WÄRMEKRAFTMASCHINE, WIE EIN VERBRENNUNGS- UND/ODER DAMPFMOTOR
    1.
    发明公开
    WÄRMEKRAFTMASCHINE, WIE EIN VERBRENNUNGS- UND/ODER DAMPFMOTOR 审中-公开
    火电装机由烧伤和/或蒸汽发动机

    公开(公告)号:EP2310629A2

    公开(公告)日:2011-04-20

    申请号:EP09781192.1

    申请日:2009-07-28

    IPC分类号: F01B1/06

    摘要: A heat engine has a rotary element (10). A plurality of drive devices (14) are arranged within the rotary element (10). Each drive device has a plurality of piston-cylinder devices (16, 18) arranged around a common central expansion chamber (20). Piston heads (22) of the piston (18) bear against a force transmission surface (24) of the rotary element (10) so as to drive said rotary element (10).

    FLUGZEUG
    2.
    发明公开
    FLUGZEUG 有权

    公开(公告)号:EP1943143A2

    公开(公告)日:2008-07-16

    申请号:EP07728486.7

    申请日:2007-04-25

    IPC分类号: B64C27/20 B64C27/28 B64C29/00

    CPC分类号: B64C29/0033

    摘要: An aircraft, in particular a VTOL craft, comprises a fuselage (10) supporting at least a pair of wings (16, 18). According to the invention, several propeller devices are connected to the fuselage (10) and optionally to the pair of wings (16, 18). The propeller devices may be pivoted about pivot axes (28, 30) independently of each other. The pivot axes are at an angle ≠ 0° to each other.

    摘要翻译: 飞行器,特别是VTOL飞行器,包括支撑至少一对翼(16,18)的机身(10)。 根据本发明,多个螺旋桨装置连接到机身(10)并且可选地连接到一对翼(16,18)。 螺旋桨装置可以独立于彼此绕枢转轴线(28,30)枢转。 枢轴相互之间的角度≠0°。

    FLUGZEUG
    3.
    发明授权
    FLUGZEUG 有权

    公开(公告)号:EP1943143B1

    公开(公告)日:2009-10-14

    申请号:EP07728486.7

    申请日:2007-04-25

    IPC分类号: B64C27/20 B64C27/28 B64C29/00

    CPC分类号: B64C29/0033

    摘要: An aircraft, in particular a VTOL craft, comprises a fuselage (10) supporting at least a pair of wings (16, 18). According to the invention, several propeller devices are connected to the fuselage (10) and optionally to the pair of wings (16, 18). The propeller devices may be pivoted about pivot axes (28, 30) independently of each other. The pivot axes are at an angle ? 0° to each other.

    摘要翻译: 飞行器,特别是VTOL飞行器,包括支撑至少一对翼(16,18)的机身(10)。 根据本发明,多个螺旋桨装置连接到机身(10)并且可选地连接到一对翼(16,18)。 螺旋桨装置可以独立于彼此绕枢转轴线(28,30)枢转。 枢轴的角度是? 彼此成0°。

    VERBRENNUNGSMOTOR
    4.
    发明公开
    VERBRENNUNGSMOTOR 审中-公开

    公开(公告)号:EP1794426A1

    公开(公告)日:2007-06-13

    申请号:EP05754577.4

    申请日:2005-06-02

    CPC分类号: F01B13/045 F02B75/265

    摘要: The invention relates to an internal combustion engine (10) comprising several combustion devices (14) each of which is provided with a cylinder section (26,32) and a piston (28, 30) guided in said section ( 26, (32), wherein the combustion devices (14) are arranged along a circular line (24). Said invention is characterised I that said combustion devices (14) are frictionally connected to each other substentially along said circular line (24) and generate a circumferentially directed force. The invention makes it possible to obtain a movement of rotation for which a crankshaft is not needed, thereby increasing the internal combustion engine (10) efficiency.

    摘要翻译: 本发明涉及一种包括多个燃烧装置(14)的内燃机(10),每个燃烧装置(14)中的每一个设置有在所述区段(26,(32))中引导的汽缸区段(26,32)和活塞(28,30) 其特征在于,所述燃烧装置(14)沿着所述环形线(24)沿着潜在方向彼此摩擦连接并且产生沿周向指向的力 本发明使得可以获得不需要曲轴的旋转运动,从而提高了内燃机(10)的效率。