Aero-engine air inlet composite material forming equipment and forming method

Through the composite forming equipment and molding methods of aircraft engine air intake passage, the problem of insufficient mechanical strength of the air intake passage is solved, and the effect of improving mechanical strength and safety is achieved, ensuring that uniform air flow is provided in various flight states.

CN119502368APending Publication Date: 2025-02-25CHENGDU HONGXIA TECH CO LTD
View PDF 0 Cites 0 Cited by

Patent Information

Application Number
CN202411674494.1
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-11-21
Publication Date
2025-02-25

AI Technical Summary

Technical Problem

The existing aircraft engine intake air ducts have insufficient mechanical strength when under heavy pressure, resulting in low safety and high failure rates, and it is difficult to provide uniform airflow in various flight states and engine operating states.

Method used

The air intake composite molding equipment and molding methods of aircraft engine air intake passage are adopted, and the movement of air intake passage parts, clamping and welding of reinforcement ribs are achieved through technical means such as mobile devices, clamping devices, movable welding devices and carbon fiber molds. And the molding of carbon fiber composite materials to improve mechanical strength and safety.

Benefits of technology

By increasing the mechanical strength and safety of the intake duct, extending service life, ensuring uniform airflow is provided in various flight states and engine operating states, reducing failure rates.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN119502368A_ABST
    Figure CN119502368A_ABST
Patent Text Reader

Abstract

The invention relates to the technical field of air inlet composite material forming, and discloses aero-engine air inlet composite material forming equipment and a forming method.The front face of a machining cabinet body is fixedly provided with a slope, the side face of the machining cabinet body is provided with a clamping window, and the right side of the interior of the machining cabinet body is provided with a first groove; a second groove is formed in the inner top face of the machining cabinet body, a third groove is formed in the inner top face of the machining cabinet body, a moving device is arranged on the inner top face of the machining cabinet body, and a clamping device is arranged on the right side of the inner portion of the machining cabinet body. According to the aero-engine air inlet composite material forming equipment and method, firstly, a to-be-machined part is placed below a moving device, the machine is started, the moving device descends, a lifting rod descends through an air cylinder, a push block makes contact with a contact ball to support a supporting rod, and a supporting plate supports and moves the inner wall of the to-be-machined part; and a layer of rubber anti-skid material covering the surface of the supporting plate has a very good anti-skid effect.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The present invention relates to the technical field of air intake composite material forming, and in particular to an aircraft engine air intake composite material forming equipment and a forming method. Background Art

[0002] The aircraft engine air inlet is the flow channel through which the aircraft engine sucks in air. It is a core component of the aircraft propulsion system. It is specially designed to provide a certain quality of air flow for the aircraft engine and can introduce the free-flowing air in front of the aircraft engine into the engine.

[0003] The design of the air inlet is crucial to the performance of aircraft engines. It needs to provide uniform and satisfactory airflow in various flight conditions and engine operating conditions. Summary of the invention

[0004] 1. Technical issues to be solved

[0005] In view of the deficiencies in the prior art, the present invention provides an aircraft engine air inlet composite molding equipment and molding method to solve the problems raised in the above background technology.

[0006] (II) Technical solution

[0007] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: an aircraft engine air intake composite molding equipment and molding method, wherein a slope is fixedly installed on the front of the processing cabinet, a clamping window is opened on the side of the processing cabinet, a groove one is opened on the inner right side of the processing cabinet, a groove two is opened on the inner top surface of the processing cabinet, a groove three is opened on the inner top surface of the processing cabinet, a moving device is arranged on the inner top surface of the processing cabinet, a clamping device is arranged on the inner right side of the processing cabinet, and a reinforcing rib is clamped on the end of the clamping device away from the processing cabinet, a movable welding device one is arranged on the inner top surface of the processing cabinet, a movable welding device two is fixedly installed on the inner bottom surface of the processing cabinet, a turntable groove is opened on the inner bottom surface of the processing cabinet, and a turntable is movably installed on the top surface of the turntable groove, hydraulic rods three are fixedly installed on both sides of the interior of the processing cabinet, a clamping plate is fixedly installed on the telescopic end of the hydraulic rod three, a carbon fiber mold is arranged on the side of the clamping plate away from the telescopic end, and an upwardly protruding part fixing block is arranged on the inner bottom surface of the processing cabinet, and a part to be processed is sleeved on the outer side of the part fixing block.

[0008] Preferably, the moving device includes a moving slider, a hydraulic rod 1 is fixedly installed on the bottom surface of the moving slider, auxiliary rods are fixedly installed on the four corners of the bottom surface of the moving slider, a limit plate is fixedly installed on the bottom surface of the auxiliary rod, a cylinder is fixedly installed on the bottom surface of the hydraulic rod 1, a fixed shell is fixedly installed on the bottom surface of the cylinder, a lifting rod is fixedly installed on the bottom surface of the cylinder, a push block is fixedly installed on the telescopic end of the lifting rod, a support rod is movably installed on the side of the fixed shell, a contact ball is fixedly installed on the end of the support rod close to the push block, a support plate is fixedly installed on the side of the support rod away from the contact ball, a return spring is sleeved on the outer side of the support rod, and a side of the support plate away from the support rod is covered with a layer of rubber anti-slip material.

[0009] Through the above technical scheme, when it is necessary to move the parts to be processed, after the moving device is moved to the top of the parts to be processed, the hydraulic rod starts to descend, and after reaching the appropriate position, the hydraulic rod stops descending, the cylinder starts to run, and the lifting rod is controlled to descend. The push block installed on the telescopic end of the lifting rod contacts the contact ball, and the support rod is pushed out of the fixed shell, so that the support plate at the other end of the support rod away from the contact ball contacts the inner wall of the parts to be processed, and a layer of rubber anti-slip material covering the surface of the support plate can play an anti-slip role between the support plate and the parts to be processed, so that the moving device can better move the parts to be processed and will not fall off, and when it is necessary to remove the processed air intake duct, the lifting rod rises to make the push block rise, and the return spring lifts the contact ball, so that the support rod is retracted to its initial position.

[0010] Preferably, the clamping device includes a hydraulic rod 2, an angle steel is fixedly installed on the top surface of the hydraulic rod 2, a clamping hand is fixedly installed on the telescopic end of the hydraulic rod 2, grooves 4 are provided on the left and right sides of the inner side of the clamping hand, a connecting base is fixedly installed on the end of the hydraulic rod 2 away from the telescopic end, and a slider 1 is fixedly installed on the side of the connecting base away from the hydraulic rod 2.

[0011] Through the above technical solution, since the air intake duct may be under tremendous pressure when in use, in order to make the parts safer and reduce the failure rate, a clamping device can be used to clamp the reinforcing ribs and movable welding device one and movable welding device two can be used to weld the reinforcing ribs, so that the mechanical strength of the air intake duct is reinforced, which greatly improves the safety and prolongs the service life.

[0012] Preferably, the movable welding device comprises an electric telescopic rod, a welding gun holder is fixedly mounted on the telescopic end of the electric telescopic rod, a slider base is fixedly mounted on the end of the electric telescopic rod away from the telescopic end, a slider is fixedly mounted on the top surface of the slider base, and a welding gun is arranged on the inner side of the welding gun holder.

[0013] Through the above technical solution, the parts to be processed are placed on the top surface of the turntable, and the position of the reinforcing ribs is adjusted according to the position of the parts to be processed. After the adjustment, the movable welding device 1 and the movable welding device 2 are adjusted according to the position of the reinforcing ribs to weld the reinforcing ribs.

[0014] Preferably, the movable welding device 2 includes an electric telescopic rod, a welding gun rack 2 is fixedly installed on the telescopic end of the electric telescopic rod 2, a welding gun is arranged on the inner side of the welding gun rack 2, a slider 3 base is fixedly installed on the bottom surface of the electric telescopic rod 2, and a slider 3 is fixedly installed on the bottom surface of the slider 3 base.

[0015] Through the above technical solution, the reinforcing ribs need to be welded on both the upper and lower sides during welding. A pair of movable welding devices can weld the upper side of the reinforcing ribs, and a movable welding device can weld the lower side of the reinforcing ribs. Welding at both locations simultaneously can effectively improve the processing efficiency, and welding at both locations can also better reinforce the mechanical strength of the parts to be processed by the reinforcing ribs.

[0016] Preferably, the carbon fiber mold includes mold one and mold two, the side of mold one is provided with an injection port, the side of mold one is fixedly installed with a clamp, the end of the clamp away from the mold is fixedly installed with a hydraulic rod three, and the side of mold two is provided with an injection port.

[0017] Through the above technical solution, the part to be processed is placed on the outside of the part fixing block, and the carbon fiber mold is started to move. The molds on both sides are pushed by hydraulic rod 3 to move and merge to completely cover the part to be processed. At this time, the hot-melted carbon fiber material is injected into the carbon fiber mold through the injection port. After the shaping is completed, the hydraulic rod 3 is started to drive the clamping plate to separate the molds on both sides. The processed air intake is then removed.

[0018] Preferably, a groove is provided on the side surface of the reinforcing rib, and the position of the groove is staggered with the position of the side surface of the reinforcing rib.

[0019] Through the above technical scheme, a clamping window is opened on the side of the processing cabinet, and the reinforcement ribs required for processing can be uniformly placed on the outside of the clamping window. During processing, the hydraulic rod 2 can be controlled to drive the clamp to extend and retract, and the groove 4 on the side of the clamp can clamp the reinforcement rib by inserting into the staggered grooves on the side of the reinforcement rib. When the mobile device places the part to be processed on the upper side of the turntable, the movable welding device 1 and the movable welding device 2 can weld the reinforcement rib when clamping the reinforcement rib, and after welding is completed, the new reinforcement rib is automatically clamped through the clamping window.

[0020] Preferably, the movable slider is movably installed in groove three, the slider one is movably installed in groove one, the slider two is movably installed in groove two, and the slider three is movably installed in groove five.

[0021] Through the above technical scheme, the moving device moves the slider along the groove three to realize the transportation of the parts to be processed, the clamping device moves the slider one in the groove one to realize the adjustment of the upper and lower positions of the reinforcing ribs, the movable welding device one realizes the position adjustment through the slider two, and the movable welding device realizes the position adjustment through the slider three.

[0022] Preferably, a turntable is arranged inside the turntable groove, and a part to be processed is arranged on the top surface of the turntable.

[0023] Through the above technical solution, after the mobile device places the part to be processed on the top surface of the turntable, the turntable starts to rotate, so that the movable welding device 1 and the movable welding device 2 can weld the reinforcing ribs at various connections of the part to be processed.

[0024] The present invention also provides a method for molding a composite material of an aero-engine air intake duct, and the molding method is as follows:

[0025] S1: Place the workpiece to be processed under the moving device and start the machine, so that the moving device is lowered and the lifting rod is lowered by the cylinder, and the support rod is supported by the push block and the contact ball so that the support plate supports the inner wall of the workpiece to be processed and moves;

[0026] S2: Before the moving device places the part to be processed on the top surface of the turntable, the clamping device is controlled to clamp the reinforcing rib and place it on the top surface of the turntable. When the moving device drives the part to be processed to be placed on the top surface of the turntable, the clamping device starts to move up and down, and stops moving when it is adjusted to a suitable position;

[0027] S3: At this time, the movable welding device 1 is lowered to the upper side of the reinforcing rib, and the movable welding device 2 is raised to the lower side of the reinforcing rib, and the welding is started after the movable welding device 1 and the movable welding device 2 are adjusted to the specified position;

[0028] S4: During welding, the turntable rotates at a constant speed, so that the movable welding device 1 and the movable welding device 2 weld the entire circle of the upper and lower sides of the reinforcing rib. After welding, the movable welding device 1 and the movable welding device return to their original positions, the parts to be processed are removed, and the moving device is used to move the parts to be processed to the outside of the part fixing block. At this time, the hydraulic rod 3 is started to move the molds on both sides of the carbon fiber mold;

[0029] S5: After the carbon fiber mold completely wraps the part to be processed, connect the hose and inject the hot-melt carbon fiber material into the mold. After cooling, start the hydraulic rod 3 to separate the molds on both sides and remove the processed air intake duct.

[0030] Compared with the prior art, the present invention provides an aircraft engine air intake composite molding equipment and molding method, which has the following beneficial effects:

[0031] 1. The composite material forming equipment and forming method of the aircraft engine air intake duct, first, place the part to be processed under the moving device and start the machine, so that the moving device is lowered and the lifting rod is lowered by the cylinder, and the support plate is supported and moved by the push block and the contact ball to support the inner wall of the part to be processed. The layer of rubber anti-skid material covered on the surface of the support plate has a good anti-skid effect, which not only ensures that the possibility of the part to be processed falling can be reduced during movement, but also avoids the material of the inner wall being damaged by the support plate when supporting the inner wall. Before the moving device places the part to be processed on the top surface of the turntable, the clamping device is controlled to clamp the reinforcing rib and place it on the top surface of the turntable. When the moving device drives the part to be processed to be placed on the top surface of the turntable, the clamping device starts to move up and down to adjust the welding position of the reinforcing rib. When it is adjusted to a suitable position, it stops moving. At this time, the movable welding device first descends to the upper side of the reinforcing rib, and the movable welding device second rises to the lower side of the reinforcing rib.

[0032] 2. The composite material forming equipment and forming method of the aircraft engine air intake duct starts welding after the movable welding device 1 and the movable welding device 2 are adjusted to the appropriate position. The welding device that can adjust the position can adjust the position according to the size of the part to be processed. The electric telescopic rod that can be extended up and down also allows welding when facing parts with different positions of the reinforcement ribs, which further improves the use scenario of the machine. During welding, the turntable rotates at a uniform speed, so that the movable welding device 1 and the movable welding device 2 weld the upper and lower sides of the reinforcement ribs in a full circle, avoiding the need to use manpower to weld the reinforcement ribs in a full circle in the processing cabinet, saving the company's labor costs. After welding is completed, the movable welding device 1 and the movable welding device return to their original positions, remove the parts to be processed, and use the movable welding device 1 to weld the parts to be processed. The moving device moves the part to be processed to the outside of the part fixing block. At this time, the hydraulic rod three is started to move the molds on both sides of the carbon fiber mold. After the carbon fiber mold completely wraps the part to be processed, the hose is connected to inject the hot-melt carbon fiber material into the mold. After cooling, the hydraulic rod three is started to separate the molds on both sides and the processed air intake duct is removed. Carbon fiber composite materials have high vibration damping, can effectively absorb and disperse vibration energy, thereby reducing structural vibration and noise, have good resistance to chemical substances such as acids, alkalis, and salts, are not easily corroded, and can maintain their physical and chemical properties in high temperature environments. When impacted, they can effectively absorb impact energy, thereby reducing damage to the structure and improving the safety of vehicles, which is particularly important in fields such as aerospace. BRIEF DESCRIPTION OF THE DRAWINGS

[0033] Figure 1 The three-dimensional structure of the present invention is shown in FIG. Figure 1 ;

[0034] Figure 2 The three-dimensional structure of the present invention is shown in FIG. Figure 2 ;

[0035] Figure 3 It is a schematic diagram of the processing cabinet structure of the present invention;

[0036] Figure 4 It is a cross-sectional schematic diagram of a processing cabinet of the present invention;

[0037] Figure 5 is a cross-sectional schematic diagram of a mobile device of the present invention;

[0038] Figure 6 It is a schematic diagram of the structure of the mobile device of the present invention;

[0039] Figure 7 This is a schematic diagram of the support plate structure of the present invention;

[0040] Figure 8 It is a schematic diagram of the structure of the clamping device of the present invention;

[0041] Fig. 9 It is a structural schematic diagram of a movable welding device of the present invention;

[0042] Fig.10 It is a schematic diagram of the carbon fiber mold structure of the present invention;

[0043] Fig.11 It is a structural schematic diagram of the movable welding device 2 of the present invention.

[0044] In the figure: 1. Processing cabinet; 2. Slope; 3. Clamping window; 4. Groove 1; 5. Groove 2; 6. Groove 3; 7. Moving device; 701. Moving slider; 702. Hydraulic rod 1; 703. Auxiliary rod; 704. Limit plate; 705. Cylinder; 706. Fixed shell; 707. Lifting rod; 708. Push block; 709. Contact ball; 710. Return spring; 711. Support plate; 8. Clamping device; 801. Hydraulic rod 2; 802. Angle steel; 803. Clamping hand; 804. Groove 4; 805. Slider 1; 806. Connecting base; 9. Reinforcement rib; 10 , turntable; 11, movable welding device one; 1101, electric telescopic rod one; 1102, welding gun stand one; 1103, slider base; 1104, slider two; 12, movable welding device two; 1201, electric telescopic rod two; 1202, welding gun stand two; 1203, slider three base; 1204, slider three; 13, hydraulic rod three; 14, clamp; 15, carbon fiber mold; 1501, mold one; 1502, injection port; 1503, mold two; 16, parts to be processed; 17, welding gun; 18, turntable groove; 19, part fixing block; 20, groove five. DETAILED DESCRIPTION

[0045] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0046] like Figure 1-4 As shown, the present invention provides a technical solution: an aircraft engine air intake duct composite molding equipment and molding method, a ramp 2 is fixedly installed on the front of the processing cabinet 1, a clamping window 3 is opened on the side of the processing cabinet 1, a groove 1 4 is opened on the right side of the interior of the processing cabinet 1, a groove 2 5 is opened on the top surface of the interior of the processing cabinet 1, a groove 3 6 is opened on the top surface of the interior of the processing cabinet 1, a moving device 7 is arranged on the top surface of the interior of the processing cabinet 1, a clamping device 8 is arranged on the right side of the interior of the processing cabinet 1, and a reinforcing rib 9 is clamped on the end of the clamping device 8 away from the processing cabinet 1, and the interior of the processing cabinet 1 is provided with a plurality of grooves 1, 2, 3, 4, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47, 48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62, 64, 65, 66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77, 7 A movable welding device 11 is arranged on the top surface of the processing cabinet 1, a movable welding device 2 12 is fixedly installed on the inner bottom surface of the processing cabinet 1, a turntable groove 18 is opened on the inner bottom surface of the processing cabinet 1, a turntable 10 is movably installed on the top surface of the turntable groove 18, hydraulic rods 3 13 are fixedly installed on both sides of the interior of the processing cabinet 1, a clamping plate 14 is fixedly installed on the telescopic end of the hydraulic rod 3 13, a carbon fiber mold 15 is arranged on the side of the clamping plate 14 away from the telescopic end, an upwardly protruding part fixing block 19 is arranged on the inner bottom surface of the processing cabinet 1, and a part 16 to be processed is sleeved on the outer side of the part fixing block 19.

[0047] Furthermore, the moving device 7 includes a moving slider 701, a hydraulic rod 702 is fixedly installed on the bottom surface of the moving slider 701, auxiliary rods 703 are fixedly installed at the four corners of the bottom surface of the moving slider 701, a limit plate 704 is fixedly installed on the bottom surface of the auxiliary rod 703, a cylinder 705 is fixedly installed on the bottom surface of the hydraulic rod 702, a fixed shell 706 is fixedly installed on the bottom surface of the cylinder 705, a lifting rod 707 is fixedly installed on the bottom surface of the cylinder 705, a push block 708 is fixedly installed on the telescopic end of the lifting rod 707, a support rod 712 is movably installed on the side of the fixed shell 706, a contact ball 709 is fixedly installed on the end of the support rod 712 close to the push block 708, a support plate 711 is fixedly installed on the side of the support rod 712 away from the contact ball 709, a return spring 710 is sleeved on the outer side of the support rod 712, and a layer of rubber anti-slip material is covered on the side of the support plate 711 away from the support rod 712.

[0048] Specifically, when it is necessary to move the part 16 to be processed, the moving device 7 is moved to the top of the part 16 to be processed, and the hydraulic rod 702 starts to descend. After reaching the appropriate position, the hydraulic rod 702 stops descending, and the cylinder 705 starts to operate to control the lifting rod 707 to descend. The push block 708 installed on the telescopic end of the lifting rod 707 contacts the contact ball 709, and the support rod 712 is pushed out of the fixed shell 706, so that the support plate 711 at the other end of the support rod 712 away from the contact ball 709 contacts the inner wall of the part 16 to be processed. The layer of rubber anti-slip material covering the surface of the support plate 711 plays a good anti-slip role between the support plate 711 and the part 16 to be processed, so that the moving device 7 can better move the part 16 to be processed and will not fall.

[0049] Furthermore, the clamping device 8 includes a hydraulic rod 801, an angle steel 802 is fixedly installed on the top surface of the hydraulic rod 801, a clamping hand 803 is fixedly installed on the telescopic end of the hydraulic rod 801, grooves 804 are provided on the left and right sides of the inner side of the clamping hand 803, a connecting base 806 is fixedly installed on the end of the hydraulic rod 801 away from the telescopic end, and a slider 805 is fixedly installed on the side of the connecting base 806 away from the hydraulic rod 801.

[0050] Specifically, since the air intake duct may be subjected to enormous pressure during use, in order to make the parts safer and reduce the failure rate, a clamping device 8 can be used to clamp the reinforcing rib 9 and a movable welding device 1 11 and a movable welding device 2 12 can be used to weld the reinforcing rib 9, so that the mechanical strength of the air intake duct is reinforced, which greatly improves the safety and prolongs the service life.

[0051] Furthermore, the movable welding device 11 includes an electric telescopic rod 1101, the telescopic end of the electric telescopic rod 1101 is fixedly installed with a welding gun holder 1102, the end of the electric telescopic rod 1101 away from the telescopic end is fixedly installed with a slider base 1103, the top surface of the slider base 1103 is fixedly installed with a slider 2 1104, and a welding gun 17 is arranged on the inner side of the welding gun holder 1102.

[0052] Specifically, the part to be processed 16 is placed on the top surface of the turntable 10, and the position of the reinforcing rib 9 is adjusted according to the position of the part to be processed 16. After the adjustment, the movable welding device 11 and the movable welding device 2 12 are adjusted according to the position of the reinforcing rib 9 to weld the reinforcing rib 9.

[0053] Furthermore, the movable welding device 12 includes an electric telescopic rod 1201, a welding gun rack 1202 is fixedly installed on the telescopic end of the electric telescopic rod 1201, a welding gun 17 is arranged on the inner side of the welding gun rack 1202, a slider 3 base 1203 is fixedly installed on the bottom surface of the electric telescopic rod 1201, and a slider 3 1204 is fixedly installed on the bottom surface of the slider 3 base 1203.

[0054] Specifically, the reinforcing rib 9 needs to be welded on both the upper and lower sides during welding. The movable welding device 11 welds the upper side of the reinforcing rib 9, and the movable welding device 12 welds the lower side of the reinforcing rib 9. Welding at both locations simultaneously can effectively improve the processing efficiency, and welding is performed at both locations.

[0055] Furthermore, the carbon fiber mold 15 includes a mold 1 1501 and a mold 2 1503, a material injection port 1502 is provided on the side of the mold 1 1501, a clamp 14 is fixedly installed on the side of the mold 1 1501, a hydraulic rod 3 13 is fixedly installed on the end of the clamp 14 away from the mold 1 1501, and a material injection port 1502 is provided on the side of the mold 2 1503.

[0056] Specifically, after the previous process is completed, the moving device 7 controls the part to be processed 16 to the designated position, and the part to be processed 16 is placed on the outside of the part fixing block 19, and then the carbon fiber mold 15 is started to move. The molds on both sides are pushed by the hydraulic rod 3 13 to move the clamping plate 14 to completely cover the part to be processed 16 after merging. At this time, the hot-melted carbon fiber material is injected into the carbon fiber mold 15 through the injection port 1502, and after the shaping is completed, the hydraulic rod 3 13 is started to drive the clamping plate 14 to separate the molds on both sides. The processed air intake duct is then removed.

[0057] Furthermore, a groove is provided on the side of the reinforcing rib 9, and the position of the groove 804 is staggered with the position of the side of the reinforcing rib 9.

[0058] Specifically, a clamping window 3 is opened on the side of the processing cabinet 1, and the reinforcing ribs 9 required for processing can be uniformly placed on the outside of the clamping window 3. During processing, the hydraulic rod 801 can be controlled to drive the clamp 803 to extend and retract, and the groove 4 804 on the side of the clamp 803 can clamp the reinforcing rib 9 by being inserted into the staggered grooves on the side of the reinforcing rib 9. When the moving device 7 places the part 16 to be processed on the upper side of the turntable 10, the movable welding device 1 11 and the movable welding device 2 12 can weld the reinforcing rib 9 when clamping the reinforcing rib 9, and after welding is completed, the new reinforcing rib 9 is automatically clamped through the clamping window 3.

[0059] Further, the movable slider 701 is movably installed in the groove three 6, the slider one 805 is movably installed in the groove one 4, the slider two 1104 is movably installed in the groove two 5, and the slider three 1204 is movably installed in the groove five 20.

[0060] Specifically, the moving device 7 moves the slider 701 along the groove three 6 to achieve the transportation of the workpiece 16 to be processed, the clamping device 8 moves the slider 805 in the groove 4 to achieve the adjustment of the upper and lower positions of the reinforcing rib 9, the movable welding device 11 achieves position adjustment through the slider two 1104, and the movable welding device 12 achieves position adjustment through the slider three 1204.

[0061] Furthermore, a turntable 10 is disposed inside the turntable groove 18 , and a part 16 to be processed is disposed on the top surface of the turntable 10 .

[0062] Specifically, after the mobile device 7 places the part 16 to be processed on the top surface of the turntable 10, the turntable 10 starts to rotate, so that the movable welding device 1 11 and the movable welding device 2 12 can weld the reinforcing ribs 9 at various connections of the part 16 to be processed.

[0063] A composite material forming method for an aircraft engine air intake duct, the forming method is as follows:

[0064] S1: Place the workpiece 16 to be processed under the moving device 7 and start the machine, so that the moving device 7 is lowered and the lifting rod 707 is lowered by the cylinder 705, and the support rod 712 is propped up by the push block 708 and the contact ball 709 so that the support plate 711 supports the inner wall of the workpiece 16 to be processed and moves;

[0065] S2: before the moving device 7 places the workpiece 16 to be processed on the top surface of the turntable 10, the clamping device 8 is controlled to clamp the reinforcing rib 9 and place it on the top surface of the turntable 10. When the moving device 7 drives the workpiece 16 to be processed to be placed on the top surface of the turntable 10, the clamping device 8 starts to move up and down, and stops moving when it is adjusted to a suitable position;

[0066] S3: At this time, the movable welding device 1 11 starts to descend to the upper side of the reinforcing rib 9, and the movable welding device 2 12 rises to the lower side of the reinforcing rib 9, and after the movable welding device 1 11 and the movable welding device 2 12 are adjusted to the specified position, welding begins;

[0067] S4: During welding, the turntable 10 rotates at a constant speed, so that the movable welding device 11 and the movable welding device 2 12 weld the entire circle of the upper and lower sides of the reinforcing rib 9. After welding, the movable welding device 11 and the movable welding device 12 return to their original positions, remove the part 16 to be processed, and use the moving device 7 to move the part 16 to the outside of the part fixing block 19. At this time, when the hydraulic rod 3 13 is started, the molds on both sides of the carbon fiber mold 15 are moved;

[0068] S5: After the carbon fiber mold 15 completely wraps the part to be processed 16, connect the hose and inject the hot-melted carbon fiber material into the mold. After cooling, start the hydraulic rod 3 13 to separate the molds on both sides and remove the processed air intake duct.

[0069] Working principle: First, place the part 16 to be processed under the moving device 7 and start the machine, so that the moving device 7 descends and the lifting rod 707 is lowered by the cylinder 705, and the support rod 712 is supported by the push block 708 and the contact ball 709 to make the support plate 711 support and move the inner wall of the part 16 to be processed. Before the moving device 7 places the part 16 to be processed on the top of the turntable 10, control the clamping device 8 to clamp the reinforcing rib 9 and place it on the top surface of the turntable 10. When the moving device 7 drives the part 16 to be processed to be placed on the top surface of the turntable 10, the clamping device 8 starts to move up and down, and stops moving when it is adjusted to a suitable position. At this time, the movable welding device 11 begins to descend to the upper side of the reinforcing rib 9, and the movable welding device 2 12 rises to the lower side of the reinforcing rib 9, waiting for the movable welding After the connecting device 11 and the movable welding device 2 12 are adjusted to the specified position, welding begins. During welding, the turntable 10 rotates at a uniform speed so that the movable welding device 11 and the movable welding device 2 12 weld the entire circle of the upper and lower sides of the reinforcing rib 9. After welding is completed, the movable welding device 11 and the movable welding device 12 return to their original positions, the part to be processed 16 is removed, and the movable device 7 is used to move the part to be processed 16 to the outside of the part fixing block 19. At this time, when the hydraulic rod 3 13 is started, the molds on both sides of the carbon fiber mold 15 are moved. After the carbon fiber mold 15 completely wraps the part to be processed 16, the hose is connected to inject the hot-melt carbon fiber material into the mold. After cooling, the hydraulic rod 3 13 is started to separate the molds on both sides, and the processed air intake duct is removed.

[0070] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An aircraft engine air intake composite molding equipment and molding method, comprising a processing cabinet (1), characterized in that: The front of the processing cabinet (1) is fixedly provided with a slope (2), the side of the processing cabinet (1) is provided with a clamping window (3), the right side of the interior of the processing cabinet (1) is provided with a groove one (4), the top surface of the interior of the processing cabinet (1) is provided with a groove two (5), the top surface of the interior of the processing cabinet (1) is provided with a groove three (6), the top surface of the interior of the processing cabinet (1) is provided with a moving device (7), the right side of the interior of the processing cabinet (1) is provided with a clamping device (8), the end of the clamping device (8) away from the processing cabinet (1) is clamped with a reinforcing rib (9), and the top surface of the interior of the processing cabinet (1) is provided with a movable welding device one (1 1), a movable welding device 2 (12) is fixedly installed on the inner bottom surface of the processing cabinet (1), a turntable groove (18) is opened on the inner bottom surface of the processing cabinet (1), a turntable (10) is movably installed on the top surface of the turntable groove (18), hydraulic rods 3 (13) are fixedly installed on both sides of the interior of the processing cabinet (1), a clamping plate (14) is fixedly installed on the telescopic end of the hydraulic rod 3 (13), a carbon fiber mold (15) is arranged on the side of the clamping plate (14) away from the telescopic end, and an upwardly protruding part fixing block (19) is arranged on the inner bottom surface of the processing cabinet (1), and a part to be processed (16) is sleeved on the outer side of the part fixing block (19).

2. The composite material forming equipment and forming method for an aircraft engine air intake duct according to claim 1, characterized in that: The moving device (7) comprises a moving slider (701), a hydraulic rod (702) is fixedly mounted on the bottom surface of the moving slider (701), auxiliary rods (703) are fixedly mounted on the four corners of the bottom surface of the moving slider (701), a limit plate (704) is fixedly mounted on the bottom surface of the auxiliary rod (703), a cylinder (705) is fixedly mounted on the bottom surface of the hydraulic rod (702), a fixed shell (706) is fixedly mounted on the bottom surface of the cylinder (705), and a lifting rod (707) is fixedly mounted on the bottom surface of the cylinder (705). A push block (708) is fixedly installed at the telescopic end of the lifting rod (707), a support rod (712) is movably installed on the side of the fixed shell (706), a contact ball (709) is fixedly installed on one end of the support rod (712) close to the push block (708), a support plate (711) is fixedly installed on the side of the support rod (712) away from the contact ball (709), a return spring (710) is sleeved on the outer side of the support rod (712), and a layer of rubber anti-slip material is covered on one side of the support plate (711) away from the support rod (712).

3. The aircraft engine air intake composite molding equipment and molding method according to claim 1, characterized in that: The clamping device (8) includes a hydraulic rod 2 (801), an angle steel (802) is fixedly installed on the top surface of the hydraulic rod 2 (801), a clamping hand (803) is fixedly installed on the telescopic end of the hydraulic rod 2 (801), and grooves 4 (804) are provided on the left and right sides of the inner side of the clamping hand (803), and a connecting base (806) is fixedly installed on the end of the hydraulic rod 2 (801) away from the telescopic end, and a sliding block 1 (805) is fixedly installed on the side of the connecting base (806) away from the hydraulic rod 2 (801).

4. The aircraft engine air intake composite molding equipment and molding method according to claim 1, characterized in that: The movable welding device (11) comprises an electric telescopic rod (1101), a welding gun holder (1102) is fixedly mounted on the telescopic end of the electric telescopic rod (1101), a slider base (1103) is fixedly mounted on the end of the electric telescopic rod (1101) away from the telescopic end, a slider (1104) is fixedly mounted on the top surface of the slider base (1103), and a welding gun (17) is arranged on the inner side of the welding gun holder (1102).

5. The aircraft engine air intake composite molding equipment and molding method according to claim 1, characterized in that: The movable welding device 2 (12) comprises an electric telescopic rod (1201), a welding gun holder 2 (1202) is fixedly mounted on the telescopic end of the electric telescopic rod 2 (1201), a welding gun (17) is arranged on the inner side of the welding gun holder 2 (1202), a slider 3 base (1203) is fixedly mounted on the bottom surface of the electric telescopic rod 2 (1201), and a slider 3 (1204) is fixedly mounted on the bottom surface of the slider 3 base (1203).

6. The aircraft engine air intake composite molding equipment and molding method according to claim 1, characterized in that: The carbon fiber mold (15) comprises a mold one (1501) and a mold two (1503), the side of the mold one (1501) is provided with an injection port (1502), the side of the mold one (1501) is fixedly installed with a clamping plate (14), the clamping plate (14) is fixedly installed with a hydraulic rod three (13) at one end away from the mold one (1501), and the side of the mold two (1503) is provided with an injection port (1502).

7. The aircraft engine air intake composite molding equipment and molding method according to claim 1, characterized in that: A groove is provided on the side of the reinforcing rib (9), and the position of the groove 4 (804) is staggered with the position of the side of the reinforcing rib (9).

8. The aircraft engine air intake composite molding equipment and molding method according to claim 1, characterized in that: The movable slider (701) is movably mounted in groove three (6), the slider one (805) is movably mounted in groove one (4), the slider two (1104) is movably mounted in groove two (5), and the slider three (1204) is movably mounted in groove five (20); a turntable (10) is arranged inside the turntable groove (18), and a part to be processed (16) is arranged on the top surface of the turntable (10).

9. The composite material forming equipment for an aircraft engine air intake according to any one of claims 1 to 8, characterized in that: The molding method is as follows: S1: Place the part to be processed (16) below the moving device (7) and start the machine, so that the moving device (7) is lowered and the lifting rod (707) is lowered through the cylinder (705), and the support rod (712) is supported by the push block (708) and the contact ball (709) so that the support plate (711) supports the inner wall of the part to be processed (16) and moves; S2: before the moving device (7) places the part to be processed (16) on the top of the turntable (10), the clamping device (8) is controlled to clamp the reinforcing rib (9) and place it on the top of the turntable (10); when the moving device (7) drives the part to be processed (16) to be placed on the top of the turntable (10), the clamping device (8) starts to move up and down, and stops moving when it is adjusted to a suitable position; S3: At this time, the movable welding device 1 (11) begins to descend to the upper side of the reinforcing rib (9), and the movable welding device 2 (12) rises to the lower side of the reinforcing rib (9), and after the movable welding device 1 (11) and the movable welding device 2 (12) are adjusted to the specified position, welding begins; S4: During welding, the turntable (10) rotates at a constant speed, so that the movable welding device 1 (11) and the movable welding device 2 (12) weld the entire circle of the upper and lower sides of the reinforcing rib (9). After welding is completed, the movable welding device 1 (11) and the movable welding device (12) return to their original positions, the part to be processed (16) is removed, and the moving device (7) is used to move the part to be processed (16) to the outside of the part fixing block (19). At this time, the hydraulic rod 3 (13) is started to move the two side molds of the carbon fiber mold (15); S5: After the carbon fiber mold (15) completely wraps the part to be processed (16), connect the hose and inject the hot-melted carbon fiber material into the mold. After cooling, start the hydraulic rod three (13) to separate the molds on both sides and remove the processed air intake duct.