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    • 1. 发明授权
    • Annular piston engine with afterburner and separable power turbine
    • 带燃烧器和可分离动力涡轮的环形活塞发动机
    • US3885386A
    • 1975-05-27
    • US46279074
    • 1974-04-22
    • BACHMANN WILLIAM V
    • BACHMANN WILLIAM V
    • F01N3/24F01N5/04F02B3/06F02B25/10F02B33/04F02B33/12F02B41/10F02B75/02F02B75/10F02B75/28F02B75/30F02B37/02
    • F02B33/12F01N3/24F01N5/04F02B3/06F02B25/10F02B33/04F02B41/10F02B75/10F02B75/28F02B75/30F02B2075/027Y02T10/16Y02T10/163
    • An internal combustion engine includes an annular or ring-type cylinder and piston therein; exhaust ports from the cylinder lead to an afterburner reactor situated generally medially of the annular cylinder; the exhaust gases are further burned within the afterburner section; to further reduce pollutants during the afterburning process, additional air is pumped into the afterburner section as by the ring piston due to its special configuration enabling it to accomplish, for example, triple functions such as: (a) to act as a power transmitting means, (b) to act as a pumping means to supply the engine''s combustion chamber with scavenging air and/or an air-fuel mixture, and (c) to act as an air pumping means to supply desired quantities of ambient air into the afterburner section even in timed intervals with a constant predetermined pressure and predetermined quantities in order to thereby maximize the degree of control of the temperature generated in the afterburner and thereby more nearly fully oxidize the unburned fuel residues entering the afterburner. The ring piston is so constructed that it can be operatively connected to an output shaft as through the use of only a single crank, single connecting rod and wrist pin. Further, to extract a considerable amount of energy from the waste exhaust gases leaving the afterburner, a power turbine is provided which is within the exit path of the exhaust gases. The power turbine is conveniently incorporated as into the engine head and the turbine output shaft is either geared by reduction gear means to work in unison with the output crank shaft, or the turbine shaft rotates at an independent speed and is geared to drive (some or all of) the engine and/or vehicular accessories.
    • 内燃机在其中包括环形或环形气缸和活塞; 来自气缸的排气口引导到通常位于环形气缸中间的加力反应器; 排气在进一步燃烧器部分进一步燃烧; 为了进一步减少在后燃过程中的污染物,由于环形活塞的特殊配置,附加的空气被泵送到加力器部分中,使得其能够实现例如以下三种功能:(a)作为动力传递装置 ,(b)作为泵送装置,为发动机的燃烧室提供清扫空气和/或空气燃料混合物,以及(c)作为空气泵送装置,以将所需量的环境空气供应到后燃室部分 即使在具有恒定的预定压力和预定量的定时间隔中,从而使得在后燃器中产生的温度的控制程度最大化,从而使进入加力燃烧器的未燃燃料残余物几乎完全氧化。 环形活塞的结构使得它可以通过仅使用单个曲柄,单个连杆和腕针来操作地连接到输出轴。 此外,为了从离开加力燃烧器的废废气中提取大量的能量,提供了在废气的出口路径内的动力涡轮机。 动力涡轮机方便地结合在发动机头部中,并且涡轮机输出轴由减速齿轮装置传动,以与输出曲轴一致地工作,或者涡轮机轴以独立的速度旋转并且被齿轮驱动(一些或 所有)发动机和/或车辆附件。
    • 2. 发明专利
    • AT76318T
    • 1992-06-15
    • AT88100382
    • 1988-01-13
    • BACHMANN WILLIAM V
    • BACHMANN WILLIAM V
    • A63C5/11A63C11/00
    • Apparatus for creating aerodynamic lift to a downhill skier (10) is shown as having a harness adapted to be worn by the skier (10), a left wing structure (40) is operatively carried by the harness (32), a right wing structure (38) is operatively carried by the harness (32), the left wing structure (40) has a first longitudinal axis extending generally transversely of the skier (10), the right wing structure (38) has a second longitudinal axis extending generally transversely of the skier, the left wing structure (40) is selectively rotatable about the first longitudinal axis, the right wing structure (38) is selectively rotatable about the second longitudinal axis, and the left (40) and right wing (38) structures are respectively rotatable about the first and second axes independently of each other by the skier (10) to respective selected positions.
    • 4. 发明专利
    • DE3871170D1
    • 1992-06-25
    • DE3871170
    • 1988-01-13
    • BACHMANN WILLIAM V
    • BACHMANN WILLIAM V
    • A63C5/11A63C11/00
    • Apparatus for creating aerodynamic lift to a downhill skier (10) is shown as having a harness adapted to be worn by the skier (10), a left wing structure (40) is operatively carried by the harness (32), a right wing structure (38) is operatively carried by the harness (32), the left wing structure (40) has a first longitudinal axis extending generally transversely of the skier (10), the right wing structure (38) has a second longitudinal axis extending generally transversely of the skier, the left wing structure (40) is selectively rotatable about the first longitudinal axis, the right wing structure (38) is selectively rotatable about the second longitudinal axis, and the left (40) and right wing (38) structures are respectively rotatable about the first and second axes independently of each other by the skier (10) to respective selected positions.
    • 7. 发明专利
    • IT1234989B
    • 1992-06-16
    • IT4755488
    • 1988-01-20
    • BACHMANN WILLIAM V
    • BACHMANN WILLIAM V
    • A63C5/11A63C11/00A63C
    • Apparatus for creating aerodynamic lift to a downhill skier (10) is shown as having a harness adapted to be worn by the skier (10), a left wing structure (40) is operatively carried by the harness (32), a right wing structure (38) is operatively carried by the harness (32), the left wing structure (40) has a first longitudinal axis extending generally transversely of the skier (10), the right wing structure (38) has a second longitudinal axis extending generally transversely of the skier, the left wing structure (40) is selectively rotatable about the first longitudinal axis, the right wing structure (38) is selectively rotatable about the second longitudinal axis, and the left (40) and right wing (38) structures are respectively rotatable about the first and second axes independently of each other by the skier (10) to respective selected positions.
    • 8. 发明专利
    • IT8847554D0
    • 1988-01-20
    • IT4755488
    • 1988-01-20
    • BACHMANN WILLIAM V
    • BACHMANN WILLIAM V
    • A63C5/11A63C11/00A63C
    • Apparatus for creating aerodynamic lift to a downhill skier (10) is shown as having a harness adapted to be worn by the skier (10), a left wing structure (40) is operatively carried by the harness (32), a right wing structure (38) is operatively carried by the harness (32), the left wing structure (40) has a first longitudinal axis extending generally transversely of the skier (10), the right wing structure (38) has a second longitudinal axis extending generally transversely of the skier, the left wing structure (40) is selectively rotatable about the first longitudinal axis, the right wing structure (38) is selectively rotatable about the second longitudinal axis, and the left (40) and right wing (38) structures are respectively rotatable about the first and second axes independently of each other by the skier (10) to respective selected positions.