A comprehensive training equipment for aircraft mechanics

Abstract

The present invention discloses an aircraft mechanics comprehensive training device, which relates to the field of flight training, and comprises a base and an aileron rotatably arranged on the base, and a seat is rotatably arranged on the base; and further comprises a power mechanism, which drives the aileron to adaptively swing while the seat is tilted. The aircraft mechanics comprehensive training device provided by the present invention can drive the aileron to adaptively swing while the seat is tilted by the power mechanism, by adding a seat and a power mechanism on the base, so that the aileron can be driven to adaptively swing while the seat is driven to swing by the power mechanism, so that the oblique flying feeling caused by the tilt of the seat can be intuitively felt while the swing of the aileron is visually observed, and has a better simulation training effect.

Description

Technical Field

[0001] The invention relates to the field of flight training, and in particular to aircraft mechanical comprehensive training equipment. Background Art

[0002] As is known to all, flight training usually refers to professional training that pilots undergo in order to obtain a pilot's license or improve their flying skills. This includes two aspects: theoretical study and practical training. The practical aspect includes simulated flight training, which involves the turning of the aircraft. The turning process of the aircraft is achieved by the swing of the aircraft's ailerons.

[0003] For example, the Chinese patent document with the authorization announcement number CN213211401U, the announcement date 2021-05-14, and the name "A Simulation Training Platform for Aircraft Transmission System" comprises a platform frame, the lower part of the outer part of the platform frame is respectively connected to the left aileron and the right aileron through the aileron support frame, pulleys are arranged on both side walls inside the platform frame, a steering wheel drum is arranged on the upper part, and a tension compensator is arranged on the lower part, the tension compensator comprises a mounting seat, a bracket is fixedly connected to the mounting seat, the roller is fixedly connected to the bracket through a fastener, springs are arranged on both sides of the bracket, and an indicator pin is also arranged on the bracket, the pulley, the steering wheel drum, the fan-shaped disc and the tension compensator are connected by a steel cable; the device has a high degree of simulation, complete practice items, and has all the basic components of the aircraft transmission system. Training items such as steel cable adjustment, push-pull rod adjustment, tension screw sleeve insurance, and aircraft transmission system calibration can be completed on the platform. The experience during the practice is similar to the experience in a real aircraft, and it is highly practical.

[0004] The disadvantages of the above-mentioned prior art are that it can only control the up and down swing of the aileron, and then observe the swing of the aileron by eyes, but cannot feel the tilt of the fuselage caused by the swing of the aileron, which makes the simulation training experience poor. Summary of the invention

[0005] The purpose of the present invention is to provide an aircraft mechanics comprehensive training device to solve the above-mentioned deficiencies in the prior art.

[0006] In order to achieve the above object, the present invention provides the following technical solutions:

[0007] An aircraft mechanics comprehensive training device comprises a base and an aileron rotatably arranged on the base, and a seat is rotatably arranged on the base;

[0008] It also includes a power mechanism, which drives the seat to tilt and drives the aileron to swing adaptively at the same time.

[0009] In the above-mentioned aircraft mechanics comprehensive training equipment, a mounting plate is slidably arranged on the base, a rotating shaft is arranged on the aileron, and the rotating shaft is rotatably connected to the mounting plate.

[0010] In the above-mentioned aircraft mechanics comprehensive training equipment, a fixed shaft is fixedly connected to the base, a rotating cylinder is provided on the seat, and the rotating cylinder is rotatably connected to the fixed shaft.

[0011] The above-mentioned aircraft mechanics comprehensive training equipment, the power mechanism includes a drive motor and a gear connected to the output end of the drive motor, a connecting part is provided on the rotating cylinder, the connecting part is slidably connected to the base, the drive motor is fixed to the connecting part, a tooth plate is provided on the base, and the gear is meshed with the tooth plate.

[0012] In the above-mentioned aircraft mechanics comprehensive training equipment, a limiting structure is provided between the connecting portion and the rotating cylinder for preventing the connecting portion and the rotating cylinder from being separated from each other.

[0013] In the above-mentioned aircraft mechanics comprehensive training equipment, a guide rail, a first branch rail, a second branch rail and a third branch rail are provided on the fixed shaft, a sliding part is provided on the rotating cylinder, the sliding part is slidably connected with the guide rail, and one of the first branch rail, the second branch rail and the third branch rail is located on the movement range of the sliding part.

[0014] In the above-mentioned aircraft mechanics comprehensive training equipment, a first baffle is rotatably provided inside the second branch rail, and a second baffle is rotatably provided on the third branch rail;

[0015] It also includes a driving assembly for driving the first baffle plate and the second baffle plate to rotate.

[0016] In the above-mentioned aircraft mechanics comprehensive training equipment, the driving assembly includes a push rod, a first rotating rod is arranged on the first baffle plate, a second rotating rod is arranged on the second baffle plate, and one of the first rotating rod and the second rotating rod is located on the movement range of the push rod.

[0017] In the above-mentioned aircraft mechanics comprehensive training equipment, a connecting rod is fixedly connected to the rotating cylinder, a transmission rod is slidably arranged on the mounting plate, a cross bar is slidably arranged on the transmission rod, a connecting shaft is arranged on the cross bar, and the connecting rod is rotatably connected to the connecting shaft;

[0018] It also includes a transmission assembly for converting the linear motion of the transmission rod into the swing of the aileron.

[0019] In the above-mentioned aircraft mechanics comprehensive training equipment, the transmission assembly includes an arc-shaped groove opened inside the transmission rod, a sliding rod is fixedly connected to the rotating shaft, and the sliding rod is slidably connected to the arc-shaped groove.

[0020] In the above technical scheme, the present invention provides an aircraft mechanics comprehensive training equipment, which adds a seat and a power mechanism on the base. While the power mechanism drives the seat to swing, it can also drive the aileron to swing adaptively, so that while visually observing the aileron swing, the oblique flight feeling caused by the tilt of the seat can be intuitively felt, thereby having a better simulation training effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in the present invention. For ordinary technicians in this field, other drawings can also be obtained based on these drawings.

[0022] Figure 1 A schematic diagram of the overall structure provided by an embodiment of the present invention;

[0023] Figure 2 A schematic diagram of the overall structure from another perspective provided by an embodiment of the present invention;

[0024] Figure 3 A partial development diagram of the outer circumference of a fixed shaft provided in an embodiment of the present invention;

[0025] Figure 4 A schematic diagram of a second branch rail opening process provided by an embodiment of the present invention;

[0026] Figure 5 A schematic diagram of a cross-sectional structure of an aileron provided in an embodiment of the present invention;

[0027] Figure 6 A schematic diagram of the abutment structure between the abutment portion and the first rotating rod provided in an embodiment of the present invention;

[0028] Figure 7 An explosion diagram provided for an embodiment of the present invention;

[0029] Figure 8 A partial expanded view provided for another embodiment of the present invention;

[0030] Fig. 9 for Figure 2 A schematic diagram of the enlarged local structure in the middle.

[0031] Description of reference numerals:

[0032] 1. Base; 2. Aileron; 3. Seat; 4. Mounting plate; 5. Rotating shaft; 6. First slideway; 7. Fixed shaft; 8. Rotating cylinder; 9. Driving motor; 10. Gear; 11. Connecting part; 12. Tooth plate; 13. Second slideway; 14. Guide rail; 15. First branch rail; 16. Second branch rail; 17. Third branch rail; 18. Sliding part; 19. First baffle; 20. Second baffle; 21. Push rod; 22. First Rotating rod; 23, second rotating rod; 24, abutment portion; 25, first section; 26, second section; 27, overlapping section; 28, overlapping rail; 29, protrusion; 30, connecting rod; 31, transmission rod; 32, cross bar; 33, connecting shaft; 34, arc groove; 35, sliding rod; 36, rectangular hole; 37, first horizontal edge; 38, second horizontal edge; 39, vertical edge; 40, through hole; 41, vertical groove; 42, limit portion. DETAILED DESCRIPTION

[0033] In order to enable those skilled in the art to better understand the technical solution of the present invention, the present invention will be further described in detail below with reference to the accompanying drawings.

[0034] In the description of the present invention, it is necessary to understand that Figure 5 The middle slide bar 35 is located at the top relative to the rotation shaft 5, and vice versa. Figure 3-Figure 4 The first baffle 19 rotates in the clockwise direction, and the reverse direction is counterclockwise. The terms "center", "length", "width", "degree", "up", "down", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", "circumferential" and the like indicate directions or positional relationships based on the directions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific direction, be constructed and operated in a specific direction, and therefore should not be understood as limiting the present invention.

[0035] Reference Figure 1-9 An embodiment of the present invention provides an aircraft mechanics comprehensive training device, comprising a base 1 and an aileron 2 rotatably arranged on the base 1, wherein a seat 3 is rotatably arranged on the base 1; and further comprising a power mechanism, wherein the power mechanism drives the seat 3 to tilt and drives the aileron 2 to swing adaptively.

[0036] Specifically, there are many ways of aircraft training, including aileron 2 swing training. When performing aileron 2 swing simulation training, in order to intuitively see the swing of aileron 2, by rotating the drum and driving the steel cable to move, a series of transmission parts drive the left aileron 2 and the right aileron 2 to swing simultaneously and oppositely. The trainer performs simulation training by observing the swing of the aileron 2. This is a prior art and will not be described in detail (see the patent document with authorization announcement number CN213211401U for details). One of the core innovations of the embodiment of the present invention is that a base 1 is provided, the base 1 is concave, and the aileron 2 and the seat 3 are rotatably arranged on the base 1. The aileron 2 is a rectangular plate structure, and there are two ailerons 2, and the two ailerons The seats 3 are arranged symmetrically, the ailerons 2 and the seats 3 can both rotate in the vertical direction, but the rotation direction of the ailerons 2 is perpendicular to the rotation direction of the seats 3, that is, the ailerons 2 rotate in the length direction of the base 1, and the seats 3 rotate in the width direction of the base 1, and the seats 3 can be provided with protective mechanisms such as seat belts, and the power mechanism can be two motors, one of which is used to drive the ailerons 2 to swing, and the other is used to drive the seats 3 to swing. The effect of such a setting is that while the power mechanism drives the seats 3 to swing, the ailerons 2 can also be driven to swing adaptively, so that while visually observing the swing of the ailerons 2, the oblique flying feeling caused by the tilt of the seats 3 can be intuitively felt, which has a better simulation training effect.

[0037] Preferably, a mounting plate 4 is slidably provided on the base 1, a rotating shaft 5 is provided on the aileron 2, and the rotating shaft 5 is rotatably connected to the mounting plate 4. Specifically, a first sliding groove 6 is provided on the inner bottom wall of the base 1, the mounting plate 4 is slidably connected to the first sliding groove 6, a rotating hole is provided on the mounting plate 4, and the aileron 2 is rotatably connected to the rotating hole through the rotating shaft 5, so that the aileron 2 can be driven to rotate in the vertical direction.

[0038] Preferably, a fixed shaft 7 is fixedly connected to the base 1, and a rotating cylinder 8 is provided on the seat 3, and the rotating cylinder 8 is rotatably connected to the fixed shaft 7. The fixed shaft 7 is a cylindrical structure, which is arranged along the length direction of the base 1, and its two ends are respectively fixedly connected to the inner walls of the two sides of the base 1, and the rotating cylinder 8 is fixedly connected to the lower surface of the seat 3. The rotating cylinder 8 rotates around the fixed shaft 7, thereby driving the seat 3 to rotate synchronously, so that the seat 3 can be changed from a vertical state to an inclined state.

[0039] Preferably, the power mechanism includes a driving motor 9 and a gear 10 connected to the output end of the driving motor 9, a connecting portion 11 is provided on the rotating cylinder 8, the connecting portion 11 is slidably connected to the base 1, the driving motor 9 is fixed to the connecting portion 11, a tooth plate 12 is provided on the base 1, and the gear 10 is meshed with the tooth plate 12. A limiting structure (such as a stopper) is provided between the connecting portion 11 and the rotating cylinder 8 to prevent the connecting portion 11 and the rotating cylinder 8 from being separated from each other. Figure 7 Specifically, the connecting portion 11 includes an annular segment and a long strip segment, and the long strip segment is located below the annular segment, the annular segment is sleeved on the outside of the rotating cylinder 8, a second slide groove 13 is provided on the inner bottom wall of the base 1, the bottom of the long strip segment is slidably connected to the second slide groove 13, the tooth plate 12 is fixedly connected to the inner bottom wall of the base 1, and is arranged along the length direction of the base 1, that is, the tooth plate 12 is arranged parallel to the second slide groove 13, the driving motor 9 is fixedly connected to the side wall of the long strip segment, and the output end of the driving motor 9 passes through the long strip segment and is fixedly connected to the gear 10, and the limiting structure can It is an annular structure arranged on the outer circumferential surface of the rotating cylinder 8, and an annular groove matching it is opened on the inner wall of the annular segment, and the two are rotatably connected, so that the annular segment and the rotating cylinder 8 can rotate relative to each other, but cannot slide relative to each other in the circumferential direction. The purpose of such a setting is to control the rotation of the gear 10 at its output end by driving the motor 9. The meshing action between the gear 10 and the tooth plate 12 can drive the connecting part 11 and the rotating cylinder 8 to reciprocate along the fixed axis 7, thereby driving the seat 3 to reciprocate to simulate the straight flight state of the aircraft.

[0040] Furthermore, the fixed shaft 7 is provided with a guide rail 14, a first branch rail 15, a second branch rail 16 and a third branch rail 17, and the rotating cylinder 8 is provided with a sliding portion 18, the sliding portion 18 is slidably connected to the guide rail 14, and one of the first branch rail 15, the second branch rail 16 and the third branch rail 17 is located on the movement stroke of the sliding portion 18. Specifically, the guide rail 14, the first branch rail 15, the second branch rail 16 and the third branch rail 17 are all provided on the outer circumference of the fixed shaft 7, and are arranged at intervals of approximately 30° with the fixed shaft 7 as the center, and the first branch rail 15 is located on the extension line of the guide rail 14, the second branch rail 16 and the third branch rail 17 are symmetrically arranged on both sides of the first branch rail 15, and the first branch rail 15, the second branch rail 16 and the third branch rail 17 are all connected to the guide rail 14, the sliding portion 18 is fixedly connected to the inner circumference of the rotating cylinder 8, and the size of the sliding portion 18 is similar to that of the guide rail 14, The sizes of the first branch rail 15, the second branch rail 16 and the third branch rail 17 are adapted to each other. The purpose of such a setting is that when the power mechanism drives the sliding part 18 from the guide rail 14 to the inside of the first branch rail 15, this is a simulated straight flight state. When the power mechanism drives the sliding part 18 from the guide rail 14 to the inside of the second branch rail 16 or the third branch rail 17, it will drive the rotating cylinder 8 and the seat 3 to rotate around the central axis of the fixed shaft 7 under the limiting effect of the sliding part 18, thereby simulating the state of the aircraft flying tilted to both sides.

[0041] Furthermore, a first baffle 19 is rotatably provided inside the second branch rail 16, and a second baffle 20 is rotatably provided on the third branch rail 17; and a driving assembly for driving the first baffle 19 and the second baffle 20 to rotate is also included. Specifically, the first baffle 19 is rotatably provided at the position where the guide rail 14 and the second branch rail 16 are connected, and the second baffle 20 is rotatably provided at the position where the guide rail 14 and the third branch rail 17 are connected, and the width of the first baffle 19 and the second baffle 20 is smaller than the depth of the guide rail 14. The driving assembly can also be a structure such as a motor for providing a rotational force. The effect of such a setting is that when the aircraft flies straight, the first baffle 19 and the second baffle 20 respectively close the second branch rail 16 and the third branch rail 17, and at this time, the sliding part 18 can only enter into the first branch rail 15 to realize the simulation of the aircraft flying straight. When the aircraft is simulating oblique flight, the first baffle 19 or the second baffle 20 will be driven to rotate by the driving assembly, so that the second baffle 19 or the second baffle 20 can rotate. When the opening of the branch rail 16 is opened (at this time, the second baffle 20 blocks the third branch rail 17), it will rotate clockwise to block the first branch rail 15, and the first baffle 19 itself will play a guiding role, that is, after the sliding part 18 abuts against the first baffle 19, the sliding part 18 will be introduced into the second branch rail 16. In the process of the sliding part 18 entering the second branch rail 16, the seat 3 will be tilted while moving along the axial direction of the fixed axis 7, thereby realizing the simulation of oblique flight. When the simulation is completed, the seat 3 is driven to move in the opposite direction by the power mechanism, which will cause the sliding part 18 to enter the guide rail 14, thereby switching the seat 3 from a tilted state to a vertical state to achieve the reset of the seat 3.

[0042] As an alternative solution for the above-mentioned motor to drive the first baffle 19 or the second baffle 20 to rotate, the driving assembly includes a push rod 21, a first rotating rod 22 is provided on the first baffle 19, and a second rotating rod 23 is provided on the second baffle 20, and one of the first rotating rod 22 and the second rotating rod 23 is located on the movement stroke of the push rod 21. Specifically, a cylindrical hole is opened inside the fixed shaft 7, and the cylindrical hole is arranged along the axial direction of the fixed shaft 7. The first rotating rod 22 and the second rotating rod 23 both penetrate the side wall of the fixed shaft 7 and extend into the cylindrical hole. The push rod 21 is rotatably connected with the cylindrical hole, and the push rod 21 can move axially along the cylindrical hole. An abutment portion 24 is provided on the push rod 21, and the abutment portion 24 is a protruding structure on the push rod 21. There is space inside the cylindrical hole for the abutment portion 24 to move. The first rotating rod 22 and the second rotating rod 23 are both L-shaped, and their vertical sections penetrate the cylindrical hole and are respectively fixed to the first baffle 19 and the second baffle 20. Its horizontal section is located on the movement stroke of the abutment portion 24, and torsion springs (not shown) are respectively arranged between the first rotating rod 22 and the second rotating rod 23 and the fixed shaft 7. The elastic force of the torsion spring makes the first baffle 19 have a tendency to rotate counterclockwise, and makes the second baffle 20 have a tendency to rotate clockwise. The effect of such arrangement is that when straight flight training is required, the first baffle 19 blocks the second branch rail 16, and the second baffle 20 blocks the third branch rail 17. At this time, the first branch rail 15 is in a conducting state, so that the sliding portion 18 can only enter the first branch rail 15. When oblique flight training is required, the sliding portion 18 is 18 enters the second branch rail 16, at this time, the push rod 21 is rotated to make the abutment portion 24 rotate toward the first rotating rod 22, and at this time, a force is applied to the push rod 21 to move toward the first rotating rod 22, so that the abutment portion 24 abuts against the horizontal section of the first rotating rod 22, so as to drive the first rotating rod 22 and the first baffle 19 to rotate (at this time, the position of the push rod 21 can be fixed by a bolt or a pin shaft), and the torsion spring is charged, so that the second branch rail 16 can be opened, so that the sliding portion 18 can only enter the second branch rail 16. When the training is completed, the sliding portion 18 is controlled to slide back to the guide rail 14, at this time, the push rod 21 is pulled in the reverse direction, so that the abutment portion 24 is separated from the horizontal section of the first rotating rod 22. At this time, the elastic force of the torsion spring is released, thereby driving the first baffle 19 to automatically reset. Similarly, when it is necessary to fly obliquely to the other side, the push rod 21 is rotated in the reverse direction, and then the push rod 21 is pushed axially along the fixed shaft 7. At this time, the abutment portion 24 will abut against the second rotating rod 23 to drive the second baffle 20 to rotate, so that the sliding portion 18 can only enter the third branch rail 17. In this way, the sliding portion 18 is controlled to enter the first branch rail 15, the second branch rail 16 or the third branch rail 17 according to different needs.

[0043] As another embodiment of the present invention, Figure 8As shown, the fixed shaft 7 is divided into a first section 25, a second section 26 and a lap section 27, and the lap section 27 is located between the first section 25 and the second section 26. Specifically, the guide rail 14 is arranged on the first section 25, the first branch rail 15, the second branch rail 16 and the third branch rail 17 are all arranged on the second section 26, and the lap section 27 is rotatably arranged between the first section 25 and the second section 26. Three lap rails 28 are arranged on the outer circumference of the lap section 27, and the three lap rails 28 are arranged corresponding to the three branch rails, respectively, one of the lap rails 28 is linear, and the other two lap rails 28 are arranged obliquely and symmetrically with respect to the linear lap rail 28. In this embodiment, a motor can be arranged on the base 1, and the output end of the motor is connected to the output end of the motor. The fixed shaft 7 is coaxially arranged and inserted into the fixed shaft 7 and connected with the center of the overlapping section 27. The purpose of such a setting is that when straight flight training is required, the linear overlapping rail 28 on the overlapping section 27 is connected to the first branch rail 15 through the motor control. When oblique flight training is required, the overlapping section 27 is rotated by controlling the motor so that one end of the inclined overlapping rail 28 is connected to the guide rail 14, and the other end is connected to the second branch rail 16 (or the third branch rail 17). In this way, the sliding part 18 can only enter the second branch rail 16, thereby completing the switching of various flight postures of the aircraft.

[0044] Furthermore, a protrusion 29 is provided on the side wall of the connecting position between the guide rail 14 and the second branch rail 16 and the third branch rail 17. Specifically, there are multiple protrusions 29, and they are located on the movement stroke of the sliding part 18. When the sliding part 18 enters the second branch rail 16 or the third branch rail 17, it will abut against the protrusion 29 on the inner wall thereof. Under the reaction force provided by the protrusion 29, the sliding part 18 will vibrate, thereby driving the entire seat 3 to vibrate, thereby simulating the bumpy state of the aircraft during flight.

[0045] As an alternative solution for the motor to drive the aileron 2 to swing, a connecting rod 30 is fixedly connected to the rotating cylinder 8, a transmission rod 31 is slidably provided on the mounting plate 4, a cross bar 32 is slidably provided on the transmission rod 31, a connecting shaft 33 is provided on the cross bar 32, and the connecting rod 30 is rotatably connected to the connecting shaft 33; and a transmission assembly for converting the linear motion of the transmission rod 31 into the swing of the aileron 2 is also included. The transmission assembly includes an arc groove 34 opened inside the transmission rod 31, a sliding rod 35 is fixedly connected to the rotating shaft 5, and the sliding rod 35 is slidably connected to the arc groove 34. Specifically, the connecting rod 30 is fixedly connected to the outer circumference of the rotating cylinder 8, the cross bar 32 is located below the rotating cylinder 8, and a rectangular hole 36 is opened in the middle position thereof. The connecting shaft 33 is fixedly connected inside the rectangular hole 36 and arranged along the width direction of the rectangular hole 36. The transmission rod 31 includes a first horizontal edge 37, a second horizontal edge 38 and a vertical edge 39. The first horizontal edge 37 is slidably connected to the mounting plate 4. A through hole 40 is opened at the top of the vertical edge 39. The rotating shaft 5 is rotatably connected to the through hole 40. The sliding rod 35 is fixedly connected to the outer circumference of the rotating shaft 5. The arc groove 34 is arranged on the inner wall of the through hole 40 and arranged along the axial direction and circumferential direction of the through hole 40, that is, the arc groove 34 is inclined (approximately spiral), and the inclination directions of the two arc grooves 34 on the two transmission rods 31 are opposite, and convex limiting portions 42 are provided at both ends of the cross bar 32, and a vertical groove 41 adapted to the limiting portion 42 is provided at the end of the first horizontal edge 37. The effect of such a setting is that when the power mechanism drives the seat 3 to rotate, it will drive the cross bar 32 through the action of the connecting rod 30 and the connecting shaft 33. The rod 32 moves vertically while swinging horizontally, and the distance of its vertical movement is adapted by the sliding of the limit portion 42 and the vertical groove 41. The distance of its horizontal movement will drive the transmission rod 31 to move horizontally, thereby driving the through hole 40 and the arc groove 34 to move horizontally synchronously. Since the arc groove 34 is arranged obliquely and the slide bar 35 is slidably connected to the arc groove 34, the slide bar 35 and the shaft 5 are driven to rotate. Since the shaft 5 is fixed to the aileron 2 and the inclination directions of the two arc grooves 34 are opposite, one aileron is driven 2 swings upward, and the other aileron 2 swings downward (preferably, in order to fit the actual flight situation, when the seat 3 tilts to one side, the aileron 2 on that side swings upward to provide a downward force on the wing, and the aileron 2 on the opposite side swings downward to provide an upward force on the wing), so as to achieve the swing training of the aileron 2. When the seat 3 switches from the tilted state to the vertical state, it will drive the connecting rod 30 to swing in the opposite direction, thereby driving the transmission rod 31 to move in the opposite direction, and driving the aileron 2 to swing in the opposite direction, so as to achieve the automatic reset of the aileron 2.

[0046] In summary, when the power mechanism drives the sliding part 18 to enter the first branch rail 15, the second branch rail 16 (or the third branch rail 17), it has the following strokes: first, it drives the sliding part 18 to enter the first branch rail 15 to simulate the state of the aircraft flying straight; second, it drives the seat 3 to tilt to simulate the tilting state when the aircraft turns; third, it drives the transmission rod 31 to move, and drives the aileron 2 to swing through the transmission rod 31 to simulate the state of the aileron 2 swinging when the aircraft turns; fourth, it drives the seat 3 to move along the fixed axis 7 to simulate the state of the aircraft flying obliquely; fifth, in the process of the sliding part 18 entering the second branch rail 16, it abuts against the protrusion 29 to simulate the state of the aircraft bumping.

[0047] The above description is only by way of illustration of certain exemplary embodiments of the present invention. It is undoubted that those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present invention. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present invention.

Claims

1. An aircraft mechanics comprehensive training device, comprising a base and an aileron rotatably arranged on the base, characterized in that: A seat is also rotatably arranged on the base; It also includes a power mechanism, which drives the aileron to swing adaptively while driving the seat to tilt; A mounting plate is slidably arranged on the base, a rotating shaft is arranged on the aileron, and the rotating shaft is rotatably connected to the mounting plate; A fixed shaft is fixedly connected to the base, and a rotating cylinder is provided on the seat, and the rotating cylinder is rotatably connected to the fixed shaft; The fixed shaft is provided with a guide rail, a first branch rail, a second branch rail and a third branch rail, the rotating cylinder is provided with a sliding part, the sliding part is slidably connected with the guide rail, and one of the first branch rail, the second branch rail and the third branch rail is located on the movement stroke of the sliding part; The guide rail, the first branch rail, the second branch rail and the third branch rail are all opened on the outer circumferential surface of the fixed shaft, the first branch rail, the second branch rail and the third branch rail are arranged at 30° intervals with the fixed shaft as the center, the first branch rail is located on the extension line of the guide rail, the second branch rail and the third branch rail are symmetrically arranged on both sides of the first branch rail, and the first branch rail, the second branch rail and the third branch rail are all connected to the guide rail, and the sliding part is fixedly connected to the inner circumferential surface of the rotating cylinder.

2. The aircraft mechanics comprehensive training equipment according to claim 1, characterized in that: The power mechanism includes a driving motor and a gear connected to the output end of the driving motor. A connecting portion is provided on the rotating cylinder, and the connecting portion is slidably connected to the base. The driving motor is fixed to the connecting portion. A toothed plate is provided on the base, and the gear is meshed with the toothed plate.

3. The aircraft mechanics comprehensive training equipment according to claim 2, characterized in that: A limiting structure is provided between the connecting portion and the rotating cylinder to prevent the connecting portion and the rotating cylinder from being separated from each other.

4. The aircraft mechanics comprehensive training equipment according to claim 1, characterized in that: A first baffle is rotatably disposed inside the second branch rail, and a second baffle is rotatably disposed on the third branch rail; It also includes a driving assembly for driving the first baffle plate and the second baffle plate to rotate.

5. The aircraft mechanics comprehensive training equipment according to claim 4, characterized in that: The driving assembly includes a push rod, a first rotating rod is arranged on the first baffle plate, a second rotating rod is arranged on the second baffle plate, and one of the first rotating rod and the second rotating rod is located on the movement stroke of the push rod.

6. The aircraft mechanics comprehensive training equipment according to claim 1, characterized in that: A connecting rod is fixedly connected to the rotating cylinder, a transmission rod is slidably arranged on the mounting plate, a cross bar is slidably arranged on the transmission rod, a connecting shaft is arranged on the cross bar, and the connecting rod is rotatably connected to the connecting shaft; and a transmission component is also included for converting the linear motion of the transmission rod into the swing of the aileron.

7. The aircraft mechanics comprehensive training equipment according to claim 6, characterized in that: The transmission assembly comprises an arc groove opened inside the transmission rod, a sliding rod is fixedly connected to the rotating shaft, and the sliding rod is slidably connected to the arc groove.

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