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Invention Publication
CN101962078A 航空螺旋桨矢量发动机 失效 - 权利终止

  • Patent Title: 航空螺旋桨矢量发动机
  • Patent Title (English): Aircraft propeller vector engine
  • Application No.: CN201010257973.5
    Application Date: 2010-08-20
  • Publication No.: CN101962078A
    Publication Date: 2011-02-02
  • Inventor: 王泽民
  • Applicant: 王泽民
  • Applicant Address: 黑龙江省哈尔滨市南岗区清明二道街4号1单元202门
  • Assignee: 王泽民
  • Current Assignee: 王泽民
  • Current Assignee Address: 黑龙江省哈尔滨市南岗区清明二道街4号1单元202门
  • Agency: 哈尔滨东方专利事务所
  • Agent 陈晓光
  • Main IPC: B64D35/00
  • IPC: B64D35/00 ;  F01D1/00
航空螺旋桨矢量发动机
Abstract:
航空螺旋桨矢量发动机。一直以来，固定翼螺旋桨飞机的起飞、降落需要一定的滑跑距离，机动动性能差，实用性受到很多限制。航空螺旋桨矢量发动机，其组成包括：螺旋桨(1)、发动机(2)，所述的发动机连接连接座(3)，所述的连接座连接万向动力传输器(4)，所述的万向动力传输器连接万向臂(5)，所述的万向臂连接螺旋桨连接轴(6)，所述的螺旋桨连接轴连接螺旋桨。本发明用于航空发动机。
Abstract(English):

The invention relates to an aircraft propeller vector engine. All these times, the take-off and the landing of fixed-wing propeller-driven planes always require a certain taxiing distance, the maneuverability is poor, and the practicability is greatly limited. The aircraft propeller vector engine comprises a propeller (1) and an engine (2), wherein the engine is connected with a connecting base (3), the connecting base is connected with a universal power transmitter (4), the universal power transmitter is connected with a universal arm (5), the universal arm is connected with a propeller connecting shaft (6), and the propeller connecting shaft is connected with the propeller. The invention is applied to aircraft engines.

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