WO2021042371A1 - 一种涡轮发动机的隔声舱体 - Google Patents

一种涡轮发动机的隔声舱体 Download PDF

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Publication number
WO2021042371A1
WO2021042371A1 PCT/CN2019/104716 CN2019104716W WO2021042371A1 WO 2021042371 A1 WO2021042371 A1 WO 2021042371A1 CN 2019104716 W CN2019104716 W CN 2019104716W WO 2021042371 A1 WO2021042371 A1 WO 2021042371A1
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Prior art keywords
turbine engine
noise reduction
sound insulation
air
intake
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PCT/CN2019/104716
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English (en)
French (fr)
Inventor
李心成
张日奎
常胜
纪晓磊
兰春强
吴义朋
李先策
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烟台杰瑞石油装备技术有限公司
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Priority to PCT/CN2019/104716 priority Critical patent/WO2021042371A1/zh
Publication of WO2021042371A1 publication Critical patent/WO2021042371A1/zh

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants

Definitions

  • the invention relates to the technical field of noise reduction, in particular to a sound insulation cabin of a turbine engine.
  • the purpose of the present invention overcomes the shortcomings of the prior art, and provides a sound insulation cabin of a turbine engine.
  • an air intake noise reduction unit at the air inlet of the turbine engine, noise reduction is achieved on the air intake of the turbine engine;
  • a ventilation noise reduction unit is added to the transmission direction of the engine to realize ventilation, cooling and noise reduction of the turbine engine; sound insulation materials are filled around the turbine engine to realize the overall noise reduction around the turbine engine.
  • a sound insulation cabin of a turbine engine the sound insulation cabin is sleeved on the turbine engine
  • the sound insulation cabin includes a cabin body, an air intake noise reduction unit And a ventilation noise reduction unit, the air intake noise reduction unit and the ventilation noise reduction unit are arranged on the cabin body, the frame of the cabin body is filled with sound insulation material, and the air intake noise reduction unit is used for the air intake reduction of the turbine engine
  • the ventilation noise reduction unit is used for noise reduction of the ventilation system of the turbine engine.
  • the air intake noise reduction unit includes an air intake filter, an air intake muffler, an air intake room, and an air intake duct.
  • the air intake room is arranged on the top of the cabin body, and the air inlet is arranged on the outer side of the air inlet room.
  • the air filter is provided with an air intake muffler on the inner side of the air intake chamber, and the air intake filter corresponds to the position of the air intake muffler.
  • the air intake chamber is connected to the air inlet of the turbine engine through an air intake pipe.
  • the ventilation and noise reduction unit includes an air inlet muffler, an air inlet fan and an exhaust air muffler, the air inlet muffler is connected to the air inlet fan, and the air inlet muffler, the air inlet fan and the exhaust air muffler are connected.
  • the air inlet muffler is arranged on the cabin body, and the air inlet silencer and the exhaust air silencer are oppositely arranged on both sides of the cabin body.
  • a sound insulation door is provided in the non-transmission direction of the turbine engine, and the sound insulation door is filled with a sound insulation material.
  • the present invention has the following beneficial effects: by adding an air intake noise reduction unit to the intake port of the turbine engine, the noise reduction of the air intake of the turbine engine is realized; and the ventilation reduction unit is added in the transmission direction of the turbine engine.
  • the noise unit realizes the ventilation, cooling and noise reduction of the turbine engine; the sound insulation material is filled around the turbine engine to realize the overall noise reduction around the turbine engine.
  • the sound insulation door filled with sound insulation materials can not only provide sound insulation in the non-transmission direction of the turbine engine, but also facilitate maintenance and daily maintenance.
  • Fig. 1 is a schematic diagram of the structure of a sound insulation cabin of a turbine engine.
  • Fig. 2 is a schematic diagram of the external structure of the sound insulation cabin of the turbine engine.
  • a sound insulation cabin of a turbine engine the sound insulation cabin is sleeved on the turbine engine 7, the sound insulation cabin includes a cabin body, an air intake noise reduction unit and a ventilation reduction
  • the air intake noise reduction unit and the ventilation noise reduction unit are arranged on the cabin body, the frame of the cabin body is filled with sound insulation material, and the air intake noise reduction unit is used to reduce the air intake noise of the turbine engine 7,
  • the ventilation noise reduction unit is used for noise reduction of the ventilation system of the turbine engine 7.
  • the sound insulation material can be glass fiber wool, rock wool, polyurethane, aluminum honeycomb panel, peak cotton and so on.
  • the air-intake noise reduction unit includes an air-intake filter 6, an air-intake muffler 5, an air-intake room 2 and an air-intake duct.
  • the air-intake room 2 is arranged on the top of the cabin body and on the outer side of the air-intake room 2.
  • An air inlet filter 6 is provided, and an air inlet muffler 5 is arranged on the inner side of the air inlet chamber 2.
  • the air inlet filter 6 corresponds to the position of the air inlet muffler 5, and an air outlet is provided on the bottom surface of the air inlet chamber 2.
  • the air inlet chamber 2 is connected to one end of the air inlet pipe through the air outlet, and the other end of the air inlet pipe is connected to the air inlet of the turbine engine 7. Both the top surface and the bottom surface of the air intake room 2 are filled with sound insulation materials.
  • An intake filter 6 and an intake muffler 5 are not provided at the exhaust end of the turbine engine 7.
  • the exhaust end is the end where the exhaust duct 10 of the turbine engine 7 is located.
  • the side surface of the air intake room 2 on the side of the exhaust end may also be filled with sound insulation material.
  • the ventilation and noise reduction unit includes an air inlet muffler 4, an air inlet fan and an exhaust air muffler 1, the air inlet muffler 4 is connected to the air inlet fan, the air inlet muffler 4, an air inlet fan and an exhaust air
  • the muffler 1 is arranged on the cabin body, and the inlet air muffler 4 and the exhaust air muffler 1 are oppositely arranged on both sides of the cabin body.
  • the ventilation and noise reduction unit is more than one group.
  • one set may be provided on both sides of the transmission direction of the turbine engine 7 respectively.
  • the exhaust muffler 1 in each group of ventilation and noise reduction unit can be set to one or two. This can better play the role of ventilation and noise reduction.
  • a sound insulation door 3 is provided in the non-transmission direction of the turbine engine 7, and the sound insulation door 3 is filled with sound insulation material.
  • Multiple soundproof doors 3 can be provided, and multiple soundproof doors 3 filled with soundproof materials can not only provide sound insulation for the turbine engine 7 in the non-transmission direction, but also facilitate maintenance and daily maintenance.
  • the air used for combustion of the turbine engine 7 enters through the intake filter 6, enters the intake chamber 2 through the intake muffler 5, and then enters the intake port of the turbine engine 7 through the intake duct.
  • the air used for the ventilation and cooling of the turbine engine 7 enters the engine sound insulation cabin through the air intake silencer 4 under the action of the air intake fan, and then is discharged to the outside of the engine sound insulation cabin through the exhaust muffler 1.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)

Abstract

一种涡轮发动机的隔声舱体，隔声舱体套设于涡轮发动机上，隔声舱体包括舱本体，进气降噪单元和通风降噪单元，进气降噪单元和通风降噪单元设在舱本体上，舱本体的四周填充隔音材料，进气降噪单元用于涡轮发动机的进气降噪，通风降噪单元用于涡轮发动机的通风系统降噪。通过在涡轮发动机的进气口增设进气降噪单元，实现对涡轮发动机的进气实现降噪；在涡轮发动机的传动方向上增设通风降噪单元，实现对涡轮发动机的通风、冷却降噪；在涡轮发动机的四周填充隔音材料，实现对涡轮发动机四周整体的降噪。

Description

一种涡轮发动机的隔声舱体 技术领域
本发明涉及降噪技术领域，具体涉及一种涡轮发动机的隔声舱体。
背景技术
在全球的油气田压裂作业现场，压裂设备的噪音扰民问题一直在困扰着油服公司。特别是在一些距离居民区近的井场，噪音扰民导致设备无法在夜间施工，进而推迟了压裂施工进度。
伴随着压裂装备技术的发展，出现了以涡轮发动机为动力源的压裂设备。虽然，涡轮发动机相比较传统的柴油发动机具有很多优势，比如单机功率密度大，可以100％以天然气为燃料以降低施工成本，等等。但是涡轮发动机的噪音远超柴油发动机，这个问题一直没有得到有效解决。
为此亟待一种涡轮发动机的隔声舱体，以解决涡轮发动机噪音大的问题。
发明内容
本发明的目的克服现有技术的不足，提供一种涡轮发动机的隔声舱体，通过在涡轮发动机的进气口增设进气降噪单元，实现对涡轮发动机的进气实现降噪；在涡轮发动机的传动方向上增设通风降噪单元，实现对涡轮发动机的通风、冷却降噪；在涡轮发动机的四周填充隔音材料，实现对涡轮发动机四周整体的降噪。
本发明的目的是通过以下技术措施达到的：一种涡轮发动机的隔声舱体，所述隔声舱体套设于涡轮发动机上，所述隔声舱体包括舱本体，进气降噪单元和通风降噪单元，所述进气降噪单元和通风降噪单元设在舱本体上，所述舱本体的框架四周填充隔音材料，所述进气降噪单元用于涡轮发动机的进气 降噪，所述通风降噪单元用于涡轮发动机的通风系统降噪。
进一步地，所述进气降噪单元包括进气过滤器，进气消音器，进气房和进气管道，所述进气房设在舱本体的顶部，在进气房的外侧面设置进气过滤器，在进气房的内侧面设置进气消音器，进气过滤器与进气消音器的位置相对应，进气房通过进气管道与涡轮发动机的进气口连接。
进一步地，在所述涡轮发动机的排气端不设置进气过滤器和进气消音器。
进一步地，所述通风降噪单元包括进风消音器，进风风机和排风消音器，所述进风消音器和进风风机连接，所述进风消音器、进风风机和排风消音器设在舱本体上，所述进风消音器与排风消音器相对设置在舱本体的两侧。
进一步地，所述通风降噪单元为1组以上。
进一步地，在涡轮发动机非传动方向上设有隔声门，所述隔声门填充隔音材料。
与现有技术相比，本发明的有益效果是：通过在涡轮发动机的进气口增设进气降噪单元，实现对涡轮发动机的进气实现降噪；在涡轮发动机的传动方向上增设通风降噪单元，实现对涡轮发动机的通风、冷却降噪；在涡轮发动机的四周填充隔音材料，实现对涡轮发动机四周整体的降噪。通过填充有隔音材料的隔声门的设置，既能起到对涡轮发动机非传动方向上的隔音，又能很好的方便维修和日常维护。
下面结合附图和具体实施方式对本发明作详细说明。
附图说明
图1是涡轮发动机隔声舱体的结构示意图。
图2是涡轮发动机隔声舱体的外部结构示意图。
其中，1.排风消音器，2.进气房，3.隔声门，4.进风消音器，5.进气消音器，6.进气过滤器，7.涡轮发动机，8.进气管道，9.进风风机，10.排气管道。
具体实施方式
如图1至2所示，一种涡轮发动机的隔声舱体，所述隔声舱体套设于涡轮发动机7上，所述隔声舱体包括舱本体，进气降噪单元和通风降噪单元，所述进气降噪单元和通风降噪单元设在舱本体上，所述舱本体的框架四周填充隔音材料，所述进气降噪单元用于涡轮发动机7的进气降噪，所述通风降噪单元用于涡轮发动机7的通风系统降噪。隔音材料可以是玻璃纤维棉，岩棉，聚氨酯，铝蜂窝板，峰型棉等。
所述进气降噪单元包括进气过滤器6，进气消音器5，进气房2和进气管道，所述进气房2设在舱本体的顶部，在进气房2的外侧面设置进气过滤器6，在进气房2的内侧面设置进气消音器5，进气过滤器6与进气消音器5的位置相对应，在进气房2的底面设有出气口，进气房2通过该出气口与进气管道的一端连接，进气管道另一端与涡轮发动机7的进气口连接。在进气房2的顶面和底面均填充有隔音材料。
在所述涡轮发动机7的排气端不设置进气过滤器6和进气消音器5。排气端为涡轮发动机7的排气管道10所在端。在排气端一侧的进气房2侧面上，也可以填充隔音材料。
所述通风降噪单元包括进风消音器4，进风风机和排风消音器1，所述进风消音器4和进风风机连接，所述进风消音器4、进风风机和排风消音器1设在舱本体上，所述进风消音器4与排风消音器1相对设置在舱本体的两侧。
所述通风降噪单元为1组以上。例如，可以在涡轮发动机7传动方向的 两侧分别设置一组。其中每组通风降噪单元中的排风消音器1可设置为1个或2个。由此可以更好地起到通风降噪的作用。
在涡轮发动机7非传动方向上设有隔声门3，所述隔声门3填充隔音材料。隔声门3可设置多个，填充有隔音材料的多个隔声门3既能起到对涡轮发动机7非传动方向上的隔音，又能很好的方便维修和日常维护。
工作原理：
用于涡轮发动机7燃烧的空气由进气过滤器6进入，经进气消音器5进入进气房2内，然后经进气管道进入涡轮发动机7的进气口。
用于涡轮发动机7通风、冷却的空气在进风风机的作用下，经进风消音器4进入发动机隔声舱体内，然后经排风消音器1排放到发动机隔声舱体的外部。
本行业的技术人员应该了解，本发明不受上述实施例的限制，上述实施例和说明书中描述的只是说明本发明的原理，在不脱离本发明精神和范围的前提下，本发明还会有各种变化和改进，这些变化和改进都落入要求保护的本发明范围内。本发明要求保护范围由所附的权利要求书及其等效物界定。

Claims (6)

  1. 一种涡轮发动机的隔声舱体，其特征在于：所述隔声舱体套设于涡轮发动机上，所述隔声舱体包括舱本体，进气降噪单元和通风降噪单元，所述进气降噪单元和通风降噪单元设在舱本体上，所述舱本体的四周填充隔音材料，所述进气降噪单元用于涡轮发动机的进气降噪，所述通风降噪单元用于涡轮发动机的通风系统降噪。
  2. 根据权利要求1所述的涡轮发动机的隔声舱体，其特征在于：所述进气降噪单元包括进气过滤器，进气消音器，进气房和进气管道，所述进气房设在舱本体的顶部，在进气房的外侧面设置进气过滤器，在进气房的内侧面设置进气消音器，进气过滤器与进气消音器的位置相对应，进气房通过进气管道与涡轮发动机的进气口连接。
  3. 根据权利要求2所述的涡轮发动机的隔声舱体，其特征在于：在所述涡轮发动机的排气端不设置进气过滤器和进气消音器。
  4. 根据权利要求1所述的涡轮发动机的隔声舱体，其特征在于：所述通风降噪单元包括进风消音器，进风风机和排风消音器，所述进风消音器和进风风机连接，所述进风消音器、进风风机和排风消音器设在舱本体上，所述进风消音器与排风消音器相对设置在舱本体的两侧。
  5. 根据权利要求1所述的涡轮发动机的隔声舱体，其特征在于：所述通风降噪单元为1组以上。
  6. 根据权利要求1所述的涡轮发动机的隔声舱体，其特征在于：在涡轮发动机非传动方向上设有隔声门，所述隔声门填充隔音材料。
PCT/CN2019/104716 2019-09-06 2019-09-06 一种涡轮发动机的隔声舱体 WO2021042371A1 (zh)

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101713335A (zh) * 2008-10-01 2010-05-26 通用电气公司 声音衰减系统和方法
CN201963435U (zh) * 2011-03-09 2011-09-07 福建明辉机电有限公司 一种柴油机空滤器进气消声机构
CN205578120U (zh) * 2016-04-18 2016-09-14 德阳东汽电站机械制造有限公司 重型燃气轮机罩壳
CN106499507A (zh) * 2016-12-19 2017-03-15 湖北鹰牌动力科技有限公司 一种静音发电机组
CN109578142A (zh) * 2018-11-14 2019-04-05 株洲航发动科南方燃气轮机有限公司 集成式燃气轮机机组箱装体

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101713335A (zh) * 2008-10-01 2010-05-26 通用电气公司 声音衰减系统和方法
CN201963435U (zh) * 2011-03-09 2011-09-07 福建明辉机电有限公司 一种柴油机空滤器进气消声机构
CN205578120U (zh) * 2016-04-18 2016-09-14 德阳东汽电站机械制造有限公司 重型燃气轮机罩壳
CN106499507A (zh) * 2016-12-19 2017-03-15 湖北鹰牌动力科技有限公司 一种静音发电机组
CN109578142A (zh) * 2018-11-14 2019-04-05 株洲航发动科南方燃气轮机有限公司 集成式燃气轮机机组箱装体

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