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SAFETY INCREASER FOR HELICOPTER

机译:直升机的安全增加

摘要

PURPOSE: To increase the stability of a helicopter on board a ship by supporting the helicopter on both the sides of a lengthwise center plane when the helicopter is placed on a platform, through a front wheel type drive gear by the stabilizing wheel of an auxiliary stable gear composed of two lateral stabilizers. CONSTITUTION: An auxiliary gear composed of two lateral stabilizers 13 is provided on the lower part of a hilicopter body 1, and rigid supporters 17 for supporting stabilizing wheels 16 in the lower ends are protruded on both the sides of the body 1 in use positions, in a direction deflecting toward an auxiliary under carriage 2 to the main and lateral under carrige 6 of a front wheel type landing gear, and biased to both the side laterals of the center lengthwise plane PP of a hilicopter. The stabilizing wheels 16 are supported on a platform moving on both the sides of the lengthwise center plane PP, when the helicopter is placed on the platform on board a ship by the front wheel type landing gears 2 and 6, and thus the stability of the helicopter on board the ship can be increased.
机译:目的:通过将直升飞机放在平台上时,通过将直升飞机放在平台上,通过前轮式驱动齿轮和辅助马by的稳定轮来支撑直升飞机的稳定性,从而提高直升飞机上的直升飞机的稳定性齿轮由两个侧向稳定器组成。构成:在直升机机体1的下部设有一个由两个侧向稳定器13组成的辅助齿轮,在使用位置,用于支撑下端稳定轮16的刚性支撑架17突出在机体1的两侧,在向副副车架2偏向前轮型起落架的主副车架6和副副车架6的方向上,偏航到直升机的中央纵向平面PP的两侧。当将直升飞机通过前轮式起落架2和6放置在船上的平台上时,稳定轮16被支撑在在纵向中心平面PP的两侧上移动的平台上,从而稳定轮16的稳定性。可以增加船上的直升机。

著录项

  • 公开/公告号JPH01254492A

    专利类型

  • 公开/公告日1989-10-11

    原文格式PDF

  • 申请/专利权人 AEROSPAT SOC NATL IND;

    申请/专利号JP19890006086

  • 发明设计人 BERUNAARU RUI ARUCHIYUURU;TOMASAN RUNE;

    申请日1989-01-17

  • 分类号B64C25/00;B64C25/02;B64C25/66;

  • 国家 JP

  • 入库时间 2022-08-22 06:47:41

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