首页> 外国专利> Noise and fuel consumption reducing method for e.g. silent supersonic cargo aircraft, involves adjusting supersonic and subsonic engines, deployed scoops, and retractable air blowers, based on different flight phases

Noise and fuel consumption reducing method for e.g. silent supersonic cargo aircraft, involves adjusting supersonic and subsonic engines, deployed scoops, and retractable air blowers, based on different flight phases

机译:降低噪音和燃料消耗的方法,例如无声超音速货运飞机,涉及根据不同的飞行阶段调整超音速和亚音速发动机,已展开的铲斗和可伸缩的鼓风机

摘要

The method involves adjusting fixed supersonic turbojet engines (21, 22) with a low dilution rate, left and right retractable or fixed subsonic turbojet engines (11, 12) with a low dilution rate, a deployed left scoop (41), a deployed right scoop and additional left and right retractable air blowers (31, 32), based on different flight phases such as supersonic and subsonic phases. The left and right air blowers are actuated by drawing of energy on the engines (11, 12).
机译:该方法包括调节具有低稀释率的固定超音速涡轮喷气发动机(21、22),具有低稀释率的左右可伸缩或固定的亚音速涡轮喷气发动机(11、12),展开的左勺(41),展开的右根据不同的飞行阶段(例如超音速和亚音速阶段),选择铲子和其他左右可伸缩鼓风机(31、32)。左右鼓风机通过在发动机(11、12)上消耗能量来致动。

著录项

  • 公开/公告号FR2915732A1

    专利类型

  • 公开/公告日2008-11-07

    原文格式PDF

  • 申请/专利权人 GFIC SOCIETE A RESPONSABILITE LIMITEE;

    申请/专利号FR20070003209

  • 发明设计人 FOURNIER GERARD FERNAND;

    申请日2007-05-04

  • 分类号B64C30;B64D27/02;B64D33;

  • 国家 FR

  • 入库时间 2022-08-21 19:47:01

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