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    • 3. 发明申请
    • ROTARY INTERNAL COMBUSTION ENGINE WITH ANNULAR CHAMBER
    • 旋转室内燃烧发动机
    • WO2008121082A1
    • 2008-10-09
    • PCT/SK2007/000008
    • 2007-09-26
    • VARGA, Peter
    • VARGA, Peter
    • F01C1/20F01C3/02
    • F01C1/20F01C3/02
    • The rotary nasal annular engine with noses on the annular with internal combustion operates on the principle of a pair of the first rotor (1 ) and the second rotor (2), as well as with usage of a block (3), where the rotors are placed and rotate synchronously. The block (3), together with the circumference surface (1.9), nose (1.2), (1.3) of the rotor (1 ) and the rotor (2) determinates the engine's combustion chamber (4.1 ), (4.2) in the shape of a torus, inside of which the rotor (1 ) is rotating with at least one nose (1.2). The rotor (2), contains, on its outer circumference surface (2.9), slots (2.7, 2.8), preferably, on its outer circumference surface, for the transition of the nose (1.2). During the nose's (1.2) transition through the slot (2.7), of the rotor (2), the compressed medium (7) is transferred through the storage system (2.5) of the rotor (2) through its intake opening (2.4) of the rotor (2) and through the outgoing opening (2.6) of the rotor (2) into the engine's combustion chamber (4.2)
    • 具有内燃环形的鼻部的旋转鼻环形发动机以一对第一转子(1)和第二转子(2)的原理运行,以及使用块(3),其中转子 被放置并同步旋转。 转子(1)和转子(2)的块体(3)与转子(1)和转子(2)的圆周表面(1.9),鼻部(1.2),(1.3)一起确定发动机的燃烧室(4.1),(4.2) 其中转子(1)内有至少一个鼻(1.2)旋转。 转子(2)在其外圆周表面(2.9)上,优选地在其外圆周表面上包含用于鼻部(1.2)的过渡的狭槽(2.7,2.8)。 在通过转子(2)的槽(2.7)的鼻部(1.2)过渡期间,压缩介质(7)通过转子(2)的储存系统(2.5)通过其转子(2)的进气口(2.4)传递 转子(2)并通过转子(2)的出口(2.6)进入发动机的燃烧室(4.2)
    • 4. 发明申请
    • MULTIPLE ROD SYSTEM WITH ELASTIC ROD-CONTAINING MEANS
    • 具有弹性夹心装置的多杆系统
    • WO2008016892A2
    • 2008-02-07
    • PCT/US2007/074789
    • 2007-07-31
    • WARSAW ORTHOPEDIC, INC.VARGA, PeterNAYET, JeromeGOURNAY, Jose
    • VARGA, PeterNAYET, JeromeGOURNAY, Jose
    • A61B17/70
    • A61B17/7032A61B17/7037
    • Bone-anchoring element, such as a screw (1), for a device for correcting deformations of the spine, which is intended to be implanted on a vertebra (3) and whose head (4) comprises a receptacle (11) for one or more rods (5-10) of said device, with a channel (13) which opens out on the upper edge of the head (4) and is defined by two lateral branches (14, 15) whose inner faces are provided with a thread (16) for the insertion and blocking of a threaded plug (30). It includes at least one elastic element which locally limits the width of the channel (13) and prevents or impedes the expulsion of the rods (5-10) from the receptacle (11) when they are inserted in the head (4) and are not yet blocked by the plug (30).
    • 骨锚固元件,例如螺钉(1),用于校正脊椎变形的装置,其旨在被植入在椎骨(3)上,并且其头部(4)包括用于一个或 所述装置的更多的杆(5-10)具有在头部(4)的上边缘上开口的通道(13),并且由两个横向分支(14,15)限定,其内表面设有螺纹 (16),用于插入和阻塞螺纹塞(30)。 它包括至少一个弹性元件,其局部地限制通道(13)的宽度,并且当它们插入头部(4)中时,防止或阻止杆(5-10)从容器(11)的排出,并且是 尚未被插头(30)阻塞。
    • 5. 发明申请
    • FLOW-THROUGH TURBINE WITH TURNING BLADES
    • 流动叶片涡流涡轮机
    • WO2011028187A2
    • 2011-03-10
    • PCT/SK2010/000004
    • 2010-09-02
    • VARGA, Peter
    • VARGA, Peter
    • F03B17/06
    • F03D3/04F03B17/065F03D3/02F03D3/067Y02E10/28Y02E10/74
    • Flow-through turbine with turning blades works on the principle of the rotor (3), advantageously another rotor (3) and with using the stator (1 ), in which the rotor (3) is placed and rotates. The rotor (3) with at least one border element (3) delimits, together with at least two blades (4.1 ), advantageously shaped, non- sealed working space (9.1 ), (9.2) of the rotor (3), in which at least two blades are rotating (4.1 ). Flow of the fluid (2) into the working space (9.1 ), (9.2) of the rotor (3) sets the blades (4.1 ) of the rotor (3), placed on outside perimeter of the rotor (3) into rotation motion in such manner that it put up pressure on at least two blades (4.1 ), advantageously shaped, when these lean individually in the starting position against at least one stopper (3.2), placed towards the centre of the rotor (3), kinetic energy of the fluid (2) is transformed to rotary motion of the turbine and its shaft (3.3), then, according to design of the turbine, in approx. 180° rotation of the rotor (3), tilts after working space (9.1 ) in the dead point and with minimum resistance in the direction of flowing fluid (2), its turbulences, effects of hydrodynamic shape of the blade (4.1) wing in cross-section and effect of centrifugal rotary forces of rotating rotor (3), by its rotation approx. by 180°, they move in non-working space (9.2) of the rotor (3) into starting position.
    • 具有转动叶片的流通涡轮机以转子(3)的原理工作,有利的是另一个转子(3),并且使用定子(1),其中转子(3)被放置和旋转。 具有至少一个边界元件(3)的转子(3)与至少两个叶片(4.1)一起限定转子(3)的有利的成形的非密封工作空间(9.1),(9.2),其中 至少两个叶片正在旋转(4.1)。 流体(2)进入转子(3)的工作空间(9.1),(9.2)的流动将转子(3)的叶片(4.1)设置在转子(3)的外周上,使其转动 以这样的方式,当它们朝着朝向转子(3)的中心放置的至少一个止动件(3.2)单独地朝着起始位置倾斜时,其对至少两个叶片(4.1)施加压力,有利地成形,动能 的流体(2)转化为涡轮机及其轴(3.3)的旋转运动,然后根据涡轮机的设计, 转子(3)的180°旋转,在死区内的工作空间(9.1)之后倾斜,并且在流体流动方向(2)上具有最小阻力,其湍流,叶片(4.1)翼的流体动力形状的影响 旋转转子(3)的离心旋转力的横截面和影响,其旋转约 它们在转子(3)的非工作空间(9.2)中移动到起始位置。
    • 6. 发明申请
    • ROTARY INTERNAL COMBUSTION ENGINE WITH ANNULAR CHAMBER
    • 旋转室内燃烧发动机
    • WO2008108743A1
    • 2008-09-12
    • PCT/SK2007/000007
    • 2007-09-26
    • VARGA, Peter
    • VARGA, Peter
    • F01C1/20F01C3/02F01C21/18
    • F01C1/20F01C3/02F01C21/18
    • The rotary nasal annular engine with internal combustion operates on the principle of a pair of the first rotor (1) and the second rotor (2) as well as with usage of a block (3), where the rotors are placed and rotate synchronously. The block (3), together with the circumference surface (1.9), nose (1.2, 1.3) of the rotor (1) and the rotor (2) determinates the engine's combustion chamber (4.1), (4.2) in the shape of a torus, inside of which the rotor (1) is rotating with at least one nose (1.2). The rotor (2) contains on its outer circumference surface (2.9), slots (2.7, 2.8) preferably for the transition of the nose (1.2). During the nose's (1.2) transition through the slot (2.7), of the rotor (2) the compressed medium (7) is transferred through the storage system (2.5) of the rotor (2) through its intake opening (2.4) of the rotor (2) and through the outgoing opening (2.6) of the rotor (2) into the engine's combustion chamber (4.2). In the case of air or oxygen, the fuel mixture explosion as well as expansion is initiated as it is the rotation of the rotor (1).
    • 具有内燃的旋转鼻环形发动机以一对第一转子(1)和第二转子(2)的原理为基础,并且使用块(3),其中转子被放置并同步旋转。 块体(3)与转子(1)和转子(2)的圆周表面(1.9),鼻部(1.2,1.3)一起确定了发动机的燃烧室(4.1),(4.2)的形状 其中转子(1)内部至少有一个鼻(1.2)旋转。 转子(2)在其外周表面(2.9)上包含优选用于鼻部(1.2)过渡的槽(2.7,2.8)。 在通过转子(2)的槽(2.7)的鼻部(1.2)过渡期间,压缩介质(7)通过其转子(2)的储存系统(2.5)通过其转子(2)的进气口(2.4) 转子(2)并通过转子(2)的出口(2.6)进入发动机的燃烧室(4.2)。 在空气或氧气的情况下,随着转子(1)的旋转,燃料混合物爆炸以及膨胀开始。
    • 7. 发明申请
    • ROTARY NASAL ENGINE WITH INTERNAL COMBUSTION
    • 旋转式NASAL发动机内燃机
    • WO2008018841A1
    • 2008-02-14
    • PCT/SK2007/000005
    • 2007-04-11
    • VARGA, Peter
    • VARGA, Peter
    • F01C3/02F04C3/02F01C21/18
    • F01C3/02F01C21/18F04C3/02
    • The rotary nasal engine with internal combustion works on the principle of a pair of the first rotor (1) and the second rotor (2) as well as with usage of a block (3), where the rotors are placed and rotate synchronously. The block (3), together with the circumference surface (1.9), nose (1.2, 1.3) of the rotor (1 ) and the rotor (2), determinates the engine's combustion chamber (4) in the shape of a torus, inside of which at least one nose (1.2) of the rotor (1) rotates. The rotor (2) has at least one contact part (2.9) with slots (2.7, 2.8) for the transition of the nose (1.2) on its outer circumference surface. By covering the opening (2.2) with the opening (3.2) and by rotation of the nose (1.2, 1.3) of the rotor (1), the intake of the medium into the engine's combustion chamber (4.1) takes place, in the combustion chamber, the determination of the rotor (2) and rotation of the rotor (1 ) the medium is transferred and compressed. During the nose's (1.2) transition through the slot (2.7), the compressed medium is transferred through the storage system (2.5), through its intake opening (2.4) and through the outgoing opening (2.6) into the engine's combustion chamber (4.2). In case of air or oxygen, the fuel mixture explosion as well as expansion is initiated as is the rotation of the rotor (1 ). By the rotation of the rotor (1) and by the rotor (2) determination, the exhaust emissions are transferred inside the engine's combustion chamber (4.2), further, by covering the opening (2.3) with the opening (3.3), by the rotor 2 determination, and by rotation of the rotor 1 , the exhaust emissions are transferred out of the engine's combustion chamber (4.2). Consequently, the nose (1.3) of the rotor 1 moves through the slot (2.8), and the intake begins repeatedly.
    • 具有内燃的旋转式鼻发动机以一对第一转子(1)和第二转子(2)的原理为基础,并且使用块(3),其中转子被放置并同步旋转。 块体(3)与转子(1)和转子(2)的圆周表面(1.9),鼻部(1.2,1.3)一起确定发动机的燃烧室(4)为圆环形状,内部 其中转子(1)的至少一个鼻(1.2)旋转。 转子(2)具有至少一个具有槽(2.7,2.8)的接触部分(2.9),用于使鼻部(1.2)在其外圆周表面上过渡。 通过用开口(3.2)覆盖开口(2.2)和通过转子(1)的鼻部(1.2,1.3)的旋转,在燃烧中发生介质进入发动机燃烧室(4.1)的入口 转子(2)的确定和转子(1)的转动介质被传送和压缩。 在通过狭槽(2.7)的鼻子(1.2)过渡期间,压缩介质通过储存系统(2.5),其进气口(2.4)和通过出口(2.6)转移到发动机的燃烧室(4.2)中, 。 在空气或氧气的情况下,与转子(1)的旋转一起开始燃料混合物爆炸以及膨胀。 通过转子(1)的旋转和转子(2)的确定,废气排放物在发动机的燃烧室(4.2)内转移,另外通过用开口(3.3)覆盖开口(2.3),由 转子2的确定,并且通过转子1的旋转,废气排放物被传送出发动机的燃烧室(4.2)。 因此,转子1的鼻部(1.3)移动通过槽(2.8),并且进气口重复开始。