Forming equipment for aerospace propeller composite material
The molding device for aerospace propellers addresses inefficiencies in disassembly and cleaning by using electric push rods and snap-fit positioning, enabling quick mold changes and automated cleaning, thus improving efficiency and quality.
Patent Information
- Application Number
- CN202411083225.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-08
- Publication Date
- 2024-12-13
- Estimated Expiration
- Not applicable · inactive patent
AI Technical Summary
Existing molding devices for aerospace propellers face challenges with inconvenient and time-consuming disassembly and cleaning due to the use of expansion screws, affecting work efficiency and cleanliness.
A molding device featuring a workbench with electric push rods for mold movement, a mounting assembly with snap-fit positioning, and a cleaning assembly with scrapers and storage for efficient mold disassembly and material removal.
Facilitates rapid mold installation and disassembly, improves maintenance efficiency, and automates mold cleaning, reducing staff workload and enhancing propeller production quality.
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Figure CN119116239A_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the technical field of propellers, and more specifically, to a molding device for composite materials of aerospace propellers. Background Art
[0002] A propeller is a device that converts the engine's rotational power into propulsion by rotating blades in the air or water. It may have two or more blades connected to the hub, and the rearward side of the blade is a spiral surface or a propeller that is close to a spiral surface. With the advancement of aerospace technology, aerospace manned or unmanned aircraft models can be seen at large aerospace exhibitions, and propellers are also used on some aerospace aircraft models. In the prior art, hot-melt composite materials are poured into a mold of an aerospace propeller model, and then the aerospace propeller is formed by extrusion.
[0003] Aerospace propellers are formed by molds. When the molds are used for a long time, they need to be disassembled for inspection or replacement. Currently, the molds are mostly installed by expansion screws, which is not convenient for quick installation and disassembly of the molds, causing inconvenience to subsequent staff and reducing work efficiency.
[0004] In order to solve the above problems, the present application provides a molding device for aerospace propeller composite materials. Summary of the invention
[0005] The present application provides a molding device for composite materials for aerospace propellers using the following technical solutions:
[0006] A molding device for composite materials of aerospace propellers, comprising a workbench, a first electric push rod is installed on the top of the workbench, a mounting seat is connected to the telescopic end of the first electric push rod, an upper mold is connected to the bottom of the mounting seat, a mounting assembly is provided between the mounting seat and the upper mold, the mounting seat and the upper mold are connected through the mounting assembly, a cleaning assembly is provided on one side of the interior of the workbench, and a lower mold is installed at the bottom of the workbench and directly below the upper mold;
[0007] Through the above technical solution, the first electric push rod can drive the upper mold to move toward the lower mold to extrude the composite material in the lower mold.
[0008] The mounting assembly includes a fixed seat installed on the outside of the mounting seat, a screw rod is connected inside the fixed seat, a handle is installed on the top of the screw rod, a movable seat is connected outside the screw rod, connecting plates are installed on both sides of the outside of the movable seat, connecting grooves are opened on both sides of the inside of the fixed seat, a positioning column is installed on the bottom of the movable seat, a notch is opened at the bottom of the fixed seat, a mounting plate is connected inside the notch, a positioning groove is opened on the top of the mounting plate, and the positioning column and the positioning groove are a snap-fit structure.
[0009] Through the above technical solution, the screw rod is driven to rotate by the handle, and the outside of the handle is provided with anti-slip grooves.
[0010] Furthermore, the connecting plate is located inside the connecting groove and is a sliding connection structure.
[0011] Through the above technical solution, the movable seat is located in the fixed seat and moves linearly through the setting of the connecting plate and the connecting groove.
[0012] Furthermore, the cleaning assembly includes a second electric push rod installed on one side of the workbench, and a scraper is connected to the telescopic end of the second electric push rod.
[0013] Through the above technical solution, the top of the scraper and the bottom of the upper mold are in the same horizontal plane, and the scraper can scrape off the material adhered to the bottom of the upper mold.
[0014] Furthermore, a fixed box is provided on one side of the exterior of the scraper, and sliding grooves are provided on both sides of the interior of the fixed box.
[0015] Furthermore, the interior of the fixed box is connected to a storage box, and slide plates are installed on both sides of the exterior of the storage box.
[0016] Through the above technical solution, the fixed box is located on one side of the scraper, and the fixed box is lower than the scraper, so that the subsequently scraped materials can fall into the storage box.
[0017] Furthermore, the slide plate is located inside the slide groove and is a sliding connection structure, and a handle is installed on one side of the outside of the storage box.
[0018] Through the above technical solution, the storage box can be pulled out from the fixed box by the handle.
[0019] In summary, this application includes the following beneficial technical effects:
[0020] (1) After long-term use, when the upper mold needs to be disassembled for maintenance, the user only needs to hold the two handles separately to operate until the moving seat drives the positioning column to disengage from the positioning groove. When the two positioning columns are both out of the positioning groove, the user slides the upper mold out from the bottom of the mounting seat to disengage the two mounting plates from the slot position. At this time, the upper mold can be disassembled successfully; this structure facilitates the rapid installation and disassembly of the upper mold, facilitates subsequent maintenance work, brings convenience to the staff, and improves work efficiency.
[0021] (2) When the upper mold is extruded, some material may adhere to the surface of the mold. When the first electric push rod drives the upper mold to reset, the user activates the two second electric push rods to make the scraper scrape off the material adhered to the lower surface of the upper mold, and the scraped material falls into the storage box. This structure facilitates the cleaning of the material adhered to the bottom of the upper mold without the need for staff to clean it, thereby reducing the workload of staff and improving the quality of subsequent aerospace propeller molding. BRIEF DESCRIPTION OF THE DRAWINGS
[0022] Figure 1 This is a schematic diagram of the overall structure of this application;
[0023] Figure 2 This is a schematic diagram of the installation components for this application;
[0024] Figure 3 A semi-exploded diagram of the installation assembly for this application;
[0025] Figure 4 This is a semi-exploded diagram of the cleaning component of this application.
[0026] Description of the numbers in the figure:
[0027] 1. Workbench; 2. First electric push rod; 3. Mounting seat; 4. Upper mold; 5. Mounting assembly; 6. Lower mold; 7. Cleaning assembly; 51. Fixed seat; 52. Screw rod; 53. Handle; 54. Moving seat; 55. Connecting plate; 56. Connecting groove; 57. Positioning column; 58. Notch; 59. Mounting plate; 510. Positioning groove; 71. Second electric push rod; 72. Scraper; 73. Fixed box; 74. Slide; 75. Storage box; 76. Slide plate; 77. Handle. DETAILED DESCRIPTION
[0028] The technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with 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, and all other embodiments obtained by ordinary technicians in this field based on the embodiments in the present application without making creative work are within the scope of protection of the present application.
[0029] In the description of the present application, it should be noted that the terms "upper", "lower", "inner", "outer", "top / bottom" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific position, be constructed and operated in a specific position, and therefore cannot be understood as limiting the present application. In addition, the terms "first" and "second" are used for descriptive purposes only, and cannot be understood as indicating or implying relative importance.
[0030] In the description of this application, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "provided with", "set / connected", "connected", etc. should be understood in a broad sense. For example, "connected" can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.
[0031] Example:
[0032] The present application embodiment discloses a molding device for composite materials of aerospace propellers, please refer to Figure 1 , comprising a workbench 1, a first electric push rod 2 is installed on the top of the workbench 1, a mounting seat 3 is connected to the telescopic end of the first electric push rod 2, an upper mold 4 is connected to the bottom of the mounting seat 3, a mounting assembly 5 is provided between the mounting seat 3 and the upper mold 4, the mounting seat 3 and the upper mold 4 are connected through the mounting assembly 5, a cleaning assembly 7 is provided on one side of the inner part of the workbench 1, and a lower mold 6 is installed at the bottom of the workbench 1 and directly below the upper mold 4;
[0033] The first electric push rod 2 can drive the upper mold to move toward the lower mold 6 to extrude the composite material in the lower mold 6;
[0034] See also Figure 2 and Figure 3 The mounting assembly 5 includes a fixed seat 51 mounted on the outside of the mounting seat 3, a screw rod 52 is connected inside the fixed seat 51, a handle 53 is installed on the top of the screw rod 52, a movable seat 54 is connected to the outside of the screw rod 52, connecting plates 55 are installed on both sides of the outside of the movable seat 54, connecting grooves 56 are opened on both sides of the inside of the fixed seat 51, the connecting plate 55 is located inside the connecting groove 56, and is a sliding connection structure, a positioning column 57 is installed at the bottom of the movable seat 54, a notch 58 is opened at the bottom of the fixed seat 51, a mounting plate 59 is connected inside the notch 58, a positioning groove 510 is opened on the top of the mounting plate 59, and the positioning column 57 and the positioning groove 510 are a snap-fit structure;
[0035] The handle 53 protrudes from one side of the fixed seat 51, and the outer wall of the handle 53 is provided with anti-slip grooves, which is convenient for the user to rotate. The connection between the screw rod 52 and the fixed seat 51 is movably connected through a bearing. The mounting plate 59 is located at the position of the notch 58 and moves. When the positioning column 57 is located inside the positioning groove 510, the mounting plate 59 can be fixed inside the notch 58; the connection groove 56 is not connected to the notch 58, so that the movable seat 54 is located in the fixed seat 51 and moves linearly;
[0036] See also Figure 4 The cleaning assembly 7 includes a second electric push rod 71 installed on one side of the workbench 1, a scraper 72 is connected to the telescopic end of the second electric push rod 71, a fixed box 73 is provided on the outer side of the scraper 72, both sides of the fixed box 73 are provided with slide grooves 74, a storage box 75 is connected to the interior of the fixed box 73, both sides of the exterior of the storage box 75 are installed with slide plates 76, the slide plates 76 are located inside the slide grooves 74, and are a sliding connection structure, and a handle 77 is installed on the outer side of the storage box 75;
[0037] The storage box 75 can be pulled out from the interior of the fixed box 73 by the handle 77, and the storage box 75 is slidably connected to the interior of the fixed box 73 by the setting of the slide plate 76 and the slide groove 74; when the surface of the upper mold 4 is not scraped, the fixed box 73 is reset by the second electric push rod 71, which does not affect the downward movement of the upper mold 4; the fixed box 73 is located on one side of the scraper 72, and the fixed box 73 is lower than the top of the scraper 72, so that the scraped material falls into the storage box 75; the top of the scraper 72 is on the same horizontal plane as the bottom of the upper mold 4, and the scraper 72 can scrape the material adhered to the bottom of the upper mold 4.
[0038] The implementation principle of this embodiment is as follows: pouring the hot melt composite material into the lower mold 6 of the aerospace propeller model, starting the first electric push rod 2 to extrude the lower mold 6 to form the aerospace propeller;
[0039] After long-term use, when the upper mold 4 needs to be disassembled for maintenance, the user only needs to hold the two handles 53 respectively to operate, rotate the handles 53, and drive the screw rod 52 to rotate through the handles 53. At this time, the movable seat 54 is located inside the fixed seat 51 through the setting of the connecting plate 55 and the connecting groove 56, and moves linearly until the movable seat 54 drives the positioning column 57 to disengage from the positioning groove 510 opened on the top of the mounting plate 59. When the two positioning columns 57 are both out of the positioning groove 510, the user slides the upper mold 4 out from the bottom of the mounting seat 3, so that the two mounting plates 59 are out of the position of the notch 58, and the upper mold 4 can be disassembled successfully at this time.
[0040] When installing the upper mold 4, slide the mounting plates 59 mounted on both sides of the upper mold 4 into the inside of the notch 58, and then rotate the handheld handle 53. At this time, the handle 53 drives the screw rod 52 to rotate in the opposite direction, so that the movable seat 54 drives the positioning column 57 to move downward until the positioning column 57 is located in the positioning groove 510, and the upper mold 4 can be successfully installed at the bottom of the mounting seat 3.
[0041] When the upper mold 4 is extruded, some material may adhere to the surface of the mold. When the first electric push rod 2 drives the upper mold 4 to reset, the user starts the two second electric push rods 71. At this time, the telescopic ends of the two second electric push rods 71 jointly drive the scraper 72 to move forward, so that the scraper 72 scrapes off the material adhered to the lower surface of the upper mold 4. The scraped material falls into the storage box 75 connected to the fixed box 73. This structure facilitates the cleaning of the lower surface of the upper mold 4.
[0042] The above are all preferred embodiments of the present application, and the protection scope of the present application is not limited thereto. Therefore, any equivalent changes made according to the structure, shape, and principle of the present application should be included in the protection scope of the present application.
Claims
1. A molding device for composite materials of aerospace propellers, comprising a workbench (1), Features: A first electric push rod (2) is installed on the top of the workbench (1), the telescopic end of the first electric push rod (2) is connected to a mounting seat (3), the bottom of the mounting seat (3) is connected to an upper mold (4), a mounting assembly (5) is provided between the mounting seat (3) and the upper mold (4), the mounting seat (3) and the upper mold (4) are connected via the mounting assembly (5), a cleaning assembly (7) is provided on one side of the interior of the workbench (1), and a lower mold (6) is installed at the bottom of the workbench (1) and directly below the upper mold (4); The mounting assembly (5) comprises a fixed seat (51) mounted on the outside of the mounting seat (3); a screw rod (52) is connected inside the fixed seat (51); a handle (53) is mounted on the top of the screw rod (52); a movable seat (54) is connected outside the screw rod (52); connecting plates (55) are mounted on both sides of the outside of the movable seat (54); connecting grooves (56) are provided on both sides of the inside of the fixed seat (51); a positioning column (57) is mounted on the bottom of the movable seat (54); a notch (58) is provided at the bottom of the fixed seat (51); a mounting plate (59) is connected inside the notch (58); a positioning groove (510) is provided on the top of the mounting plate (59); the positioning column (57) and the positioning groove (510) are snap-fit structures.
2. A molding device for composite materials for aerospace propellers according to claim 1, Features: The connecting plate (55) is located inside the connecting groove (56) and is a sliding connection structure.
3. A molding device for composite materials for aerospace propellers according to claim 1, Features: The cleaning assembly (7) comprises a second electric push rod (71) installed on one side of the interior of the workbench (1), and a scraper (72) is connected to the telescopic end of the second electric push rod (71).
4. A molding device for composite materials for aerospace propellers according to claim 3, Features: A fixed box (73) is provided on one side of the exterior of the scraper (72), and sliding grooves (74) are provided on both sides of the interior of the fixed box (73).
5. A molding device for composite materials for aerospace propellers according to claim 4, Features: The interior of the fixed box (73) is connected to a storage box (75), and slide plates (76) are installed on both sides of the exterior of the storage box (75).
6. A molding device for composite materials for aerospace propellers according to claim 5, Features: The slide plate (76) is located inside the slide groove (74) and is a sliding connection structure. A handle (77) is installed on one side of the outside of the storage box (75).
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