Bird impact test launching device for a vertical rotor tester

Abstract

The application relates to a bird impact test launching device of a vertical rotor tester, which is arranged on the upper cover of the vertical rotor tester and comprises a control system, a launching device, a blocking mechanism and a barrel. The launching device comprises an actuating mechanism and a bird body positioning structure. The barrel is vertically arranged on one side of the upper cover of the vertical rotor tester and the axis of the barrel penetrates the rotor blade of the vertical rotor tester, the bird body positioning structure is fixedly connected to the upper side of the barrel, and the bird body positioning structure is internally provided with a bird body loading cabin coaxially arranged with the barrel. The bird body is arranged in the bird body loading cabin, and the actuating mechanism is arranged below the bird body positioning structure and connected with the barrel. A bird body launching structure in a vertical state is formed, after the actuating mechanism is controlled to move out from the lower side of the bird body loading cabin, the bird body freely falls under the action of gravity and penetrates the through hole to fall on the rotating blade, so that the bird impact test under the single or multiple blade rotating state is completed.

Description

TECHNICAL FIELD

[0001] The application belongs to the field of bird impact test design, and particularly relates to a vertical rotor tester bird impact test launching device. BACKGROUND

[0002] To solve the problems of insufficient bird body constitutive model precision and incomplete working condition representation in the process of engine bird impact mechanism research, high-precision multidisciplinary simulation research and full-process multi-level bird impact resistance virtual verification platform establishment, the bird impact test technology system is improved from the part level to the component level and then to the whole machine level, the single blade or multiple blade segment rotating state bird impact test technology blank in the domestic test capability system is filled, and the vertical rotor tester bird impact test launching device is developed. SUMMARY

[0003] The application aims to provide a vertical rotor tester bird impact test launching device to solve the problem of lacking bird impact test in the single or multiple blade rotating state in the prior art.

[0004] The technical scheme of the application is as follows: a vertical rotor tester bird impact test launching device, comprising a control system, a launching device, an arresting mechanism and a barrel; the launching device comprises an actuating mechanism and a bird positioning structure;

[0005] The barrel is vertically arranged on one side of the upper part of the upper cover of the vertical rotor tester, and the axis of the barrel passes through the rotor blade of the vertical rotor tester; the bird positioning structure is fixedly connected to the upper side of the barrel; the bird positioning structure is internally provided with a bird loading cabin coaxially arranged with the barrel; the bird is arranged in the bird loading cabin; the actuating mechanism is arranged below the bird positioning structure and connected with the barrel; the actuating mechanism is provided with a supporting plate corresponding to the position below the bird loading cabin; the actuating mechanism can drive the supporting plate to move to the lower side of the bird loading cabin to support the bird before the bird is launched; the control system is electrically connected with the actuating mechanism;

[0006] The control system is electrically connected with the actuating mechanism, and the control system can control the actuating mechanism to drive the supporting plate to move; the arresting mechanism is arranged on the barrel, and the arresting mechanism can arrest the bird entering the barrel; the lower end of the barrel is sealingly connected with the upper cover of the vertical rotor tester; the upper cover of the vertical rotor tester is provided with a through hole corresponding to the position of the barrel, so that the bird can continue to fall.

[0007] Preferably, the bird positioning mechanism comprises an upper shell, an outer shell, a middle shell and an inner shell; the upper shell and the inner shell are arranged in correspondence with each other in the up-down direction, and the outer shell, the middle shell and the inner shell are coaxially arranged in the inside-outside direction; the upper shell is a hollow cylindrical structure, and the bird loading cabin is located in the upper shell; the outer shell, the middle shell and the inner shell are all hollow cylindrical structures, and the bottom of the upper shell is provided with a partition plate fixedly connected with the top of the outer shell and the middle shell; the inner shell is provided with a central cavity in communication with the bird loading cabin, the space between the inner shell and the middle shell is a receiving cavity, the space between the middle shell and the outer shell is an outer cavity, and the actuating mechanism is in communication with the receiving cavity.

[0008] Preferably, a connecting rod mechanism capable of supporting the bird is arranged between the central cavity and the bird loading cabin, the supporting plate is connected with the end of the connecting rod mechanism, and the connecting rod mechanism is controlled by the actuating mechanism; the connecting rod mechanism comprises a telescopic rod, a hinged seat and a swing plate; the lower end of the telescopic rod is connected with the output end of the actuating system, the hinged seat is arranged on the inner wall of the middle shell, the swing plate is arranged horizontally when the bird is not launched, one end of the swing plate is hinged with the hinged seat, the other end of the swing plate is connected with the supporting plate, a swing groove is arranged in the swing plate along the length direction of the swing plate, the upper end of the telescopic rod is provided with a connecting column, and the connecting column is slidingly connected in the swing groove and can rotate in the swing groove.

[0009] Preferably, the actuating mechanism comprises a vacuum air release cavity, a driving air pressure cavity, a piston pressure cavity and a piston; the driving pressure cavity is in communication with the outer cavity of the bird positioning mechanism, the piston pressure cavity is correspondingly arranged on the inner side of the driving pressure cavity, the driving pressure cavity and the piston pressure cavity are both connected with a gas source, the upper end of the piston pressure cavity is in communication with the driving pressure cavity, the lower end of the piston pressure cavity is in communication with the vacuum pressure cavity, and the piston is arranged in the piston pressure cavity and the upper end of the piston is connected with the connecting rod mechanism.

[0010] Preferably, the barrel is divided into an upper barrel and a lower barrel, the arresting mechanism is arranged between the upper barrel and the lower barrel, and the arresting mechanism comprises an arresting box, a slide, a plug plate, a push-pull rod and an electric push rod; the arresting box is horizontally connected between the upper barrel and the lower barrel, the slide is horizontally arranged in the arresting box, and the push-pull rod is horizontally slidingly matched in the slide; one side of the plug plate is fixedly connected with the push-pull rod, and the other side of the plug plate is horizontally inserted into the gap between the upper barrel and the lower barrel; the electric push rod is arranged outside the arresting box and connected with the push-pull rod; when the electric push rod is retracted, the plug plate can be pulled out of the upper barrel and the lower barrel through the push-pull rod, and when the electric push rod is extended, the plug plate can be pushed into the upper barrel and the lower barrel through the push-pull rod, so as to realize the closing function.

[0011] Preferably, the control system comprises a local control cabinet and a remote control computer; the remote control computer is used to issue control instructions to the local control cabinet, and the local control cabinet controls the specific action of the actuating mechanism according to the control instructions; the actuating system is provided with a sensor connected to the local control cabinet; and the local control cabinet can transmit the signals collected by the sensor to the remote control computer.

[0012] The bird impact test launching device of the vertical rotor tester of the application forms a bird body launching structure in a vertical state. After the control actuating mechanism is moved out from below the bird body loading cabin, the bird body freely falls under the action of gravity and falls through the through hole to the rotating blade to complete the bird impact test in the single or multiple blade rotating state. The blocking mechanism can effectively prevent the test cost caused by the accidental falling of the bird body before the release instruction is issued, and solves the problem of blocking the accidental falling of the bird body. Since the bird body is in a free and relaxed state before release, there is no extra object participating in the impact with the bird body, and the problem of bird body residence before vertical release is solved. Since the bird body is in a free falling state for bird impact test, the speed of the bird body can be calculated very accurately, and the problem of the influence of the rapid movement of the release mechanism on the speed of the bird body is solved. BRIEF DESCRIPTION OF DRAWINGS

[0013] In order to more clearly illustrate the technical solutions provided by the application, the following will briefly introduce the drawings. Obviously, the drawings described below are only some embodiments of the application.

[0014] Figure 1 It is a schematic diagram of the overall structure of the application;

[0015] Figure 2 It is a schematic diagram of the overall process of the application;

[0016] Figure 3 It is a schematic diagram of the bird body positioning structure of the application;

[0017] Figure 4 It is a schematic diagram of the actuating mechanism structure of the application;

[0018] Figure 5 It is a schematic diagram of the blocking mechanism structure of the application;

[0019] Figure 6 It is a schematic diagram of the sealing adapter structure of the application.

[0020] 1, control system; 2, projection device; 3, blocking mechanism; 4, barrel; 5, supporting plate; 6, upper shell; 7, outer shell; 8, middle shell; 9, inner shell; 10, telescopic rod; 11, hinged seat; 12, swing plate; 13, connecting column; 14, vacuum air release cavity; 15, driving air cavity; 16, piston pressure cavity; 17, piston; 18, blocking box; 19, slide; 20, insertion plate; 21, push-pull rod; 22, local control cabinet; 23, remote control computer; 24, bird body; 25, upper cover; 26, sealing switching structure. DETAILED DESCRIPTION

[0021] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the present application.

[0022] A vertical rotor tester bird impact test launching device is arranged on an upper cover 25 of a vertical rotor tester, and includes a control system 1, a projection device 2, a blocking mechanism 3 and a barrel 4. The projection device 2 includes an actuating mechanism and a bird body positioning structure.

[0023] The barrel 4 is vertically arranged on one side of the upper portion of the upper cover 25 of the vertical rotor tester, and the axis of the barrel 4 passes through the rotor blade of the vertical rotor tester. The bird body positioning structure is fixedly connected to the upper portion of the barrel 4, and the bird body positioning structure is internally provided with a bird body 24 loading cabin coaxially arranged with the barrel 4. The bird body 24 is arranged in the bird body 24 loading cabin. The actuating mechanism is arranged below the bird body positioning structure and connected to the barrel 4. The actuating mechanism is provided with a supporting plate 5 corresponding to the position below the bird body 24 loading cabin. Before the bird body 24 is launched, the actuating mechanism can drive the supporting plate 5 to move to the position below the bird body 24 loading cabin to support the bird body 24. When the bird body 24 is launched, the actuating mechanism can drive the supporting plate 5 to move out from the position below the bird body 24 loading cabin. The control system 1 is electrically connected to the actuating mechanism.

[0024] The control system 1 is electrically connected to the actuating mechanism and can control the actuating mechanism to drive the supporting plate 5 to move. The blocking mechanism 3 is arranged on the barrel 4 and can block the bird body 24 entering the barrel 4. The lower end of the barrel 4 is sealingly connected to the upper cover 25 of the vertical rotor tester. The upper cover 25 of the vertical rotor tester is provided with a through hole corresponding to the position of the barrel 4, so that the bird body 24 can continue to fall.

[0025] Through the above design, a vertical bird body 24 launching structure is formed. After the control actuating mechanism is moved out from below the bird body 24 loading cabin, the bird body 24 freely falls under gravity and falls through the through hole to the rotating blade to complete the bird impact test in the single or multiple blade rotating state. The blocking mechanism 3 can effectively prevent the test cost caused by accidental falling of the bird body 24 before the release instruction is issued, and solves the problem of blocking the bird body 24 from accidentally falling.

[0026] Since the bird body 24 is in a free and relaxed state before release, there is no extra object participating in the impact with the bird body 24, and the problem of bird body 24 staying before vertical release of the bird body 24 is solved. Since the bird body 24 is in a free fall state for bird impact test, the speed of the bird body 24 can be calculated very accurately, and the problem of the release mechanism moving quickly and affecting the speed of the bird body 24 is solved.

[0027] And the different positions of the barrel 4 and the vertical rotor tester upper cover 25 can be connected to realize different impact point test capability.

[0028] The functions and effects of each part are described as follows:

[0029] I. Control system design

[0030] The control system 1 is an electric control system for issuing control instructions to the actuating mechanism, including a local control cabinet 22 and a remote control computer 23. The remote control computer 23 is used to issue control instructions to the local control cabinet 22, and the local control cabinet 22 controls the specific actions of the actuating mechanism according to the control instructions.

[0031] The actuating mechanism is provided with pressure, position and other sensors. The signals collected are transmitted to the remote control computer 23 through the local control cabinet 22. The remote control computer 23 is provided with control software. The signals collected by the sensors are converted into data and displayed in the control software, which is used to judge whether the blocking mechanism 3 is in place, whether the bird body 24 is in place, whether the loading mechanism rear cover is installed in place, etc. Other conditions that cannot be directly judged in the control system 1 and need to be confirmed before launching can be added to the judgment combination of the preset conditions by the operator.

[0032] The operation interface is displayed in a graphical interface, and various condition judgments and button states are distinguished by obvious colors.

[0033] To ensure operation safety, a manual air release valve and an emergency stop button connected to the actuating system are provided on site. The control system 1 can realize local / remote control switching, and the overall process is as follows: Figure 2As shown, after the actuation mechanism is ready, the bird body 24 is loaded, and the high-speed camera is prepared. Then the tester is started, the control system 1 controls the bird body 24 to launch, and at the same time controls the high-speed camera to trigger and record the launch of the bird body 24 until the bird body 24 hits the rotating blade and stops.

[0034] II. Bird Body Positioning Structure

[0035] like Figure 3 As shown, the bird body 24 positioning mechanism includes an upper shell 6, an outer shell 7, a middle shell 8, and an inner shell 9. The upper shell 6 and the inner shell 9 are arranged vertically correspondingly, and the outer shell 7, the middle shell 8, and the inner shell 9 are coaxially arranged internally and externally. The upper shell 6 is a hollow cylindrical structure, and the loading compartment of the bird body 24 is located inside the upper shell 6. The outer shell 7, the middle shell 8, and the inner shell 9 are all hollow cylindrical structures. The bottom of the upper shell 6 is provided with a partition that is fixedly connected to the top of the outer shell 7 and the middle shell 8. The inner shell 9 has a central cavity that communicates with the loading compartment of the bird body 24. The space between the inner shell 9 and the middle shell 8 is a receiving cavity, and the space between the middle shell 8 and the outer shell 7 is an outer cavity. The actuating mechanism communicates with the receiving cavity to expand the volume of the pressure chamber outside the actuating mechanism, reduce the pressure drop in the cavity when the piston 17 moves, and maximize the movement speed of the piston 17.

[0036] A linkage mechanism supporting the bird 24 is provided between the central cavity and the loading compartment of the bird 24. The support plate 5 is connected to the end of the linkage mechanism, which is controlled by an actuation mechanism. The linkage mechanism includes a telescopic rod 10, a hinge seat 11, and a swing plate 12. The lower end of the telescopic rod 10 is connected to the output end of the actuation system. The hinge seat 11 is located on the inner wall of the middle shell 8. The swing plate 12 is horizontally positioned when the bird 24 is not launched. One end of the swing plate 12 is hinged to the hinge seat 11, and the other end is connected to the support plate 5. A swing groove is formed inside the swing plate 12 along its length. A connecting post 13 is provided at the upper end of the telescopic rod 10. The connecting post 13 is slidably connected in the swing groove and can rotate within the swing groove.

[0037] The actuation mechanism drives piston 17 and piston rod 17 to move tray 5 between the central cavity and the receiving cavity. When tray 5 is in a horizontal position, the bird body 24 is located in the bird body 24 loading compartment above tray 5. During "launch", tray 5 is rapidly retracted and enters the receiving compartment under the action of the actuation mechanism, and the bird body 24 falls freely. The upper part of the bird body 24 loading compartment is designed with a sealed door that is easy to open and close for loading the bird body 24 before launch.

[0038] III. Actuating Mechanism

[0039] like Figure 4As shown, the actuating mechanism includes a vacuum venting cavity 14, a driving pressure cavity 15, a piston pressure cavity 16 and a piston 17. The bird 24 can pass through the barrel 4 and the central cavity. The piston pressure cavity 16 is inflated to push the piston 17 to move upward, push the swing plate 12 upward, keep the support plate 5 horizontal and enable the support plate 5 to support the bird 24. When the bird 24 is released, the gas in the piston pressure cavity 16 is discharged into the vacuum venting cavity 14, the piston 17 moves downward under the driving of the gas in the driving pressure cavity and moves the support plate 5 into the storage cavity, and the bird 24 falls freely.

[0040] The driving pressure cavity is in communication with the cavity outside the bird 24 positioning mechanism, which is used to expand the cavity volume, reduce the pressure drop in the cavity when the piston 17 moves, and maximize the speed of the piston 17. The piston pressure cavity 16 is correspondingly arranged inside the driving pressure cavity. The driving pressure cavity and the piston pressure cavity 16 are connected to the gas source. The upper end of the piston pressure cavity 16 is in communication with the driving pressure cavity, the lower end of the piston pressure cavity 16 is in communication with the vacuum pressure cavity, the piston 17 is arranged in the piston pressure cavity 16, and the upper end of the piston 17 is connected to the telescopic rod 10. The lower vacuum venting cavity 14 is used to receive the compressed air discharged from the piston pressure cavity 16, so as to reduce the pressure in the piston pressure cavity 16 to the lowest and improve the moving speed of the piston 17. If necessary, the lower vacuum venting cavity 14 can be in communication with the vacuum chamber of the vertical rotor tester.

[0041] Four, barrel

[0042] The barrel 4 is divided into an upper barrel and a lower barrel. The effective barrel 4 length can be changed in size according to actual needs, and the caliber of the barrel 4 can be adjusted. A connecting body is specially designed at the connection between the barrel mouth and the original opening of the vertical rotor test system upper cover 25, which is used for docking conversion and sealing between different interface sizes. Sensor mounting holes are designed on the connecting body, which are used to measure the speed of the bird 24 when passing through and detect whether the bird 24 passes through. The barrel 4 structure is as shown in Figure 5 A sealing adapter structure 26 is arranged between the barrel 4 and the upper cover 25, as shown in Figure 6 The middle part of the sealing adapter structure 26 is in communication with the barrel 4 for the bird 24 to pass through, and the two sides of the sealing adapter structure 26 extend out to be sealingly connected with the upper cover 25.

[0043] Five, blocking mechanism

[0044] In order to prevent the projectile from entering the vacuum chamber before the target moment, a blocking mechanism 3 is designed at the barrel mouth. The structure is as shown in Figure 5 The blocking plug-in plate 20 is inserted into the barrel 4 to prevent the projectile from falling into the vacuum chamber due to accidental circumstances. Before the bird 24 is released, the blocking plug-in plate 20 is withdrawn from the barrel 4 under the driving of the external electric push rod and the push-pull rod 21. The bird loading chamber is provided with a position sensor for identifying whether the bird 24 is in the position to be launched. There is a gap between the upper barrel and the lower barrel, and the blocking mechanism 3 is arranged at the joint of the upper barrel and the lower barrel.

[0045] The blocking mechanism 3 comprises a blocking box 18, a slide 19, an insertion plate 20, a push-pull rod 21 and an electric push rod.

[0046] The blocking box 18 is horizontally connected between the upper barrel and the lower barrel, the slide 19 is horizontally arranged in the blocking box 18, and the push-pull rod 21 is horizontally slidably arranged in the slide 19; one side of the insertion plate 20 is fixedly connected with the push-pull rod 21, and the other side is horizontally inserted into the gap between the upper barrel and the lower barrel; the electric push rod is arranged outside the blocking box 18 and connected with the push-pull rod 21. When the electric push rod is retracted, the insertion plate 20 can be pulled out of the upper barrel and the lower barrel through the push-pull rod 21, and when the electric push rod is extended, the insertion plate 20 can be pushed into the upper barrel and the lower barrel through the push-pull rod 21, so as to realize the closing function.

[0047] The overall principle is shown in Figure 1 Before launching, compressed air is filled in the actuator, the actuator piston 17 reaches the designated position, and the detachable support plate 5 of the bird body 24 positioning mechanism is driven by the rod of the actuator piston 17 to reach the working position. After the bird body 24 is loaded, the launching is prepared. When the vacuum chamber of the vertical rotor tester is vacuumized, the barrel 4 and the inside of the bird body 24 positioning mechanism are also vacuumized. When the rotor reaches the predetermined rotating speed, the control system 1 sends a launching instruction, the actuator piston pressure cavity 16 discharges compressed air, the piston 17 moves quickly under the action of the compressed air in the driving pressure cavity 15 and drives the bird body 24 support plate 5 to move, the bird body 24 accelerates under the action of gravity and collides with the rotating blades. In an emergency, the emergency stop button is pressed, the blocking mechanism is closed, and the control software enters the emergency program.

[0048] Finally, it should be noted that: the drawings of the disclosed embodiments only involve the structures involved in the disclosed embodiments, other structures can refer to the general design, and in the case of no conflict, the same embodiments and different embodiments of the present application can be combined with each other;

[0049] Finally, the above only describes the preferred embodiments of the present application and is not used to limit the present application, and any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the present application shall be included in the protection scope of the present application.

Claims

1. A bird impact test launch device for a vertical rotor tester bird impact test, characterized by: Including control system (1), projection device (2), blocking mechanism (3) and cannon barrel (4), the projection device (2) includes actuating mechanism and bird positioning structure; The cannon barrel (4) is vertically arranged on one side of the upper part of the cover (25) of the vertical rotor tester, and the axis of the cannon barrel (4) passes through the rotor blade of the vertical rotor tester, the bird positioning structure is fixedly connected above the cannon barrel (4), a bird (24) loading cabin coaxial with the cannon barrel (4) is arranged in the bird positioning structure, the bird (24) is arranged in the bird (24) loading cabin, and the actuating mechanism is arranged below the bird positioning structure and connected with the cannon barrel (4); the actuating mechanism is provided with a supporting plate (5) corresponding to the position below the bird (24) loading cabin, the actuating mechanism can drive the supporting plate (5) to move below the bird (24) loading cabin to support the bird (24) before the bird (24) is launched, and the actuating mechanism can drive the supporting plate (5) to move out from below the bird (24) loading cabin when the bird (24) is launched; the control system (1) is electrically connected with the actuating mechanism, and the control system (1) can control the actuating mechanism to drive the supporting plate (5) to move, the blocking mechanism (3) is arranged on the cannon barrel (4), and the blocking mechanism (3) can block the bird (24) entering the cannon barrel (4), the lower end of the cannon barrel (4) is sealingly connected with the upper cover (25) of the vertical rotor tester, and the upper cover (25) of the vertical rotor tester is provided with a through hole corresponding to the position of the cannon barrel (4), so that the bird (24) can continue to fall; The cannon barrel (4) is divided into an upper cannon barrel and a lower cannon barrel, the blocking mechanism (3) is arranged between the upper cannon barrel and the lower cannon barrel, and the blocking mechanism (3) includes a blocking box (18), a slide (19), a plug plate (20), a push-pull rod (21) and an electric push rod; the blocking box (18) is horizontally connected between the upper cannon barrel and the lower cannon barrel, the slide (19) is horizontally arranged in the blocking box (18), and the push-pull rod (21) is horizontally slidably fitted in the slide (19); one side of the plug plate (20) is fixedly connected with the push-pull rod (21), and the other side is horizontally inserted into the gap between the upper cannon barrel and the lower cannon barrel; the electric push rod is arranged outside the blocking box (18) and connected with the push-pull rod (21); when the electric push rod is retracted, the plug plate (20) can be pulled out of the upper cannon barrel and the lower cannon barrel through the push-pull rod (21), and when the electric push rod is extended, the plug plate (20) can be inserted between the upper cannon barrel and the lower cannon barrel through the push-pull rod (21), so that the closing function is realized. ​ 2. The vertical rotor tester bird impact test launch device of claim 1, wherein: The bird positioning structure comprises an upper shell (6), an outer shell (7), a middle shell (8) and an inner shell (9); the upper shell (6) is arranged in correspondence with the inner shell (9) in an up-down direction, and the outer shell (7), the middle shell (8) and the inner shell (9) are coaxially arranged in an inside-outside direction; the upper shell (6) is a hollow cylindrical structure, and a bird loading cabin (24) is arranged in the upper shell (6); the outer shell (7), the middle shell (8) and the inner shell (9) are all hollow cylindrical structures, and the bottom of the upper shell (6) is fixedly connected to the top of the outer shell (7) and the middle shell (8) through a partition plate; a central cavity in communication with the bird loading cabin (24) is arranged in the inner shell (9), a receiving cavity is arranged between the inner shell (9) and the middle shell (8), an outer cavity is arranged between the middle shell (8) and the outer shell (7), and the actuating mechanism is in communication with the receiving cavity.

3. The bird impact test launch device for a vertical axis rotor tester bird impact test apparatus of claim 2, wherein: A connecting rod mechanism capable of supporting the bird (24) is arranged between the central cavity and the bird loading cabin (24), the supporting plate (5) is connected to the end of the connecting rod mechanism, and the connecting rod mechanism is controlled by the actuating mechanism; the connecting rod mechanism comprises a telescopic rod (10), a hinged seat (11) and a swing plate (12); the lower end of the telescopic rod (10) is connected to the output end of the actuating system, the hinged seat (11) is arranged on the inner wall of the middle shell (8), the swing plate (12) is arranged horizontally when the bird (24) is not launched, one end of the swing plate (12) is hinged to the hinged seat (11), the other end of the swing plate (12) is connected to the supporting plate (5), a swing groove is arranged in the swing plate (12) along the length direction of the swing plate (12), the upper end of the telescopic rod (10) is provided with a connecting column (13), and the connecting column (13) is slidably connected in the swing groove and can rotate in the swing groove.

4. The bird impact test launch device for a vertical axis rotor tester bird impact test of claim 3, wherein: The actuating mechanism comprises a vacuum air release cavity (14), a driving air compression cavity (15), a piston pressure cavity (16) and a piston (17); the driving air compression cavity (15) is in communication with the outer cavity of the bird positioning structure, the piston pressure cavity (16) is arranged on the inner side of the driving air compression cavity (15) in correspondence, the driving air compression cavity (15) and the piston pressure cavity (16) are both connected to a gas source, the upper end of the piston pressure cavity (16) is in communication with the driving air compression cavity (15), the lower end of the piston pressure cavity (16) is in communication with the vacuum air release cavity (14), and the piston (17) is arranged in the piston pressure cavity (16) and the upper end of the piston (17) is connected to the connecting rod mechanism.

5. The vertical rotor tester bird impact test launch device of claim 1, wherein: The control system (1) comprises a local control cabinet (22) and a remote control computer (23); the remote control computer (23) is used for issuing a control instruction to the local control cabinet (22), the local control cabinet (22) controls the specific action of the actuating mechanism according to the control instruction, a sensor connected to the local control cabinet (22) is arranged in the actuating mechanism, and the local control cabinet (22) can transmit the signal collected by the sensor to the remote control computer (23).

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