公开(公告)号：US3983833A

公开(公告)日：1976-10-05

申请号：US552127

申请日：1975-02-21

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: B63B1/24 ,  B63B35/50 ,  B63H23/26 ,  B64D35/00 ,  B63H5/08

CPC classification number: B64D35/00 ,  B63B1/246 ,  B63B35/50 ,  B63H23/26

Abstract: An air, water, or land vehicle has a body adapted to travel in a normal direction of travel and having a pair of forwardly directed propellers symmetrically spaced to each side of the centerline of the vehicle and each carried on a respective fluid motor. An engine on the vehicle drives at least one pump having two independent working chambers each of whose output is connected to the input of a respective one of the propeller-carrying motors and an adjustment is provided for increasing the discharge rate of the one pump relative to the other and vice versa for steering the vehicle.

公开(公告)号：US3960060A

公开(公告)日：1976-06-01

申请号：US487271

申请日：1974-07-10

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: F03C1/38 ,  F04B1/04 ,  F01B1/00

CPC classification number: F04B1/0465 ,  F03C1/0444

Abstract: A pressure responsive control body in the housing of a fluid handling device has a control face which abuts against the control face at one axial end of a rotor which is provided with working chambers for the inflow and expulsion of a fluid. A portion of the control body extends into a pressure chamber of the housing and the control body is movable axially of the housing. The control body seals a portion of the pressure chamber by means of an eccentrically located cylindrical shoulder a portion of which extends radially beyond the control face. This insures that the position of the pressure center of the eccentric shoulder relative to the axis of the rotor is the same as the position of the pressure center between the control faces. Such positioning of the pressure centers guarantees a smooth running of the control face on the rotor relative to the control face on the control body and prevents relative tilting or adherence of the control faces to each other so that the control mirror between the control faces operates with a high degree of efficiency even at high fluid pressures and at a high RPM of the rotor.

Abstract translation: 在流体处理装置的壳体中的压力响应控制体具有控制面，该控制面在转子的一个轴向端处抵靠控制面，该转子具有用于流体流入和排出的工作室。 控制体的一部分延伸到壳体的压力室中，并且控制体可在壳体的轴向移动。 控制体通过偏心定位的圆柱形肩部密封压力室的一部分，其一部分径向延伸超过控制面。 这确保偏心肩部的压力中心相对于转子轴线的位置与控制面之间的压力中心的位置相同。 压力中心的这种定位保证了转子上的控制面相对于控制体上的控制面的顺利运行，并且防止控制面相对倾斜或粘附到彼此之间，使得控制面之间的控制反射镜与 即使在高流体压力和转子的高RPM下也具有高效率。

公开(公告)号：US3949648A

公开(公告)日：1976-04-13

申请号：US466246

申请日：1974-05-02

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: F03C1/24 ,  F01B1/06 ,  F01B13/06 ,  F03C1/247 ,  F03C1/28 ,  F04B1/10 ,  F04B1/107 ,  F04B1/113 ,  F16J1/14

CPC classification number: F01B13/065 ,  F01B1/0644

Abstract: A rotor is rotatably mounted in a housing and formed with angularly spaced radially oriented cylinder bores in each of which a piston is radially reciprocable. The radially outer end of each piston is formed with an inwardly extending recess having a length greater than the length of the piston stroke. A control ring which is eccentric relative to the rotor surrounds the latter, and its inner circumferential surface is slidingly contacted by respective piston shoes each of which is associated with one of the pistons and each of which has a shaft that is freely received in the recess of the associated piston and whose length is also greater than the length of the piston stroke.

Abstract translation: 转子可旋转地安装在壳体中并且形成有角度间隔开的径向取向的气缸孔，其中活塞可径向往复运动。 每个活塞的径向外端形成有具有大于活塞冲程长度的长度的向内延伸的凹部。 相对于转子偏心的控制环围绕转子环绕其内圆周表面与相应的活塞鞋滑动接触，每个活塞与活塞中的一个相关联，并且每个活塞具有自由接收在凹部中的轴 并且其长度也大于活塞行程的长度。

公开(公告)号：US5109666A

公开(公告)日：1992-05-05

申请号：US313673

申请日：1989-02-22

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: F01B1/06 ,  F01B3/00 ,  F01B29/04 ,  F01L7/02 ,  F01L33/02 ,  F01L33/04 ,  F02B1/04 ,  F02B3/06 ,  F02B41/06 ,  F02B45/02 ,  F02F3/28 ,  F02G3/02 ,  F04B53/10

CPC classification number: F02B45/02 ,  F01B1/0603 ,  F01B1/062 ,  F01B1/0668 ,  F01B29/04 ,  F01B3/0076 ,  F01L33/02 ,  F01L33/04 ,  F01L7/02 ,  F02B41/06 ,  F02F3/28 ,  F02G3/02 ,  F04B53/1022 ,  F04B53/103 ,  F04B53/109 ,  F02B1/04 ,  F02B3/06 ,  Y02T10/34

Abstract: A solid fuel preferred to be prepared from cleaned and pressed coal powder to a high density is led into a combustion chamber. Air is compressed to a high temperature which exceeds the self ignition temperature of the mentioned solid fuel. This compressed air is also led into the combustion chamber to meet there the tip of the solid fuel sheet and to ignite and burn the fuel in the hot air in the combustion chamber. The hot burned gas can then be led into an expander and the expander can drive a compressor for the supply of the mentioned hot air. The device then forms a combustion engine with continuous combustion in an external combustion chamber. In my parental U.S. Pat. No. 4,809,503 the solid fule is a fuel bar. This present application deals mainly with a solid fuel sheet or tape which is wider than it is thick. Thereby it is secured that the fuel portions meet exactly the required amounts of hot air locally at a wide meeting and burning place.

Abstract translation: 优选由清洁和压制的煤粉制备成高密度的固体燃料被引入燃烧室。 空气被压缩到高于所述固体燃料的自燃温度的高温。 该压缩空气也被引入到燃烧室中以在那里与固体燃料片的尖端相接触并点燃和燃烧燃烧室中的热空气中的燃料。 然后将热的燃烧气体引入膨胀器中，并且膨胀器可驱动压缩机供应所述热空气。 然后，该装置在外部燃烧室中形成具有连续燃烧的内燃机。 在我父母的美国专利 第4,809,503号固体是燃料棒。 本申请主要涉及比较粗的固体燃料片或带。 因此，确保燃料部分在广泛的会议和燃烧场所局部地满足所需量的热空气。

公开(公告)号：US4984970A

公开(公告)日：1991-01-15

申请号：US332319

申请日：1989-04-03

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: F04B43/00 ,  F04B43/067

CPC classification number: F04B43/0063 ,  F04B43/067

Abstract: When pumping chambers were provided between tapered discs of axial compressibility and expandability, the discs worked perfect in the subcritical pressure range. But in the supercritical pressure range the high pressure in fluid would depart the discs away from each other and open a gap between the discs because the force of pressure in fluid in the chamber between the tapered discs was higher than the internal strength of the material of which the respective coned element was made. The invention now discovers that it is possible to provide a means which prevents the departure of a coned ring from a neighbored ring. The invention obtains this by providing a means which presses under actions of pressure in surrounding fluid the neighboring coned ring elements at all times together for a close and perfect sealing between them. This means which the invention now discloses is the provision of seals radially inwards and outwards of a defined radial dimension of a meeting area between two neighborings discs of a respective pair of coned ring elements. The radial extension of the meeting area defines the force with which the neighboring elements are pressed against each other for a close sealing procedure. The elements are produced from respective material, for example, from hardened stainless steel.

Abstract translation: 当在轴向压缩性和可扩展性的锥形盘之间设置泵送室时，盘在亚临界压力范围内工作良好。 但是在超临界压力范围内，流体中的高压将使盘离开彼此，并且打开盘之间的间隙，因为锥形盘之间的腔室中的流体中的压力的​​力高于材料的内部强度 制成相应的锥形元件。 本发明现在发现可以提供一种防止锥形环离开相邻环的装置。 本发明通过提供一种在相邻的锥形环元件周围的压力作用下压在一起的装置，以使它们之间的密封和完美的密封。 本发明现在公开的这种方式是在相应的一对锥形环元件的两个相邻盘之间的会议区域的限定的径向尺寸内径向向内和向外设置密封件。 会议区域的径向延伸部分限定了相邻元件相互压靠的力以进行紧密的密封程序。 元件由各种材料制成，例如由硬化的不锈钢制成。

公开(公告)号：US4982914A

公开(公告)日：1991-01-08

申请号：US330668

申请日：1989-03-30

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: B64C11/28 ,  B64C27/04 ,  B64C27/12 ,  B64C29/00 ,  B64D27/24 ,  B64D31/14 ,  B64D35/00 ,  F02B75/02

CPC classification number: B64D35/00 ,  B64C11/28 ,  B64C27/12 ,  B64C29/00 ,  B64C29/0016 ,  B64D27/24 ,  B64D31/14 ,  B64C2700/6281 ,  F02B2075/025 ,  Y02T50/44 ,  Y02T50/62

Abstract: An aircraft has a pair of wing portions with propellers of a propeller pair which are driven and synchronized by a fluid transmission between the power plant and the propellers. A fluid line structure keeps most components of the craft together and consists preferredly of three pipes which are also utilized to carry the driving fluid to and from the motors, to hold the motors and to hold the wings. The take over of a plurality of functions by the interior pipe structure reduces weight and secures safe and economic operation of the craft. The pipe structure can be pivoted in respective bearings to effect the pivotal movement of the propellers and wing portions for either vertical take off and landing or for horizontal flight. The pipe structure is built by pipes without bends in order to make the cleaning of the interiors of the pipes from dirt and from remainders of welding possible. Ribs and holding portions are provided on the structure for assembly and/or disassembly of the wing portions of the pipe structure.

Abstract translation: 飞机具有一对具有螺旋桨对的螺旋桨的机翼部分，其通过在发电厂和螺旋桨之间的流体传动驱动并同步。 流体管线结构将工艺的大多数部件保持在一起，并且优选地由三个管道组成，这三个管道也用于将驱动流体运送到电动机和从电动机运送驱动流体，以保持电动机并保持机翼。 通过内部管道结构接管多个功能减轻了重量并确保了工艺的安全和经济的操作。 管道结构可以在相应的轴承中枢转，以实现螺旋桨和翼部的枢转运动，用于垂直起飞和降落或用于水平飞行。 管道结构由没有弯头的管道构成，以便使管道内部的清洁从污物和焊接余地中清除。 在结构上设置有肋和保持部，用于组装和/或拆卸管结构的翼部。

公开(公告)号：US4925131A

公开(公告)日：1990-05-15

申请号：US239234

申请日：1988-09-01

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: B64C11/28 ,  B64C27/04 ,  B64C27/12 ,  B64C29/00 ,  B64D27/24 ,  B64D31/14 ,  B64D35/00 ,  F02B75/02

CPC classification number: B64D35/00 ,  B64C11/28 ,  B64C27/12 ,  B64C29/00 ,  B64D27/24 ,  B64D31/14 ,  B64C2700/6281 ,  F02B2075/025 ,  Y02T50/44 ,  Y02T50/62

Abstract: An aircraft has a pair of wing portions with propellers of a propeller pair which are driven and synchronized by a fluid transmission between the power plant and the propellers. A fluid line structure keeps most components of the craft together and consists preferredly of three pipes which are also utilized to carry the driving fluid to and from the motors, to hold the motors and to hold the wings. The take over of a plurality of functions by the interior pipe structure reduces weight and secures safe and economic operation of the craft.The pipe structure can be pivoted in respective bearings to effect the pivotal movement of the propellers and wing portions for either vertical take off and landing or horizontal flight. The pipe structure is built by pipes without bends in order to make the cleaning of the interiors of the pipes from dirt and remainders of weldings possible. Ribs and holding portions are provided on the structure for assembly and/or disassembly of the wing portions to the pipe structure.

Abstract translation: 飞机具有一对具有螺旋桨对的螺旋桨的机翼部分，其通过在发电厂和螺旋桨之间的流体传动驱动并同步。 流体管线结构将工艺的大部分组件保​​持在一起，并且优选地由三个管道组成，这三个管道也用于将驱动流体运送到电动机和从电动机运送驱动流体，以保持电动机并保持机翼。 通过内部管道结构接管多个功能减轻了重量并确保了工艺的安全和经济的操作。 管道结构可以在相应的轴承中枢转，以实现螺旋桨和翼部的枢转运动，用于垂直起飞和降落或水平飞行。 管道结构由没有弯头的管道构成，以便使管道内部的清洁成为污垢和焊接余留物。 肋和保持部分设置在结构上，用于将翼部件组装和/或拆卸到管道结构。

公开(公告)号：US4913100A

公开(公告)日：1990-04-03

申请号：US286565

申请日：1988-12-19

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: F02B25/04 ,  F02B33/08 ,  F02B37/04 ,  F02B75/02 ,  F02F7/00

CPC classification number: F02B33/08 ,  F02B25/04 ,  F02B37/04 ,  F02B2075/025 ,  F02B2075/027 ,  F02F7/006 ,  Y02T10/144

Abstract: A double piston engine has a doubly acting piston reciprocably provided in a cylinder arrangement to form two working chambers which periodically increase and decrease their volumes. The invention provides inlet means with supply means for a cleaning flow through the working chambers and inlet means and supply means for a loading flow in excess of atmospheric pressure to the respective chambers. Means are further provided to secure that the loading flow enters the respective working chamber after the closing of the inlet for the cleaning flow. By this arrangement of the invention it becomes possible to operate two cycle engines with turbo-chargers or other loaders. A very powerful engine at compact space and low weight is obtained, while the poisenous gases of two stroke engines are prevented to a high degree.

Abstract translation: 双活塞发动机具有可往复地设置在气缸装置中的双作用活塞，以形成周期性增加和减小其体积的两个工作室。 本发明提供了一种入口装置，其具有用于通过工作室和入口装置的清洁流动的供给装置和用于相对于各个室的超过大气压的负载流的供给装置。 进一步提供装置以确保在用于清洁流动的入口关闭之后装载流进入相应的工作室。 通过本发明的这种布置，可以使用涡轮增压器或其他装载机来操作两冲程发动机。 获得了紧凑的空间和低重量的非常强大的发动机，同时可以高度地防止两冲程发动机的高压气体。

公开(公告)号：US4896564A

公开(公告)日：1990-01-30

申请号：US4018

申请日：1987-01-16

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: F04B43/00 ,  F04B43/02

CPC classification number: F04B43/02 ,  F04B43/0063 ,  B64C2700/6281 ,  F02F2200/04 ,  F05C2201/021 ,  F05C2201/0448 ,  F05C2201/046

Abstract: In an axial piston motor or pump the cylinder barrel is mounted on a medial shaft which has a shoulder which axially bears against the front end of the rotor barrel. The rear end of the medial shaft is radially borne in a housing portion. The front portion of the medial shaft is provided with a bearing member of an axial thrust bearing for support on a respective axial thrust bearing member in the housing. On the rear end of the rotary barrel an axially selfthrusting control body is provided to seal the flow of fluid to and from the cylinders of the rotary barrel. The control body presses against the rotary barrel, the rotary barrel presses against the shoulder of the medial shaft and the thrust bearing member of the shaft bears on the thrust bearing member of the housing. As a result thereof the cylinders in the rotary barrel can be straight through bores. The manufacturing of the rotor barrel is thereby simplified and the flow acceleration losses of former bore type cylinders are prevented.

Abstract translation: 在轴向活塞马达或泵中，缸筒安装在内侧轴上，该内侧轴具有轴向地抵靠转子筒的前端的肩部。 内侧轴的后端径向地承载在壳体部分中。 内侧轴的前部设置有用于支撑在壳体中的相应的轴向推力轴承构件上的轴向推力轴承的轴承构件。 在旋转筒的后端，提供轴向自调控制体以密封流体流向和从旋转筒的圆筒的流动。 控制体压靠旋转筒，旋转筒压靠在内侧轴的肩部上，轴的止推轴承部件承载在壳体的止推轴承部件上。 结果，旋转筒中的圆筒可以是直通孔。 因此，转子筒的制造被简化，并且防止了前孔型气缸的流动加速损失。

公开(公告)号：US4815275A

公开(公告)日：1989-03-28

申请号：US124534

申请日：1987-11-16

Applicant: Karl Eickmann

Inventor： Karl Eickmann

IPC: F01L1/28 ,  F01L9/02 ,  F02B75/02 ,  F02G3/02

CPC classification number: F01L1/285 ,  F01L9/02 ,  F02G3/02 ,  F02B2075/027

Abstract: A combustion engine has a combustion chamber separated from the compression and expansion chamber(s). Passages are provided between the combustion chamber and the compression chamber(s) and the combustion chamber and the expansion chamber(s) with respective valves in the passages and inlet and exhaust valves provided in the combustion and expansion chamber. The combustion chamber maintains the combustion after passing fuel into the compressed air received from the compression chamber. The valves and piston heads are formed to prevent dead space in the cylinders in order to obtain a good efficiency by full discharge of the compressed air into the combustion chamber. Fuel cleaning means like, for example, a rotary separator and pure gas collecter are provided in the combustion chamber to separate unclean fuel particles, as, for example, ash or sand in coal, from the burned gases and collect the unclean particles in separated collection spaces. The engine can thereby burn unclean fuels, as for example coal powder or coal sludge and the like. The valves can be timed for different styles of combustion cycles if so desired. The engine may use conventional four stroke or two stroke engine arrangements and provide them with combustion chambers, pistons and cylinder heads of the invention to modify them from gasoline combustion to coal combustion or other cheaper and more avialable fuels for the combustion in the compressed air.

Abstract translation: 内燃机具有与压缩和膨胀室分离的燃烧室。 在燃烧室和压缩室之间提供通道，燃烧室和膨胀室具有设置在燃烧和膨胀室中的通道和入口和排气门中的相应阀。 燃烧室在将燃料送入从压缩室接收的压缩空气中之后维持燃烧。 形成阀和活塞头以防止气缸中的死区，以通过将压缩空气全部排出到燃烧室中来获得良好的效率。 在燃烧室中设置有例如旋转分离器和纯气体收集器的燃料清洁装置，以将不清洁的燃料颗粒，例如煤中的灰分或沙子与燃烧的气体分离，并收集分离的收集物中的不洁颗粒 空格 因此，发动机可以燃烧不洁净的燃料，例如煤粉或煤泥等。 如果需要，这些阀门可以定时处理不同风格的燃烧循环。 发动机可以使用传统的四冲程或二冲程发动机装置，并为它们提供本发明的燃烧室，活塞和气缸盖，以将它们从汽油燃烧改变为煤燃烧，或者用于燃料在压缩空气中燃烧的其它更便宜和更可利用的燃料。