箱更多的单位，并降低每单位的运输成本。 这允许海外制造商与当地制造商更具竞争力。 这是通过鼓风机设计实现的，其利用完全模块化的组件，其可以由鼓风扇的分配器或最终终端用户快速且容易地组装。 鼓风扇可以包括多个相同的护罩弯曲构件，具有相同数量的饼形前格栅构件，以及相同数量的饼形后格栅构件，以及其他模块化构件，其易于嵌套，包装，存储 并相互交船。 击倒式风扇将大大减少包装尺寸从现有的鼓风机的50％降低到大约75％。 由于模块化部件，拆卸式风扇易于重新组装，并且拆卸风扇尺寸可应用于直径约24“，36”和42“直径约60”的任何尺寸的鼓风机 。