首页> 外国专利> DEVICE FOR TURNING A TURBOPUMPS DRIVING TURBINE FOR A ROCKET ENGINE OPERATING ON LIQUID FUEL

DEVICE FOR TURNING A TURBOPUMPS DRIVING TURBINE FOR A ROCKET ENGINE OPERATING ON LIQUID FUEL

机译:用于在液体燃料上操作火箭发动机的涡轮转动涡轮的装置

摘要

The device is used in rocket engines. It increases the powerof the engines. The device includes several stages is driven. Thegas turbine (14) of the first stage of driving by compressed airfrom a tank (4) and revolves turbopump (9) for fuel and turbopump(15) for oxidant. Another turbine (44) of the following stage isdriven by the combusted fuel mixture in a nozzle (18) and drivesturbines for fuel and for oxidant in that stage. Turbine (19) ofthe last stage is driven by the combusted fuel mixture in nozzle(45) by driving two turbopumps - for fuel and for oxidant whichpumps feed manifold (24). The fuel mixture burns in another nozzle(25) where the general traction of the whole driving system isformed.1 claim, 3 figures
机译:该设备用于火箭发动机。它增加了发动机的功率。该设备包括多个驱动阶段。第一阶段的燃气轮机(14)由来自罐(4)的压缩空气驱动,并且使用于燃料的涡轮泵(9)和用于氧化剂的涡轮泵(15)公转。下一级的另一涡轮机(44)由喷嘴(18)中燃烧的燃料混合物驱动,并驱动该级中用于燃料和氧化剂的涡轮机。最后一级的涡轮机(19)由喷嘴(45)中已燃烧的燃料混合物驱动两个涡轮泵-用于燃料和氧化剂的泵驱动进气歧管(24)驱动。混合气在另一个喷嘴(25)中燃烧,形成整个驱动系统的总牵引力。1项权利要求,3个数字

著录项

  • 公开/公告号BG98866A

    专利类型

  • 公开/公告日1996-03-29

    原文格式PDF

  • 申请/专利权人 LJUBENOV IVAN T.;

    申请/专利号BG19940098866

  • 发明设计人 LJUBENOV IVAN T.;

    申请日1994-06-20

  • 分类号F02K9/42;

  • 国家 BG

  • 入库时间 2022-08-22 03:54:54

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