The present invention relates to the technical field of noise reduction, and specifically to a soundproof cabin of a turbine engine.
In fracturing operation site of oil and gas fields all over the world, noise disturbance from fracturing equipment has been bothering oilfield service companies for a long time. Especially in some well sites close to residential areas, the noise causes the equipment to be unable to operate at night, thus delaying the fracturing process.
With the development of fracturing equipment technology, fracturing equipment with turbine engine as the power source appears. Although the turbine engine has many advantages compared with traditional diesel engines, for example, it has a high single power density, it can use 100% natural gas as the fuel to reduce the construction cost, etc. However, turbine engines are much noisier than diesel engines, and this problem has not been effectively addressed.
Therefore, there is an urgent need for a soundproof cabin of a turbine engine to solve the problem of turbine engine noise.
To overcome the deficiencies in the prior art, an objective of the present invention is to provide a soundproof cabin of a turbine engine, an induction noise reduction unit is disposed at an air inlet of the turbine engine to reduce the induction noise of the turbine engine; a ventilation noise reduction unit is disposed on the transmission direction of the turbine engine to reduce the ventilation and cooling noise of the turbine engine; the surrounding of the turbine engine is filled with soundproof materials to achieve the overall noise reduction around the turbine engine.
The objective of the present invention is achieved by the following technical measures. For example, a soundproof cabin of a turbine engine is disclosed. The soundproof cabin is sleeved on the turbine engine. The soundproof cabin includes a cabin body, an induction noise reduction unit and a ventilation noise reduction unit. The induction noise reduction unit and the ventilation noise reduction unit are disposed on the cabin body. The surrounding of the cabin body frame is filled with soundproof materials. The induction noise reduction unit is used to reduce the induction noise of the turbine engine. The ventilation noise reduction unit is used to reduce the noise of the ventilation system of the turbine engine.
Further, the induction noise reduction unit includes an intake filter, an intake silencer, an intake chamber and an intake piping. The intake chamber is disposed on the top of the cabin body. The intake filter is arranged on the outer side face of the intake chamber. The intake silencer is arranged on the inner side face of the intake chamber, with the position of the intake filter corresponding to that of the intake silencer. The intake chamber is connected to an air inlet of the turbine engine through the intake piping.
Further, there may be no intake filters and intake silencers arranged at the exhaust end of the turbine engine.
Further, the ventilation noise reduction unit includes an inlet air silencer, an inlet air fan and an outlet air silencer. The inlet air silencer is connected to the inlet air fan. The inlet air silencer, the inlet air fan and the outlet air silencer are disposed on the cabin body, and the inlet air silencer and the outlet air silencer are arranged on opposite sides of the cabin body.
Further, there may be one or more sets of ventilation noise reduction unit.
Further, the turbine engine is provided with a soundproof door in non-transmission direction. The soundproof door is filled with soundproof materials.
This aspects of the systems disclosed herein has the following beneficial feature and/or effects: an induction noise reduction unit is disposed at an air inlet of the turbine engine to reduce the induction noise of the turbine engine; a ventilation noise reduction unit is disposed on the transmission direction of the turbine engine to reduce the ventilation and cooling noise of the turbine engine; the surrounding of the turbine engine is filled with soundproof materials to achieve the overall noise reduction around the turbine engine; and a soundproof door filled with soundproof materials is arranged for noise insulation of the turbine engine in non-transmission direction, offering improved convenience for repair and daily maintenance.
The present invention will be described in detail below with reference to the accompanying drawings and specific implementations.
Wherein, 1. outlet air silencer, 2. intake chamber. 3. soundproof door, 4. inlet aft silencer, 5. intake silencer, 6. intake filter, 7. turbine engine, 8. intake piping, 9. inlet air fan, 10. exhaust duct.
As shown in
The induction noise reduction unit may include an intake filter 6, an intake silencer 5, an intake chamber 2 and an intake piping. The intake chamber 2 may be disposed on the top of the cabin body. The intake filter 6 may be arranged on the outer side face of the intake chamber 2, and the intake silencer 5 may be arranged on the inner side face of the intake chamber 2, with the position of the intake filter 6 corresponding to that of the intake silencer 5. The bottom of the intake chamber 2 may be provided with an air outlet, through which the intake chamber 2 is connected to one end of the intake piping. The other end of the intake piping may be connected to an air inlet of the turbine engine 7. Both the top and bottom surfaces of the intake chamber 2 may be filled with soundproof materials. As shown in
There may be no intake filters 6 and intake silencers 5 arranged at the exhaust end of the turbine engine 7. The exhaust end refers to the end at which the exhaust duct 10 of the turbine engine 7 is disposed. The side face of the intake chamber 2 at the side of the exhaust end can also be filled with soundproof materials.
The ventilation noise reduction unit may include an inlet air silencer 4, an inlet air fan and an outlet air silencer 1, wherein the inlet air silencer 4 is connected to the inlet air fan. The inlet air silencer 4, the inlet air fan and the outlet air silencer 1 may be disposed on the cabin body. The inlet air silencer 4 and the outlet air silencer 1 may be arranged on opposite sides of the cabin body.
There may be one or more sets of ventilation noise reduction units. For example, either side of the transmission direction of the turbine engine 7 can be provided with a set of ventilation noise reduction units. Likewise, there may be one, two or more outlet air silencers 1 in each set of ventilation noise reduction unit, thus better effectuating ventilation and noise reduction.
The turbine engine 7 may be further provided with a soundproof door 3 in non-transmission direction, which may be filled with soundproof materials. There may be multiple soundproof doors 3. The multiple soundproof doors filled with soundproof materials may be used for noise insulation of the turbine engine 7 in non-transmission direction, and also offer convenience for repair and daily maintenance.
Operating Principle:
The air used for combustion in the turbine engine 7 is fed through the intake filter 6, enters the intake chamber 2 through the intake silencer 5, and then enters the air inlet of the turbine engine 7 through the intake piping.
The air used for ventilation and cooling in the turbine engine 7 may be fed, under the action of the inlet air fan, into the soundproof cabin of the engine through the inlet air silencer 4, and then discharged to the outside of the soundproof cabin of the engine through the outlet air silencer 1.
It will be appreciated to persons skilled in the art that the present invention is not limited to the foregoing embodiments, which together with the context described in the specification are only used to illustrate the principle of the present invention. Various changes and improvements may be made to the present invention without departing from the spirit and scope of the present invention. All these changes and improvements shall fall within the protection scope of the present invention. The protection scope of the present invention is defined by the appended claims and equivalents thereof.
Number | Date | Country | Kind |
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201910843129.1 | Sep 2019 | CN | national |
This application is continuation application of and claims the benefit of priority to U.S. patent application Ser. No. 16/832,214, filed on Mar. 27, 2020 and entitled “Soundproof Cabin of Turbine Engine,” which is based on Chinese Patent Application No. 201910843129.1, filed on Sep. 6, 2019. These prior patent applications are herein incorporated by reference in their entireties.
Number | Date | Country | |
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Parent | 16832214 | Mar 2020 | US |
Child | 17889101 | US |