CN211234970U - Supersonic engine test bed thrust measurement exhaust apparatus - Google Patents

Abstract

A supersonic engine test bed thrust measurement exhaust device comprises an engine thrust measurement rack, an exhaust system, a tail gas treatment system and a high-altitude simulation cabin; the high-altitude simulation cabin is of a sealed shell structure, the engine thrust measurement rack is fixedly arranged in the high-altitude simulation cabin, and the tested engine is arranged on the engine thrust measurement rack; one end of the exhaust system penetrates through the surface of the shell of the high-altitude simulation cabin and is fixedly installed in the high-altitude simulation cabin, and the other end of the exhaust system is fixedly communicated with the tail gas treatment system. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, its engine thrust measurement rack has realized the measurement of engine thrust, simple structure, simultaneously, has realized the processing of engine test bench tail gas, makes and accords with national pollutant emission standard by alkaline spray column gas outlet combustion gas. Through setting up the amortization tower, carried out the amortization and fallen the noise to exhaust system's exhaust, avoided noise pollution.

Description

Supersonic engine test bed thrust measurement exhaust apparatus

Technical Field

The utility model belongs to the technical field of the engine test technique and specifically relates to a supersonic engine test bench thrust measurement exhaust apparatus.

Background

The engine test and test technology is an important component of the solid propulsion technology, and the thrust measurement is an important parameter to be measured in the engine test and test. To study engine thrust, numerous trial and error tests are required, which are not possible if all are put into flight tests. The main reasons are high flight test cost, long period, small information yield, risk and large manpower consumption. The engine ground test is to perform static test on the system according to specific conditions and environmental requirements on the ground to obtain various performance index information describing the system so as to solve the key problem in the engine thrust test process.

Secondly, aiming at the engine test beds of the aerospace engines such as the turbofan engine and the solid impact engine, the main components of the exhaust gas are carbon dioxide and hydrogen sulfide and contain certain particulate matters, the particulate matters mainly comprise diboron trioxide and magnesium oxide, if the exhaust gas exhausted by the test beds is directly exhausted into the atmosphere, the atmosphere is greatly polluted, acid rain is generated, meanwhile, pollutants such as PM10 and PM2.5 can be formed on the exhausted particulate matters to pollute the atmosphere, the method is not environment-friendly, and in the prior art, no mature and effective method exists for treating the exhaust gas of the engine test beds of the aerospace engines such as the turbofan engine and the solid impact engine.

In addition, the noise sources polluting various workplaces and surrounding environments of the engine test bed mainly come from aerodynamic noise, and the noise sources only exist in the test bed, and when high-pressure, high-speed and high-temperature compressed air and fuel gas flow in a metal or other building envelope or are discharged to the atmosphere, the noise is generated to be more than 130dB (A). Noise is unnecessary sound, the frequency of sound that can be heard by human ears is within 20HZ to 20000HZ, which is directly perceived by human beings, and noise outside this frequency is not perceived by human ears as a silent killer, and is also the object of noise control. At present, each country regulates noise to be controlled within different sound pressure levels according to different environments. According to the relevant regulations of the domestic environmental protection law, the noise sound pressure level of a newly built enterprise working for 8 hours every day is allowed to be 85dB (A), and the noise sound pressure level of the newly built enterprise working for 1 hour every day is allowed to be 94dB (A). For the engine test bed with the acoustic power larger than 130dB (A), short action time and the working place far away from towns and residential areas, the noise control aims to ensure that the noise of the working place of the test bed staff reaches the specified index and reduce the noise of the environment outside the test bed as far as possible.

For the method of noise reduction of noise generation of the test bed, the prior art has not been a very mature and effective technical means, and the applicant previously applied CN203910262U and proposed a muffler, which has a certain effect on noise reduction of the test bed, but the way of staggered arrangement of the thick components and the thin components of the muffler needs a larger floor area, on one hand, when the exhaust flow of the engine test bed is small, in order to ensure the noise reduction quality, a plurality of thick components and thin components (each layer of the muffler component needs at least 2 thick components of the muffler and 2 thin components of the muffler, and the other half of the muffler thick components and half of the muffler thin components) still need to be established, resulting in a great increase in cost; on the other hand, when the floor area of the engine test stand, which allows the installation of the muffler device, is small and does not allow the thick sheet component and the thin sheet component of the muffler as described in this patent application to be provided for each layer in a staggered arrangement, the elimination of any one muffler sheet leads to a reduction in the sound-deadening ability.

Disclosure of Invention

The technical solution problem of the utility model is that: the supersonic engine test bed thrust measurement exhaust device overcomes the defects of the prior art.

The technical solution of the utility model is that: a supersonic engine test bed thrust measurement exhaust device comprises an engine thrust measurement rack, an exhaust system, a tail gas treatment system and a high-altitude simulation cabin; the high-altitude simulation cabin is of a sealed shell structure, the engine thrust measurement rack is fixedly arranged in the high-altitude simulation cabin, and the tested engine is arranged on the engine thrust measurement rack; one end of the exhaust system penetrates through the surface of the shell of the high-altitude simulation cabin and is fixedly installed in the high-altitude simulation cabin, and the other end of the exhaust system is fixedly communicated with the tail gas treatment system.

Compared with the prior art, the utility model the advantage lie in:

1. the utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, its engine thrust measurement rack has realized the measurement of engine thrust, simple structure.

2. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, its engine thrust measurement rack, ingenious will move the frame and hang on the shelf location through the spring leaf to the thrust of assisting force transducer measurement engine, simple and easy.

3. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, in its engine thrust measurement rack, set up the measurement section bracket to the measurement section that is used for guaranteeing to be used for measuring the air inlet parameter of the engine under test is coaxial with the engine, has both guaranteed the engine precision of the simulation of admitting air, has improved the engine precision of parameter measurement of admitting air again.

4. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, in its engine thrust measurement rack, it moves a set of global rigidity great, in order to guarantee test frame dynamic behavior, reasonable distribution atress component in the design adopts intensity principle such as structure, removes optimization design such as not atress part of material, alleviates and moves a quality.

5. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, in its engine thrust measurement rack, its decides the frame and sets up horizontal base, improves the load capacity of whole frame.

6. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, in its engine thrust measurement rack, set up locking state, when making the engine install the engine before not test condition or experiment, move the frame and keep the fixed state with the stationary frame, the life of engine thrust measurement rack has been prolonged, avoid exerting irreversible external force and causing the damage even to the spring leaf when moving the frame and installing engine under the self-condition (not using locking state) and relevant testpieces simultaneously, the precision of engine thrust measurement rack has been guaranteed.

7. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, in its engine thrust measurement rack, adopt planer-type engine mounting bracket, hang the engine and set up, improved the measurement accuracy of engine thrust to it is adjustable with the rear joint position to set up the front connector, improved the application scope of engine mounting bracket by a wide margin, solved the problem that an engine set up an engine mounting bracket in the past.

8. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, in its engine thrust measurement rack, adopt standard force sensor to carry out the error of working force sensor to the working force sensor and confirm, static calibration, known "simulation thrust" that produces a set of high accuracy from this carries out the degree of definite to force measuring system, because it has reappeared the deformation and the atress condition of test condition, eliminated because the deformation that produces during the experiment, the installation, the temperature, the most system error that causes such as restraint, thereby the uncertainty of thrust measurement has been reduced.

9. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, in its engine thrust measurement rack, draw the characteristic curve graph of standard force sensor and working force sensor through demarcating, pass through the true value of the accurate definite force of characteristic curve graph with the power value of working force sensor output, avoided experimental calibration to the working force sensor at every turn, it is with low costs, efficient.

10. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, spray the platform through setting up confined circulating water pond and 2 sets of alkalis, the processing of engine test bench tail gas has been realized, make and accord with national pollutant emission standard by the gas of basicity spray column gas outlet, set up 2 parallelly connected alkalis of cover and spray the platform, make engine test bench tail gas fall into 2 ways and carry out the alkalis and spray, the velocity of flow of engine test bench tail gas through the alkalis spray column has been reduced, it is more abundant to make the alkalis spray the process, the work load of every alkalis spray column has been reduced simultaneously, further abundant alkalis of having carried out spray, and simultaneously, through setting up the amortization tower, exhaust to exhaust system has carried out the amortization and has fallen the noise.

11. The utility model provides a supersonic engine test bed thrust measurement exhaust apparatus, in the amortization process, creatively provides thin thick combination amortization piece plain film, has realized that thin amortization piece and thick amortization piece have been set up respectively in an air current passageway 2 side, under the prerequisite of guaranteeing the noise-damping capacity, has reduced the use quantity of amortization piece (thick piece subassembly and the thin piece subassembly of half silencer are added to the thick piece subassembly that needs 2 silencers at least for each layer of amortization piece subassembly of prior art and the thin piece subassembly of 2 silencers, the utility model provides an each layer of amortization piece subassembly is equivalent to only needing the thick piece subassembly of 1 silencer and the thin piece subassembly of 1 silencer and the thick piece subassembly and the thin piece subassembly of half silencer in addition), area is little (also be applicable to the small flow engine test bed when being suitable for the test bed), the application range is wide, and the cost is greatly reduced.

12. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, at the amortization in-process, it sets up the water conservancy diversion piece on the amortization piece, to the gaseous water conservancy diversion that gets into airflow channel for gas flow is even, has further improved the amortization efficiency.

13. The utility model discloses a supersonic engine test bench thrust measurement exhaust apparatus, its engine test bench tail gas processing system, creative set up 2 layers of spraying system in every basicity spray column, make and spray more thoroughly.

14. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, in its engine test bench tail gas processing system, it has ceramic material's packing layer to set up to pack in every layer of spraying system, has improved the throughput of alkaline spray column by a wide margin.

15. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust, among its engine test bench tail gas processing system, through setting up circulating water pond, waste water treatment equipment and closed cooling tower have realized the reuse of alkaline circulating water, and testing cost reduces by a wide margin.

16. The utility model discloses an exhaust apparatus is measured to supersonic engine test bench thrust has add spraying system in the amortization tower, and further tail gas carries out degradation for the tail gas treatment capacity further improves.

Drawings

Fig. 1 is the structure schematic diagram of the supersonic engine test bed thrust measurement exhaust device of the utility model.

Fig. 2 is the utility model discloses an among the supersonic engine test bench thrust measurement exhaust apparatus, the structure elevation of engine thrust measurement rack.

Fig. 3 is an enlarged view of a portion a in fig. 2.

Fig. 4 is an enlarged view of a portion B in fig. 2.

Fig. 5 is the utility model discloses an among the supersonic engine test bench thrust measurement exhaust apparatus, engine thrust measures rack construction top view.

Fig. 6 is an enlarged view of the portion C of fig. 5.

Fig. 7 is the utility model discloses an among the supersonic engine test bench thrust measurement exhaust apparatus, the structural sketch of the measurement section bracket of engine thrust measurement rack.

Fig. 8 is an enlarged view of a portion D in fig. 7.

Fig. 9 is an enlarged view of a portion E of fig. 7.

Fig. 10 is a front view of the engine mounting rack of the engine thrust measuring rack in the thrust measuring exhaust device of the supersonic engine test stand of the present invention.

Fig. 11 is a side view of the structure of the engine mounting bracket of the engine thrust measuring rack in the supersonic engine test stand thrust measuring exhaust device of the present invention.

Fig. 12 is the structure diagram of the engine mounting top frame of the engine thrust measuring rack in the thrust measuring exhaust device of the supersonic engine test stand of the present invention.

Fig. 13 is the utility model discloses an among the supersonic engine test bench thrust measurement exhaust apparatus, the principle sketch map of the force sensor calibration of engine thrust measurement rack.

FIG. 14 is the schematic structural diagram of the alkali liquor spray tower of the engine test stand tail gas treatment system in the supersonic engine test stand thrust measurement exhaust device of the present invention.

Fig. 15 is the schematic structural diagram of 3 layers of noise reduction sheet assemblies of the engine test stand tail gas treatment system in the supersonic engine test stand thrust measurement exhaust device of the present invention.

Fig. 16 is a schematic structural diagram of a layer 1 noise reduction sheet assembly of an engine test stand tail gas treatment system in the supersonic engine test stand thrust measurement exhaust device of the present invention.

Fig. 17 is the structure diagram of the semi-thin silencing sheet of the engine test stand tail gas treatment system in the supersonic engine test stand thrust measurement exhaust device of the present invention.

Fig. 18 is the structure diagram of the half-thickness silencing sheet of the tail gas treatment system of the supersonic engine test stand in the thrust measurement exhaust device of the supersonic engine test stand.

Fig. 19 is a schematic structural diagram of a thin and thick combined noise damping sheet of an engine test stand tail gas treatment system in the supersonic engine test stand thrust measurement exhaust device of the present invention.

Detailed Description

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", and the like, indicate the orientation or positional relationship indicated based on the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention. Furthermore, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted", "connected" and "abutted" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

A supersonic speed engine, especially a test bed thrust measurement exhaust apparatus of aerospace engines such as turbofan engine, solid rush engine, etc., includes the engine thrust measures the rack, exhaust system 700, tail gas treatment system and high altitude simulation cabin 900; the high-altitude simulation cabin 900 is a sealed shell structure, the shape of the high-altitude simulation cabin is not limited, and the high-altitude simulation cabin can be a cuboid, an ellipsoid and the like; the engine thrust measuring rack is fixedly arranged in the high-altitude simulation cabin 900, and the tested engine 1 is arranged on the engine thrust measuring rack; one end of the exhaust system 700 penetrates through the surface of the shell of the high-altitude simulation cabin 900 and is fixedly installed inside the high-altitude simulation cabin 900, and the other end of the exhaust system is fixedly communicated with the tail gas treatment system.

The engine thrust measuring rack comprises a fixed rack 100, a movable rack 200 and a loading measuring device; the loading measuring device comprises a spring piece, a loading mechanism 330 and a working force sensor 350; the movable frame 200 is suspended on the fixed frame 100 through the spring plate, the loading mechanism 330 is fixedly mounted on the fixed frame 100, and two ends of the working force sensor 350 are respectively connected with the fixed frame 100 and the movable frame 200.

The fixed frame comprises a base 110, a front mounting seat 120, a loading mechanism mounting seat 130, a first fixed frame spring piece mounting seat 140, a fixed frame working force sensor mounting seat 150, a rear mounting seat 160 and a second fixed frame spring piece mounting seat 170; the base 110 is of a cuboid structure, the front mounting seat 120 and the rear mounting seat 160 are respectively and fixedly mounted at the front end and the rear end of the base 110 along the length direction of the base 110, the rear mounting seat 160 comprises a transverse plate and a vertical plate, and the transverse plate and the vertical plate form an L shape; the loading mechanism mounting seat 130 is fixedly mounted on the front mounting seat 120, the first fixed frame spring leaf mounting seat 140 includes a first right fixed frame spring leaf mounting seat 141 and a first left fixed frame spring leaf mounting seat 142, and the first right fixed frame spring leaf mounting seat 141 and the first left fixed frame spring leaf mounting seat 142 are fixedly mounted at the front end of the base 110 and are respectively located on two sides of the front mounting seat 120; the fixed frame working force sensor mounting seat 150 is fixedly mounted on the base 110 and is positioned on a central line along the length direction of the base 110; the second fixed frame spring piece mounting seat 170 includes a second right fixed frame spring piece mounting seat 171 and a second left fixed frame spring piece mounting seat 172, and the second right fixed frame spring piece mounting seat 171 and the second left fixed frame spring piece mounting seat 172 are fixedly mounted at the rear end of the base 110 and respectively located at two sides of the rear mounting seat 160.

The movable frame 200 comprises a movable frame body 210, a first movable frame spring piece mounting seat 220, a movable frame working force sensor mounting seat 230, a second movable frame spring piece mounting seat 240 and a movable frame standard force sensor mounting seat 250, wherein the movable frame body 210 comprises a right movable frame body 211, a left movable frame body 212 and a movable frame connecting plate 260, the right movable frame body 211 and the left movable frame body 212 are identical in structure, both of which are cuboid structures and are parallel to the base 110, the central line of the right movable frame body 211 and the left movable frame body 212 in the length direction is parallel to the central line of the base 110 in the length direction, the right movable frame body 211 and the left movable frame body 212 are symmetrically arranged relative to the central line of the base 110 in the length direction, the number of the movable frame connecting plates 260 is multiple, and the right movable frame body 211 and the left movable frame body 212 are fixedly connected by the plurality of the movable frame connecting plates 260; along the length direction of the movable frame body 210, a movable frame standard force sensor mounting seat 250 is fixedly mounted on the bottom surface of the front end of the movable frame body 210; the first moving frame spring piece mounting seat 220 comprises a first right moving frame spring piece mounting seat and a first left moving frame spring piece mounting seat, and the first right moving frame spring piece mounting seat and the first left moving frame spring piece mounting seat are respectively fixedly mounted on the bottom surfaces of the front ends of the right moving frame body 211 and the left moving frame body 212 and are respectively positioned on two sides of the moving frame standard force sensor mounting seat 250; the movable frame working force sensor mounting base 230 is fixedly mounted at the bottom of one movable frame connecting plate 260 of the movable frame body 210 and is located on a central line along the length direction of the movable frame body 210; the second moving frame spring piece mounting seat 240 comprises a second right moving frame spring piece mounting seat and a second left moving frame spring piece mounting seat, and the second right moving frame spring piece mounting seat and the second left moving frame spring piece mounting seat are fixedly mounted on the bottom surfaces of the rear ends of the right moving frame body 211 and the left moving frame body 212 respectively.

The loading measuring device comprises a first spring plate 310, a second spring plate 320, a loading mechanism 330, a standard force sensor 340 and a working force sensor 350; the first spring piece 310 comprises a first right spring piece 311 and a first left spring piece 312, two ends of the first right spring piece 311 are respectively and fixedly connected with a first right fixed frame spring piece mounting seat 141 and a first right movable frame spring piece mounting seat, and two ends of the first left spring piece 312 are respectively and fixedly connected with a first left fixed frame spring piece mounting seat 142 and a first left movable frame spring piece mounting seat; the second spring piece 320 comprises a second right spring piece 321 and a second left spring piece 322, two ends of the second right spring piece 321 are fixedly connected with the second right fixed frame spring piece mounting seat 171 and the second right movable frame spring piece mounting seat respectively, and two ends of the second left spring piece 322 are fixedly connected with the second left fixed frame spring piece mounting seat 172 and the second left movable frame spring piece mounting seat respectively; the loading mechanism 330 is fixedly mounted on a transverse plate of the front mounting seat 120, the standard force sensor 340 is fixedly mounted on a baffle plate at the front end of the movable frame body 210, and the loading mechanism 330 and the standard force sensor 340 are coaxially arranged and are parallel to the central line of the base 110 along the length direction; two ends of the working force sensor 350 are respectively and fixedly connected with the fixed frame working force sensor mounting seat 150 and the movable frame working force sensor mounting seat 230, and the working force sensor 350, the loading mechanism 330 and the standard force sensor 340 are coaxially arranged; the loading mechanism 330 comprises a servo motor, a motor power supply, a hydraulic loading device and a calibration oil cylinder, wherein the motor power supply is electrically connected with the servo motor, the servo motor is sequentially connected with the hydraulic loading device and the calibration oil cylinder, and a piston of the calibration oil cylinder is connected with a standard force sensor.

The engine thrust measuring rack comprises a measuring section bracket for supporting a measuring section, the measuring section bracket comprises a first measuring section bracket 410 and a second measuring section bracket 420 which are coaxially arranged, and the first measuring section bracket 410 and the second measuring section bracket 420 have the same structure and are both fixedly arranged on the top surface of the movable rack body 210; the measuring section bracket comprises a measuring section bracket 411, a measuring section bracket lower ring 412, a measuring section bracket upper ring 413, a measuring section bracket positioning mechanism 414 and a locking device 415; the bottom surface of the measurement section bracket 411 is fixedly connected with the top surface of the movable frame body 210, the measurement section bracket lower ring 412 and the measurement section bracket upper ring 413 are both of a semicircular structure, and the measurement section bracket lower ring 412 and the measurement section bracket upper ring 413 are connected to form a circle; the measuring section bracket lower ring 412 and the measuring section bracket 411 are integrally formed; the number of the measuring section bracket positioning mechanisms 414 is 3, the structures of the measuring section bracket positioning mechanisms are the same, and the measuring section bracket positioning mechanisms 414 are used for positioning and measuring the measuring sections of the intake parameters of the tested engine 1, the 3 measuring section bracket positioning mechanisms 414 are uniformly distributed along the radial direction of a circle formed by connecting the measuring section bracket lower ring 412 and the measuring section bracket upper ring 413, wherein one measuring section bracket positioning mechanism 414 is arranged at the top of the measuring section bracket upper ring 413, and the rest 2 measuring section bracket positioning mechanisms 414 are arranged on the measuring section bracket lower ring 412; the measuring section bracket positioning mechanism 414 comprises a positioning mechanism nut 4141, a positioning mechanism locking nut 4142 and a positioning mechanism screw 4143, the positioning mechanism screw 4143 passes through the measuring section bracket lower ring 412 or the measuring section bracket upper ring 413, the positioning mechanism locking nut 4142 is sleeved on the positioning mechanism screw 4143, is arranged on the outer side of the measuring section bracket lower ring 412 or the measuring section bracket upper ring 413 and is abutted against the measuring section bracket lower ring 412 or the measuring section bracket upper ring 413 and is used for locking the positioning mechanism screw 4143, and the positioning mechanism nut 4141 is sleeved on the positioning mechanism screw 4143 and is abutted against the positioning mechanism locking nut 4142; the number of the locking devices 415 is 2, and the structures of the locking devices are the same, and the locking devices 415 are used for fixedly connecting the lower ring 412 of the measurement section bracket and the upper ring 413 of the measurement section bracket, 2 locking devices 415 are arranged at the connecting ends of the lower ring 412 of the measurement section bracket and the upper ring 413 of the measurement section bracket, the locking device 415 includes an upper locking plate 4151, a lower locking plate 4152, a locking bolt 4153 and a locking nut 4154, the upper locking plate 4151 is fixedly attached to the front end surface of the upper ring 413 of the measurement section bracket, the lower surface of the upper locking plate 4151 coincides with the lower surface of the upper ring 413 of the measurement section bracket, the lower locking plate 4152 is fixedly attached to the front end surface of the measuring section bracket lower ring 412, the upper surface of the lower lock plate 4152 coincides with the upper surface of the measuring section bracket lower ring 412, the locking bolt 4153 passes through the lower and upper locking plates 4152 and 4151 in sequence, the lock nut 4154 is engaged with the lock bolt 4153 and abuts against the upper lock plate 4151.

The engine thrust measuring rack comprises a locking device, the locking device comprises a fastening screw rod 510, a fastening baffle 520 and a fastening nut 530, the fastening screw rod 510 sequentially penetrates through a rear end baffle of the movable rack body 210, the fastening baffle 520, a vertical plate and a fastening nut 530 of the rear mounting seat 160, the fastening nut 530 is matched with the fastening screw rod 510, and the fastening baffle 520 and the fastening nut 530 are both abutted to the vertical plate of the rear mounting seat 160.

The engine thrust measuring rack comprises an engine mounting rack 600, wherein the engine mounting rack 600 comprises an engine mounting top rack 610, a left upright column 620 and a right upright column 630 which are identical in structure, a front joint 640, a rear joint 650 and a lifting lug 660; the bottom surfaces of the left upright post 620 and the right upright post 630 are detachably connected with the movable frame 200; the engine mounting top frame 610 is fixedly connected with the top surfaces of the left upright column 620 and the right upright column 630 to form a gantry type, the front joint 640 and the rear joint 650 are detachably mounted on the engine mounting top frame 610, and the lifting lug 660 is fixedly connected with the engine mounting top frame 610; the engine mounting top frame 610 comprises a front beam 611, a rear beam 612 and a longitudinal beam 613, wherein the front beam 611 and the rear beam 612 are arranged in parallel and are fixedly connected with the longitudinal beam 613, the rear beam 612 is fixedly connected with one end of the longitudinal beam 613, and the front beam 611, the rear beam 612 and the longitudinal beam 613 form a shape like the Chinese character 'tu'; the longitudinal beam 613 is provided with a mounting hole 614 for mounting a front joint 640 and a rear joint 650; the left upright post 620 comprises a front post 621, a rear post 622 and upright post connecting rods 623, wherein the front post 621 and the rear post 622 are arranged in parallel and are fixedly connected through the upright post connecting rods 623.

The engine thrust measurement rack comprises a force sensor calibration device, and the force sensor calibration device comprises an industrial personal computer, a display, a standard force sensor data acquisition device and a working force sensor data acquisition device; the industrial personal computer is respectively electrically connected with the display and the servo motor, the standard force sensor data acquisition device is respectively electrically connected with the standard force sensor and the industrial personal computer, and the working force sensor data acquisition device is respectively electrically connected with the working force sensor and the industrial personal computer.

The exhaust system 700 is prior art, see in particular the applicant's chinese utility model patent ZL201610786167.4, wherein a portion of the tail chamber section 710 of the exhaust system 700 passes through the high altitude simulation cabin 900 and is located within the high altitude simulation cabin 900; a small replaceable tail chamber is fixedly arranged in the tail chamber section 710; the outlet of the exhaust system 700 is communicated with a tail gas treatment system input pipeline 850 of the tail gas treatment system, and the tail gas treatment system input pipeline 850 is respectively communicated with the spray tower air inlets 802 of the first alkali liquor spray tower 810 and the second alkali liquor spray tower 820 of the tail gas treatment system.

The tail gas treatment system comprises a first alkali liquor spray tower 810, a second alkali liquor spray tower 820, an alkali liquor supply pool 830, a silencing tower 840 and a tail gas treatment system input pipeline 850. The alkaline liquid supply tank 830 is of a closed reinforced concrete structure, and is filled with alkaline liquid.

The first alkali liquor spraying tower 810 and the second alkali liquor spraying tower 820 are identical in structure, the first alkali liquor spraying tower 810 comprises a spraying tower body 801, a spraying tower air inlet 802, a spraying tower air outlet 803, a spraying tower alkali liquor inlet 804, a spraying tower first packing layer 805, a spraying tower first spraying system 806, a spraying tower second packing layer 807, a spraying tower second spraying system 808, a spraying tower liquid level meter 809, a spraying tower circulating pump 811, a spraying tower overflow vent 812, a spraying tower drain 813 and a spraying tower maintenance vent 814; the spray tower body 801 is of a hollow cylindrical structure, the spray tower air inlet 802, the spray tower alkali liquor inlet 804, the spray tower overflow port 812, the spray tower drain 813 and the spray tower maintenance port 814 are all arranged on the side part of the spray tower body 801, and the spray tower air outlet 803 is arranged on the top of the spray tower body 801; the spray tower gas inlets 802 of the first alkali liquor spray tower 810 and the second alkali liquor spray tower 820 are both communicated with a tail gas treatment system input pipeline 850, the spray tower gas outlets 803 are both communicated with the silencing tower 840 through pipelines, one end of a conveying pipeline for conveying alkali liquor to a spray system is communicated with the alkali liquor supply tank 830, the other end of the conveying pipeline penetrates through the spray tower alkali liquor input port 804 and is respectively communicated with the spray tower first spray system 806 and the spray tower second spray system 808, and the spray tower circulating pump 811 is arranged outside the spray tower body 801 and is used for pumping the alkali liquor in the alkali liquor supply tank 830 out and conveying the alkali liquor to the spray tower first spray system 806 and the spray tower second spray system 808 through the conveying pipeline for conveying the alkali liquor to the spray system; preferably, the conveying pipeline for conveying the alkaline liquid to the spraying system is provided with a seal through the spraying tower alkaline liquid inlet 804; the arrangement position of the spray tower overflow port 812 is higher than the spray tower air inlet 802, the spray tower alkali liquor input port 804 and the spray tower drain 813, and the spray tower drain 813 is communicated with the external wastewater treatment equipment 850 through a pipeline. Along the axis of the spray tower body 801, a first spray tower filler layer 805, a first spray tower spraying system 806, a second spray tower filler layer 807 and a second spray tower spraying system 808 are fixedly installed inside the spray tower body 801 from bottom to top in sequence, and preferably, the fillers in the first spray tower filler layer 805 and the second spray tower filler layer 807 are ceramic fillers. The spray tower liquid level meter is arranged on the side part of the spray tower body 801 and is positioned on the lower part of the first packing layer 805 of the spray tower and used for monitoring the water level of the wastewater at the bottom of the spray tower body 801.

The silencing tower 840 is of a reinforced concrete structure and comprises an inlet silencing sheet installation cavity 841 and an outlet silencing sheet installation cavity 842, the bottoms of the inlet silencing sheet installation cavity 841 and the outlet silencing sheet installation cavity 842 are communicated, an inlet silencing sheet assembly 843 is fixedly installed at the inlet silencing sheet installation cavity 841, an outlet silencing sheet assembly 844 is fixedly installed at the outlet silencing sheet installation cavity 842, the spray tower gas outlets 803 of the first alkali liquor spray tower 810 and the second alkali liquor spray tower 820 are communicated with the inlet silencing sheet installation cavity 841 of the silencing tower 840 through pipelines, and the outlets of the outlet silencing sheet installation cavity 842 are communicated with the atmosphere; in the outlet sound damping fin installation cavity 842, a lower layer spraying system 845, a middle layer spraying system 846 and an upper layer spraying system 847 are fixedly installed below the outlet sound damping fin assembly 844 from bottom to top in sequence, the lower layer spraying system 845, the middle layer spraying system 846 and the upper layer spraying system 847 are communicated with the alkaline liquid supply tank 830 through pipelines, and a pump for pumping and conveying the alkaline liquid in the alkaline liquid supply tank 830 to the lower layer spraying system 845, the middle layer spraying system 846 and the upper layer spraying system 847 is arranged outside the silencing tower 840. The inlet and outlet silencer assemblies 843, 844 are identical in construction.

The inlet silencing sheet assembly 843 comprises a lower silencing sheet assembly 888431, a middle silencing sheet assembly 888432 and an upper silencing sheet assembly 888433 which are sequentially arranged from bottom to top; each layer of silencing sheet component comprises semi-thin silencing sheets 8431, semi-thick silencing sheets 8432 and thin-thick combined silencing sheets 8433 which are arranged at intervals, in each layer of silencing sheet component, the semi-thin silencing sheets 8431 and the semi-thick silencing sheets 8432 are arranged at two ends and fixedly connected with two end faces of an inlet silencing sheet mounting cavity 841 of the silencing tower 840, a plurality of thin-thick combined silencing sheets 8433 are arranged at intervals between the semi-thin silencing sheets 8431 and the semi-thick silencing sheets 8432, and the adjacently arranged silencing sheets form an airflow channel; the method of mounting each layer of sound attenuation panel assembly and the method of attachment to the tower are known in the art, in a manner substantially in accordance with the applicant's prior application (CN 201482057351.1).

On the same end side, the types of the sound-deadening sheets of the adjacent 2 layers are different, so that the air flow passages formed by the adjacent sound-deadening sheet assemblies are staggered, and the sound-deadening capacity of the sound-deadening device is further improved, in a preferred embodiment of the present application, in the lower sound-deadening sheet assembly 888431, the sound-deadening sheets are arranged in a manner of a half-thin sound-deadening sheet 8431, a thin-thick combined sound-deadening sheet 8433 and a half-thick sound-deadening sheet 8432 along the horizontal direction of the sound-deadening tower, wherein the thick sound-deadening sheet parts in the thin-thick combined sound-deadening sheet 8433; in the middle-layer silencing piece assembly 888432, the arrangement modes of silencing pieces are a half-thick silencing piece 8432, a thin-thick combined silencing piece 8433 and a half-thin silencing piece 8431, wherein the thick silencing pieces in the thin-thick combined silencing piece 8433 face the half-thin silencing piece 8431; in the upper layer silencing piece assembly 888433, the silencing pieces are arranged in a mode of a half-thin silencing piece 8431, a thin-thick combined silencing piece 8433 and a half-thick silencing piece 8432, wherein the thick silencing pieces in the thin-thick combined silencing piece 8433 face the half-thin silencing piece 8431.

The semi-thin silencing sheet 8431 comprises a semi-thin silencing sheet flat sheet 884311 and 2 semi-thin silencing sheet flow guide conical sheets 884312, the 2 semi-thin silencing sheet flow guide conical sheets 884312 are fixedly connected with two ends of the semi-thin silencing sheet flat sheet 884311, and preferably, the 2 semi-thin silencing sheet flow guide conical sheets 884312 and the semi-thin silencing sheet flat sheet 884311 are integrally formed; the surfaces of the semi-thin silencing plate flat sheet 884311 and the semi-thin silencing plate flow guiding conical sheet 884312 are both provided with a plurality of silencing plate micropores 8434, the plurality of silencing plate micropores 8434 are through holes penetrating through the surfaces of the semi-thin silencing plate 884311 and the semi-thin silencing plate flow guiding conical sheet 884312, the structure of the semi-thin silencing plate 8431 is the prior art and is a semi-sheet structure of a sheet component in the prior application (application number: CN201482056663.0, utility model name: sheet component for silencer) of the applicant, and the gas flow guiding of an entering gas flow channel is realized by arranging the semi-thin silencing plate flow guiding conical sheet 884312, so that the gas flows uniformly, and the silencing effect is further improved.

The half-thick silencing piece 8432 comprises a half-thick silencing piece flat piece 884321 and 2 half-thick silencing piece flow guide conical pieces 884322, the 2 half-thick silencing piece flow guide conical pieces 884322 are fixedly connected with two ends of the half-thick silencing piece flat piece 884321, and preferably, the 2 half-thick silencing piece flow guide conical pieces 884322 and the half-thick silencing piece flat piece 884321 are integrally formed; the surfaces of the half-thick silencing plate flat sheet 884321 and the half-thick silencing plate flow guiding conical sheet 884322 are both provided with a plurality of silencing plate micropores 8434, and the plurality of silencing plate micropores 8434 are through holes penetrating through the surfaces of the half-thick silencing plate flat sheet 884321 and the half-thick silencing plate flow guiding conical sheet 884322; wherein, the structure of the half-thickness silencing sheet 8432 is the prior art, which is the half-sheet structure of the thin sheet component in the prior application of the applicant (application number: CN201482056662.6, utility model name: thick sheet component for silencer); the gas flow guiding of the gas entering the gas flow channel is realized by arranging the half-thick silencing sheet flow guiding conical sheet 884322, so that the gas flows uniformly, and the silencing effect is further improved.

The thin and thick combined silencing sheet 8433 is a combined sheet formed by fixedly connecting and combining the horizontal planes of the half-thin silencing sheet 8431 and the half-thick silencing sheet 8432, in the combined thin and thick combined silencing sheet 8433, the half-thin silencing sheet 884311 and the half-thick silencing sheet 884321 are arranged in parallel to form a thin and thick combined silencing sheet 884331 of the thin and thick combined silencing sheet 8433, and the 2 half-thin silencing sheet guide cone pieces 884312 and the 2 half-thick silencing sheet guide cone pieces 884322 form 2 thin and thick combined silencing sheet guide cone pieces 884332 of the thin and thick combined silencing sheet 8433; the air flow guiding of the air entering the air flow channel is realized by arranging the thin and thick combined silencing piece flow guiding conical piece 884332, so that the air flows uniformly, and the silencing effect is further improved.

The thickness of the half-thin silencing sheet 8431 is L1, the thickness of the half-thick silencing sheet 8432 is L2, and the thickness of the thin-thick combined silencing sheet 8433 is L3, wherein L1 is more than L2 and less than L3, and L3 is equal to L1+ L2.

Preferably, the diameter of the silencing sheet micro-hole 8434 is 0.6mm-1mm, and more preferably, the diameter of the silencing sheet micro-hole 8434 is 0.8 mm.

Preferably, horizontal cross sections in the inlet silencing piece installation cavity 841 and the outlet silencing piece installation cavity 842 are square channels, the wall thickness of the tower body 811 is 0.5m, and further preferably, the horizontal cross section in the tower body 811 is a square channel with a size of 0.5m × 0.5 m.

Preferably, the thickness L1 of the half-thin silencing sheet 8431 is 80mm to 85mm, and more preferably, the thickness L1 of the half-thin silencing sheet 8431 is 82 mm.

Preferably, the thickness L2 of the half-thickness silencing sheet 8432 is 195mm to 205mm, and more preferably, the thickness L2 of the half-thickness silencing sheet 8432 is 820 mm.

Preferably, the alkaline liquid supply tank 830 is provided with a water injection port for injecting municipal tap water.

Preferably, a detector for detecting the ph of the alkaline liquid in the alkaline liquid supply tank 830 and a liquid level meter for displaying the level of the alkaline liquid in the alkaline liquid supply tank 830 are disposed in the alkaline liquid supply tank 830.

Preferably, the alkaline liquid supply tank 830 is provided with a feeding port for feeding alkaline materials, so as to ensure that the alkalinity-acidity of the alkaline liquid in the alkaline liquid supply tank 830 reaches a predetermined value.

The method for measuring the thrust of the supersonic engine and treating and discharging tail gas by using the supersonic engine test bed thrust measurement exhaust device comprises the following steps:

s100), installing the tested engine 1 and measuring section

S110), sequentially enabling a measuring section for measuring engine air inlet parameters to pass through the first measuring section bracket 410 and the second measuring section bracket 420, and placing the measuring section in the first measuring section bracket 410 and the second measuring section bracket 420;

s120), mounting the front joint 640 and the rear joint 650 to the longitudinal beam 613 according to the suspension position of the engine 1 under test;

s130), mounting the engine mounting frame 600 on the movable frame body 210, and then mounting the tested engine 1 on the front joint 640 and the rear joint 650;

s140) adjusting the measuring section, connecting one end of the measuring section with the air inlet of the tested engine 1, adjusting a positioning mechanism screw 4143 in the measuring section bracket positioning mechanism 414, enabling the measuring section and the engine air inlet to be coaxial, and then sequentially rotating a positioning mechanism locking nut 4142 and a positioning mechanism nut 4141 in the measuring section bracket positioning mechanism 414.

S200), disassembling and locking device

The fastening nut 530 is loosened, the fastening screw 510 is pulled out from the vertical plate of the rear mounting seat 160, the fastening baffle 520 and the baffle at the rear end of the movable frame body 210 in sequence, and then the fastening baffle 520 is taken out.

S300), determining the error of the working force sensor

S310), the industrial personal computer controls the servo motor to start to drive the hydraulic loading device to work, the hydraulic loading device drives the calibration oil cylinder to work, a piston of the calibration oil cylinder drives the standard force sensor 340 to displace so as to drive the movable frame body 210 to displace, and force is applied to the working force sensor 350 in the displacement process of the movable frame body 210;

s320), the hydraulic loading device drives the calibration oil cylinder to work, and the loading force is unloaded to a zero value after the loading force is continuously applied to the standard force sensor 340 to a preset value; the standard force sensor data acquisition device and the working force sensor data acquisition device respectively acquire force values output by the standard force sensor 340 and the working force sensor 350 in the loading force applying and unloading processes and feed back the force values to the industrial personal computer, and the display displays the force values output by the standard force sensor 340 and the working force sensor 350 in the loading force applying and unloading processes, which are acquired by the standard force sensor data acquisition device and the working force sensor data acquisition device;

s330), drawing characteristic curve graphs of the standard force sensor 340 and the working force sensor 350 according to force values output by the standard force sensor 340 and the working force sensor 350 in the process of applying loading force and unloading loading force, wherein the force values are displayed by a display and acquired by the standard force sensor data acquisition device and the working force sensor data acquisition device; under the same loading force, the difference between the force value output by the working force sensor 350 acquired by the working force sensor data acquisition device and the force value output by the standard force sensor 340 acquired by the standard force sensor data acquisition device is the working force sensor error.

S400), starting a spraying system

S410), respectively starting a spray tower circulating pump 811 and pumps for pumping out and conveying the alkaline liquid in the alkaline liquid supply tank 830 to the lower layer spray system 845, the middle layer spray system 846 and the upper layer spray system 847, respectively pumping out and conveying the alkaline liquid in the alkaline liquid supply tank 830 to the first spray system 806 of the spray tower, the second spray system 808 of the spray tower, the lower layer spray system 845, the middle layer spray system 846 and the upper layer spray system 847 of the spray tower of the first alkali liquid spray tower 810 and the second alkali liquid spray tower 820, respectively.

S420), respectively starting the first spraying system 806 of the spraying tower, the second spraying system 808 of the spraying tower, the lower spraying system 845 of the spraying tower, the middle spraying system 846 and the upper spraying system 847 of the first alkali liquor spraying tower 810 and the second alkali liquor spraying tower 820, starting the spraying of the alkali liquor, and keeping the first spraying system 806 of the spraying tower, the second spraying system 808 of the spraying tower, the lower spraying system 845 of the spraying tower, the middle spraying system 846 and the upper spraying system 847 of the first alkali liquor spraying tower 810 and the second alkali liquor spraying tower 820 to work.

S500), simulating the high-altitude flight environment pressure of the engine

Starting an ejector in the exhaust system 700, and extracting gas in the high-altitude simulation cabin 900 to enable the pressure of the high-altitude simulation cabin 900 to be the same as the environmental pressure of the engine at the altitude in high-altitude flight;

s600), measuring thrust of tested engine

After the engine is ignited and the measurement section detects that the air inlet parameter of the tested engine 1 reaches the working condition, the display displays the force value output by the working force sensor 350 and collected by the working force sensor data collection device.

S700) and tail gas treatment

S710) and performing engine test, wherein tail gas of the engine test bed is discharged by an exhaust system (the exhaust system can be an exhaust pipeline, an ejector and the like), and enters the spray tower air inlet 802 of the first alkali liquor spray tower 810 and the second alkali liquor spray tower 820 respectively through the tail gas processing system input pipeline 850.

S720), after sequentially passing through a first packing layer 805 and a second packing layer 807 of the spray tower, the tail gas of the engine test bed entering a gas inlet 802 of the spray tower is discharged from a gas outlet 803 of the spray tower and enters an inlet silencing sheet installation cavity 841 from the top of a silencing tower 840 through a pipeline, and when the tail gas of the engine test bed passes through the first packing layer 805 of the spray tower and the second packing layer 807 of the spray tower, alkaline liquid and the tail gas of the engine test bed are subjected to degradation treatment.

S730), the gas entering the inlet silencing piece mounting cavity 841 is subjected to secondary spraying after being subjected to silencing and noise reduction through staggered airflow channels formed by 3 layers of silencing piece assemblies and entering the outlet silencing piece mounting cavity 842.

S740), the gas after the secondary spraying is passed through the staggered airflow channels formed by 3 layers of silencing sheet assemblies to reduce noise and then is exhausted from the top of the outlet silencing sheet installation cavity 842 of the silencing tower 840.

S800), closing the spraying system

After the engine test is finished and the time reaches the preset time, preferably 2-4 hours, and more preferably 3 hours after the test is finished, the spray tower circulating pump 811 is closed, and the valve arranged at the alkaline circulating water delivery port for delivering alkaline circulating water below the alkaline circulating water level of the circulating water tank 830 is closed after the first spray system 806 and the spray tower second spray system 808 are closed.

After the engine test is finished and the time reaches the preset time, preferably 2-4 hours, and further preferably 3 hours after the test is finished, the spray tower circulating pump 811 is turned off to pump out the alkaline liquid in the alkaline liquid supply tank 830 and convey the alkaline liquid to the pumps of the lower layer spray system 845, the middle layer spray system 846, the upper layer spray system 847, the first spray system 806, the spray tower second spray system 808, the lower layer spray system 845, the middle layer spray system 846, and the upper layer spray system 847.

Preferably, after each engine test, tap water is injected through a water injection port provided in the alkaline liquid supply tank 830 and used for injecting municipal tap water, and alkaline materials are injected through a material injection port provided in the alkaline liquid supply tank 830 and used for injecting alkaline materials, so that the ph of the alkaline liquid in the alkaline liquid supply tank 830 reaches a predetermined value.

In the description herein, references to the description of the term "one embodiment," "some embodiments," "an illustrative embodiment," "an example," "a specific example," or "some examples" or the like mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

While embodiments of the present invention have been shown and described, it will be understood by those of ordinary skill in the art that: various changes, modifications, substitutions and alterations can be made to the embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the claims and their equivalents.

Claims (9)

1. A supersonic engine test bed thrust measurement exhaust device is characterized by comprising an engine thrust measurement rack, an exhaust system, a tail gas treatment system and a high-altitude simulation cabin; the high-altitude simulation cabin is of a sealed shell structure, the engine thrust measurement rack is fixedly arranged in the high-altitude simulation cabin, and the tested engine is arranged on the engine thrust measurement rack; one end of the exhaust system penetrates through the surface of the shell of the high-altitude simulation cabin and is fixedly installed in the high-altitude simulation cabin, and the other end of the exhaust system is fixedly communicated with the tail gas treatment system.

2. The supersonic engine test stand thrust measurement exhaust apparatus of claim 1, wherein: the engine thrust measuring rack comprises a fixed rack, a movable rack and a loading measuring device; the loading measuring device comprises a spring piece, a loading mechanism and a working force sensor; the movable frame is hung on the fixed frame through the spring piece, the loading mechanism is fixedly installed on the fixed frame, and two ends of the working force sensor are respectively connected with the fixed frame and the movable frame.

3. The supersonic engine test stand thrust measurement exhaust apparatus of claim 2, wherein: the movable frame comprises a movable frame body, a first movable frame spring piece mounting seat, a movable frame working force sensor mounting seat, a second movable frame spring piece mounting seat and a movable frame standard force sensor mounting seat; the movable frame standard force sensor mounting seat is fixedly mounted on the bottom surface of the front end of the movable frame body along the length direction of the movable frame body; the first movable frame spring piece mounting seat comprises 2 fixed mounting seats which are fixedly mounted on the bottom surface of the front end of the movable frame body and are respectively positioned on two sides of the movable frame standard force sensor mounting seat; the movable frame working force sensor mounting seat is fixedly mounted at the bottom of the movable frame body and is positioned on a central line along the length direction of the movable frame body; the second movable frame spring piece mounting seat comprises 2 spring pieces which are respectively fixedly mounted on the bottom surface of the rear end of the movable frame body.

4. The supersonic engine test stand thrust measurement exhaust apparatus of claim 3, wherein:

the fixed frame comprises a base, a front mounting seat, a loading mechanism mounting seat, a first fixed frame spring piece mounting seat, a fixed frame working force sensor mounting seat, a rear mounting seat and a second fixed frame spring piece mounting seat; the base is of a cuboid structure, the front mounting seat and the rear mounting seat are fixedly mounted at the front end and the rear end of the base respectively along the length direction of the base, the rear mounting seat comprises a transverse plate and a vertical plate, and the transverse plate and the vertical plate form an L shape; the loading mechanism mounting seats are fixedly mounted on the front mounting seat, the number of the first fixing frame spring piece mounting seats is 2, and the first fixing frame spring piece mounting seats are fixedly mounted at the front end of the base and are respectively positioned on two sides of the front mounting seat; the fixed frame working force sensor mounting seat is fixedly arranged on the base and is positioned on a central line along the length direction of the base; the second fixed frame spring piece mounting seat comprises 2 spring pieces which are fixedly mounted at the rear end of the base and are respectively positioned on two sides of the rear mounting seat.

5. The supersonic engine test stand thrust measurement exhaust apparatus of claim 4, wherein: the loading measuring device comprises a first spring piece, a second spring piece, a loading mechanism, a standard force sensor and a working force sensor; the number of the first spring pieces is 2, each first spring piece is fixedly connected with a first fixed frame spring piece mounting seat and a first movable frame spring piece mounting seat, the number of the second spring pieces is 2, and two ends of each second spring piece are fixedly connected with a second fixed frame spring piece mounting seat and a second movable frame spring piece mounting seat respectively; the loading mechanism is fixedly arranged on a transverse plate of the front mounting seat, the standard force sensor is fixedly arranged on a baffle plate at the front end of the movable frame body, and the loading mechanism and the standard force sensor are coaxially arranged and are parallel to the central line of the base along the length direction; the two ends of the working force sensor are respectively and fixedly connected with the fixed frame working force sensor mounting seat and the movable frame working force sensor mounting seat, and the working force sensor, the loading mechanism and the standard force sensor are coaxially arranged.

6. The supersonic engine test stand thrust measurement exhaust apparatus of claim 1, wherein the tail gas treatment system comprises a first lye spray tower, a second lye spray tower, a lye supply pool, a muffler tower and a tail gas treatment system input line; the gas inlets of the spray towers of the first alkali liquor spray tower and the second alkali liquor spray tower are communicated with an input pipeline of a tail gas treatment system, the gas outlets of the spray towers are communicated with a silencing tower through pipelines, one end of a conveying pipeline for conveying alkali liquor to the spray system is communicated with an alkali liquor supply pool, and the other end of the conveying pipeline penetrates through an alkali liquor input port of the spray tower and is respectively communicated with a first spray system of the spray tower and a second spray system of the spray tower; the lower layer spraying system, the middle layer spraying system and the upper layer spraying system are sequentially and fixedly arranged in the silencing tower from bottom to top, and the lower layer spraying system, the middle layer spraying system and the upper layer spraying system are communicated with an alkaline liquid supply tank through pipelines.

7. The thrust measurement exhaust device of a supersonic engine test stand according to claim 6, wherein the first alkali lye spray tower and the second alkali lye spray tower are identical in structure, the first alkali lye spray tower comprises a spray tower body, a spray tower air inlet, a spray tower air outlet, a spray tower alkali lye inlet, a spray tower first packing layer, a spray tower first spray system, a spray tower second packing layer, a spray tower second spray system, a spray tower level gauge, a spray tower circulating pump, a spray tower overflow port, a spray tower drain outlet and a spray tower maintenance port; the spray tower body is of a hollow cylindrical structure, a spray tower air inlet, a spray tower alkali liquor inlet, a spray tower overflow port, a spray tower drain outlet and a spray tower maintenance port are arranged on the side part of the spray tower body, and a spray tower air outlet is arranged on the top of the spray tower body; the spray tower circulating pump is arranged outside the spray tower body and used for pumping out the alkaline liquid in the alkaline liquid supply tank and conveying the alkaline liquid to the first spray system of the spray tower and the second spray system of the spray tower through a conveying pipeline for conveying the alkaline liquid to the spray system; the overflow port of the spray tower is arranged higher than the air inlet of the spray tower, the alkali liquor inlet of the spray tower and the sewage outlet of the spray tower are communicated with external wastewater treatment equipment through a pipeline; along the axis of the spray tower body, a first packing layer of the spray tower, a first spraying system of the spray tower, a second packing layer of the spray tower and a second spraying system of the spray tower are sequentially and fixedly installed inside the spray tower body from bottom to top, and a liquid level meter of the spray tower is arranged on the lower portion of the first packing layer of the spray tower on the side portion of the spray tower body and used for monitoring the water level of wastewater at the bottom of the spray tower body.

8. The thrust measurement exhaust device of the supersonic engine test stand according to claim 6, wherein the silencer tower comprises an inlet silencer mounting cavity and an outlet silencer mounting cavity, the bottoms of the inlet silencer mounting cavity and the outlet silencer mounting cavity are communicated, an inlet silencer assembly is fixedly mounted at the inlet silencer mounting cavity, an outlet silencer assembly is fixedly mounted at the outlet silencer mounting cavity, the air outlets of the spray towers of the first alkali liquor spray tower and the second alkali liquor spray tower are communicated with the inlet silencer mounting cavity of the silencer tower through pipelines, and the outlet of the outlet silencer mounting cavity is communicated with the atmosphere; in the outlet silencing piece installation cavity, a lower layer spraying system, a middle layer spraying system and an upper layer spraying system are fixedly installed below the outlet silencing piece assembly from bottom to top in sequence, the lower layer spraying system, the middle layer spraying system and the upper layer spraying system are communicated with an alkaline liquid supply pool through pipelines, and a pump for pumping and conveying alkaline liquid in the alkaline liquid supply pool to the lower layer spraying system, the middle layer spraying system and the upper layer spraying system is arranged outside the silencing tower.

9. The supersonic engine test bench thrust measuring exhaust apparatus of claim 6, wherein the inlet silencer assembly and the outlet silencer assembly are identical in structure, and the inlet silencer assembly comprises a lower silencer assembly, a middle silencer assembly and an upper silencer assembly which are sequentially arranged from bottom to top; each layer of silencing sheet component comprises semi-thin silencing sheets, semi-thick silencing sheets and thin and thick combined silencing sheets which are arranged at intervals, wherein in each layer of silencing sheet component, the semi-thin silencing sheets and the semi-thick silencing sheets are arranged at two ends and are fixedly connected with two end faces of an inlet silencing sheet mounting cavity of the silencing tower, a plurality of thin and thick combined silencing sheets are arranged at intervals between the semi-thin silencing sheets and the semi-thick silencing sheets, and the adjacent silencing sheets form an airflow channel.

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