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1. 发明申请

WO2012120285A2 ROTARY ENGINE ROTOR 审中-公开
标题翻译：旋转发动机转子
公开(公告)号：WO2012120285A2
公开(公告)日：2012-09-13
申请号：PCT/GB2012050480
申请日：2012-03-05
申请人： UAV ENGINES LTD , BIDDULPH CHRISTOPHER JOHN , BAGNELL JONATHAN MARK
发明人： BIDDULPH CHRISTOPHER JOHN , BAGNELL JONATHAN MARK
IPC分类号： F01C1/22 , F01C21/06 , F01C21/08
CPC分类号： F16J1/001 , F01C1/22 , F01C21/06 , F01C21/08
摘要： A rotary engine rotor (10) comprises a body (12) comprising an outer surface (18), an inner surface (22), an insert (14) and a fixing member (16).The outer surface (18) comprises three rotor sides (20) arranged in an equilateral triangle shape. The inner surface (22) comprises a location portion (24) at the midpoint of each rotor side (20), the location portions (24) together defining a location aperture (26). One location portion (24) is provided with a first fixing socket (28) extending radially from the inner surface (22) of the body (12), towards the outer surface (18) of the body (12). Cooling channels (30) are provided axially through the body (12) in the region of each apex (31). The insert (14) is provided in the location aperture (26) and comprises a bearing part (38) with a second fixing socket (40) extending radially through the insert (14) and in alignment with the first fixing socket (28).The fixing member (6) is provided through the second fixing socket (40) and received in the first fixing socket (28) to couple the insert (14) to the body (12).
摘要翻译：旋转发动机转子（10）包括主体（12），其包括外表面（18），内表面（22），插入件（14）和固定构件（16）。外表面（18）包括三个转子侧面（20）以等边三角形排列。内表面（22）包括在每个转子侧（20）的中点处的定位部分（24），所述位置部分（24）一起限定位置孔（26）。一个位置部分（24）设置有从主体（12）的内表面（22）径向延伸到主体（12）的外表面（18）的第一固定插座（28）。在每个顶点（31）的区域中，冷却通道（30）沿轴向穿过主体（12）。所述插入件（14）设置在所述定位孔（26）中并且包括具有径向延伸穿过所述插入件（14）并与所述第一固定插座（28）对准的第二固定插座（40）的支承部件（38）。固定构件（6）穿过第二固定插座（40）设置并被容纳在第一固定插座（28）中，以将插入件（14）耦合到主体（12）。

2. 发明申请

WO2012120285A3 ROTARY ENGINE ROTOR 审中-公开
公开(公告)号：WO2012120285A3
公开(公告)日：2012-09-13
申请号：PCT/GB2012/050480
申请日：2012-03-05
申请人： UAV ENGINES LTD. , BIDDULPH, Christopher John , BAGNELL, Jonathan Mark
发明人： BIDDULPH, Christopher John , BAGNELL, Jonathan Mark
IPC分类号： F01C1/22 , F01C21/06 , F01C21/08
摘要： A rotary engine rotor (10) comprises a body (12) comprising an outer surface (18), an inner surface (22), an insert (14) and a fixing member (16). The outer surface (18) comprises three rotor sides (20) arranged in an equilateral triangle shape. The inner surface (22) comprises a lo¬ cation portion (24) at the midpoint of each rotor side (20), the location portions (24) together defining a location aperture (26). One location portion (24) is provided with a first fixing socket (28) extending radial¬ ly from the inner surface (22) of the body (12), towards the outer sur¬ face (18) of the body (12). Cooling channels (30) are provided axially through the body (12) in the region of each apex (31). The insert (14) is provided in the location aperture (26) and comprises a bearing part (38) with a second fixing socket (40) extending radially through the in¬ sert (14) and in alignment with the first fixing socket (28). The fixing member (16) is provided through the second fixing socket (40) and received in the first fixing socket (28) to couple the insert (14) to the body (12).

3. 发明申请

WO2009053749A1 A FUEL HEATING APPARATUS 审中-公开
标题翻译：燃油加热装置
公开(公告)号：WO2009053749A1
公开(公告)日：2009-04-30
申请号：PCT/GB2008/050987
申请日：2008-10-24
申请人： UAV ENGINES LTD , BIDDULPH, Christopher John
发明人： BIDDULPH, Christopher John
IPC分类号： F02M53/02 , F02M53/06 , F02M31/125
CPC分类号： F02M53/02 , F02M31/125 , F02M31/13 , F02M53/06 , Y02T10/126
摘要： A fuel heating apparatus for an internal combustion engine or other type ofspark ignition engine having an associated pressurised fueldeliverysystem, the apparatus comprising a chamber for receiving a volume of a pressurised liquid fuel; and means for heating the fuel within the chamber to provide heated liquid fuel to the fuel delivery system of the engine, to thereby minimise condensation of the fuel and facilitate ignition of the engine within relatively low ambient temperature environments. The apparatus has particular application with 'heavy fuels', such as diesel or kerosene, and improves the reliabilityand performance of the engine especially during 'cold starts' and while transitioning to fast-idling.
摘要翻译：一种用于内燃机或其它类型的具有相关联的加压熔融系统的喷燃发动机的燃料加热装置，该装置包括用于容纳一定体积的加压液体燃料的室; 以及用于加热室内的燃料以将加热的液体燃料提供给发动机的燃料输送系统的装置，从而最小化燃料的冷凝并促进发动机在相对低的环境温度环境中点燃。该装置特别适用于柴油或煤油等重质燃料，特别是在“冷启动”期间以及过渡到快速空转时，可提高发动机的可靠性和性能。

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