首页> 外国专利> Short take-off - aircraft, which the noise during the take-off and landing concentrate on the airport

Short take-off - aircraft, which the noise during the take-off and landing concentrate on the airport

机译:短距起飞-飞机,其起飞和降落期间的噪音集中在机场

摘要

Short take-off - aircraft, which the noise during the take-off and landing concentrate on the airport. For this purpose, two engines (1) arranged under the bearing surfaces. An auxiliary - engine (4) is located in the rear of the aircraft. The thrust nozzles (3, 5) are pivotally. The vectors of the thrust nozzles (3, 5) form a stable spring 37 at the take-off and landing. The strong engines (1), instead of a fan having a compressor (2) equipped. In addition to the reduction for the surrounding area, this aircraft have the advantage that no long start - and landing runway is required. For this is particularly wihtig an airport, because an additional runway abuts on large resistance.
机译:短距起飞-飞机,其起飞和降落期间的噪音集中在机场上。为此,在轴承表面下方布置了两个发动机(1)。辅助引擎(4)位于飞机的后部。推力喷嘴(3、5)可枢转。推力喷嘴(3、5)的矢量在起飞和降落时形成稳定的弹簧37。强劲的发动机(1)代替配备了压缩机(2)的风扇。除了减少周围区域外,这架飞机还具有无需长时间起降和降落跑道的优势。为此,尤其是机场,因为一条额外的跑道紧靠着巨大的阻力。

著录项

  • 公开/公告号DE102015002912A1

    专利类型

  • 公开/公告日2016-09-08

    原文格式PDF

  • 申请/专利权人 GERHARD BIHLER;

    申请/专利号DE20151002912

  • 发明设计人 GLEICH ANMELDER;

    申请日2015-03-06

  • 分类号B64C29/00;

  • 国家 DE

  • 入库时间 2022-08-21 14:09:37

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号