首页> 外国专利> Aerospace jet 1 / 2 v.t.o.l. (1 / 2 vertical take off and land)

Aerospace jet 1 / 2 v.t.o.l. (1 / 2 vertical take off and land)

机译:航空喷气机1 / 2 v.t.o.l. (1 / 2垂直起飞和降落)

摘要

"Aerospace jet 1 / 2 v.t.o.l. (1 / 2 vertical take off and land)". Utility model patent of air transport, the jet space of 1 / 2 v.t.o.l.(1 / 2 vertical take off and land) configured in its aerodynamic shape, which enables you a better vu00f3o, maneuverability, takeoff and landing in the short space of the ground or track.For the carriage of passengers and cargo, airborne with the autonomy of a long journey without gas.With impulse turbine antegravitacionias (7) slightly inclined in the vertical direction below the wings (13) trespassing this, part of a propulsion body (2) equipment of FIG.N 0 04 and details of the same.That way of engaging the aircraft with the power to speed up the nose (14) of the same giving it a lower weight in the total structure and part of the earth 's gravity.Allowing this art with the impetus of its two (02) reactors, reverse thrust, (4) in the tails of their bodies of propulsion (2),With the speed necessary to raise vu00f3o immediately in a short runway, IRA at an angle of + - 30 198 degrees.The 02 (two) tails (28) parallel gives the safety of elevator (6) (elevator), according to the law of physics, it helps to leverage the structure of the 1 / 2 v.t.o.l.For the same stick your nose (14) and raise vu00f3o.In terms of its landing, besides the two (02) flaps (8) on the wings (13) its 02 (two) reactors of impulse reversible (4) with negative forces.This aircraft has the innovation of braking, 04 (four) flaps of braking of the stabilizers in the pressure of the wind tunnel (32) which gives a powerful anchor (3).5 m2) of braking and unprecedented level of aviation.
机译:“航空航天飞机1 / 2 v.t.o.l.(1 / 2垂直起飞和降落)”。实用新型航空运输专利,其喷气形状的1 / 2 vtol(1 / 2垂直起飞和着陆)的喷气空间配置为空气动力学形状,可在较短的时间内提供更好的v u00f3o,可操纵性,起飞和着陆地面或轨道的空间。用于载运旅客和货物,在无气体的情况下可以长途飞行而自主飞行。脉冲涡轮增压一体机(7)在机翼(13)下方垂直方向略微倾斜,超过了机翼的一部分图N <0> 04的推进器(2)设备及其详细信息。通过这种方式使飞机接合以加速其机头(14)的力量,使飞机的整体结构重量更轻借助其两个(02)反应堆的推动力,反向推力(4)位于推进器尾部(2)的推动力,以提高v u00f3o所需的速度立即在一条短跑道上,IRA以+-30 <198>度的角度旋转。02(两条)尾巴( 28)平行提供了电梯(6)(电梯)的安全性,根据物理定律,它有助于利用1 / 2 vtol的结构来使鼻子(14)伸出同样的鼻子并提高v u00f3o。就着陆而言,除了机翼(13)上的两个(02)襟翼(8)之外,它的02(两个)带有负力的脉冲可逆(4)反应堆。该飞机具有制动创新,04(四个)在风洞(32)的压力下,稳定器的制动襟翼可提供强大的制动锚(3).5 m2)和空前的航空水平。

著录项

  • 公开/公告号BR8002027U

    专利类型

  • 公开/公告日2002-04-09

    原文格式PDF

  • 申请/专利权人 ROBERTO STEWARD JR;

    申请/专利号BR8002027U

  • 发明设计人 ROBERTO STEWARD JR;

    申请日2000-08-17

  • 分类号B64C1/08;B64D27/18;

  • 国家 BR

  • 入库时间 2022-08-22 00:46:00

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