CN220534991U - Pre-curing forming tool for foam reinforcing rib of rotor blade - Google Patents

Pre-curing forming tool for foam reinforcing rib of rotor blade Download PDF

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Publication number
CN220534991U
CN220534991U CN202322306426.7U CN202322306426U CN220534991U CN 220534991 U CN220534991 U CN 220534991U CN 202322306426 U CN202322306426 U CN 202322306426U CN 220534991 U CN220534991 U CN 220534991U
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CN
China
Prior art keywords
frame
rotor blade
stop block
reinforcing rib
holding surface
Prior art date
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Active
Application number
CN202322306426.7U
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Chinese (zh)
Inventor
余坤
徐小艳
程翔
刘洋
张�杰
谢小梦
叶国友
陈德华
余辉
熊烺录
饶建佳
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Jiangxi Changhe Aviation Industries Co Ltd
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Jiangxi Changhe Aviation Industries Co Ltd
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Priority to CN202322306426.7U priority Critical patent/CN220534991U/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

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  • Moulding By Coating Moulds (AREA)

Abstract

The utility model relates to a pre-curing and forming tool for a foam reinforcing rib of a rotor blade, which comprises a frame, pulleys, a stop block assembly and a positioning pin; the frame is rectangular shape supporting platform, the dog subassembly is in the last holding surface of frame encloses into the solidification die cavity, the dog subassembly forms rectangular shape die cavity, just the dog subassembly is opened there is the connecting hole, the holding surface of frame is opened there is the mounting hole, through the locating pin can with the dog subassembly is fixed the holding surface of frame. The surface of the reinforcing rib is smooth and glossy after the pre-curing and forming, and the defects of glue accumulation, wrinkles and the like are avoided; the integral rigidity of the pre-cured and molded foam and the reinforcing rib assembly is improved, and the problem that the outline dimension stability of the autoclave molding C-shaped Liang Jiangshe is poor is solved.

Description

Pre-curing forming tool for foam reinforcing rib of rotor blade
Technical Field
The utility model relates to the technical field of composite material foam reinforcing rib pre-curing and forming, and particularly provides a rotor blade foam reinforcing rib pre-curing and forming tool.
Background
Autoclave molding technology is a main method for manufacturing continuous fiber reinforced thermosetting composite material parts, and is widely applied to molding of advanced composite material structures, honeycomb sandwich structures and metal or composite material glued structures. At present, the technology is firstly applied to manufacturing autonomous airfoil composite material paddles, the rotor project paddle forming tool adopts a structure of a frame type INVAL steel lower die body and a composite material upper die body, and an autoclave forming mode has the advantages of lower tool cost, shorter development period and the like. However, compared with the blade compression molding technology with higher maturity in the prior art, the scheme has the technical problems of unstable molding quality, large deviation of the external dimension of the blade and the like. Therefore, the fixture tool for pre-curing and forming the foam reinforcing rib of the rotor blade is designed, foam and the reinforcing rib can be preformed, the rigidity of the inner structure of the blade is improved, and deformation caused by uneven force transmission in the curing process of the composite material upper die body is reduced.
Disclosure of Invention
The purpose of the utility model is that: the defects of surface wrinkles, dislocation and the like of the reinforcing ribs are overcome, the rigidity of the internal structure of the blade is improved, the problem of poor stability of the external shape and the dimension of the molded C-shaped Liang Jiangshe of the autoclave is solved, and the product percent of pass is improved.
The technical scheme of the utility model is as follows:
providing a rotor blade foam reinforcing rib pre-curing forming tool, which comprises a frame 1, a pulley 2, a stop block assembly 4 and a positioning pin;
the frame is rectangular shape supporting platform, the dog subassembly is in the last holding surface of frame encloses into the solidification die cavity, the dog subassembly forms rectangular shape die cavity, just the dog subassembly is opened there is the connecting hole, the holding surface of frame is opened there is the mounting hole, through the locating pin can with the dog subassembly is fixed the holding surface of frame.
Further, the positioning pin comprises a ball pin 5 and a pin 6.
Further, the block assembly comprises a left block and a right block, and a die cavity is arranged between the left block and the right block.
Further, the frame is provided with a plurality of lightening holes.
Further, pulleys are arranged on two sides of the frame. Facilitating movement of the frame.
Further, the frame is provided with a threaded hole, and the threaded hole is used for installing curing equipment.
The process method comprises the following steps:
1. paving prepreg carbon cloth on PMI foam according to the requirement, integrally pumping a vacuum bag, vacuumizing (less than or equal to-0.8 Mpa) and curing for more than 2 hours;
2. opening a vacuum bag, and cutting the prepreg carbon cloth paved on the PMI foam according to the drawing size;
3. detaching a detachable one-side stop block assembly 4, wrapping PMI foam with a layer of isolating film, attaching the inner molded surface of the tool, and fixing the stop block assembly by using a ball pin 5 and a pin 6;
4. and (5) spreading putty strips along the edges of the stop blocks, and integrally punching a vacuum bag. Pushing the tooling into a curing furnace, vacuumizing, heating to 85+/-5 ℃ at a speed of less than or equal to 3 ℃/min, preserving heat and pressure for 1-1.5 h, cooling to room temperature immediately, and releasing pressure and discharging from the furnace;
5. opening the vacuum bag, detaching the detachable one-side stop block assembly 4, taking out the solidified foam and the reinforcing rib assembly, and cleaning the glue tumor on the surface of the reinforcing rib by using a craft knife.
The utility model has the advantages that: 1. the surface of the reinforcing rib after pre-curing molding is smooth and glossy, and the defects of glue accumulation, wrinkles and the like are avoided; 2. the integral rigidity of the pre-cured and molded foam and the reinforcing rib assembly is improved, and the problem that the outline dimension stability of the autoclave molding C-shaped Liang Jiangshe is poor is solved.
Drawings
FIG. 1 is a schematic diagram of the overall structure of a stiffening rib pre-curing and forming tool;
FIG. 2 is a partial top view of a stiffener preforming tooling;
FIG. 3 is a detailed schematic diagram of a stiffener preforming tooling;
wherein: frame 1, pulley 2, screw hole 3, dog subassembly 4, bulb round pin 5, pin 6.
Detailed Description
The disclosed examples will be described more fully with reference to the accompanying drawings, in which some, but not all of the disclosed examples are shown. Indeed, many different examples may be described and should not be construed as limited to the examples set forth herein. Rather, these examples are described so that this disclosure will be thorough and complete, and will fully convey the scope of the disclosure to those skilled in the art.
Providing a rotor blade foam reinforcing rib pre-curing forming tool, which comprises a frame 1, a pulley 2, a stop block assembly 4 and a positioning pin;
the frame is rectangular shape supporting platform, the dog subassembly is in the last holding surface of frame encloses into the solidification die cavity, the dog subassembly forms rectangular shape die cavity, just the dog subassembly is opened there is the connecting hole, the holding surface of frame is opened there is the mounting hole, through the locating pin can with the dog subassembly is fixed the holding surface of frame.
The locating pin comprises a ball stud 5 and a pin 6.
The stop block assembly comprises a left stop block and a right stop block, and a die cavity is arranged between the left stop block and the right stop block.
The frame is provided with a plurality of lightening holes.
Pulleys are arranged on two sides of the frame. Facilitating movement of the frame.
The description of the different advantageous arrangements has been presented for purposes of illustration and description, but is not intended to be exhaustive or limited to the examples in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. Additionally, the different advantageous examples may describe different advantages compared to other advantageous examples. The example or examples selected are chosen and described in order to best explain the principles of the examples, the practical application, and to enable others of ordinary skill in the art to understand the disclosure for various examples with various modifications as are suited to the particular use contemplated.

Claims (6)

1. Rotor blade foam stiffening rib pre-curing shaping frock, its characterized in that: comprises a frame, pulleys, a stop block assembly and a positioning pin;
the frame is rectangular shape supporting platform, the dog subassembly is in the last holding surface of frame encloses into the solidification die cavity, the dog subassembly forms rectangular shape die cavity, just the dog subassembly is opened there is the connecting hole, the holding surface of frame is opened there is the mounting hole, through the locating pin can with the dog subassembly is fixed the holding surface of frame.
2. The rotor blade foam rib pre-cure molding tooling of claim 1, wherein: the locating pin comprises a ball pin and a pin.
3. The rotor blade foam rib pre-cure molding tooling of claim 1, wherein: the stop block assembly comprises a left stop block and a right stop block, and a die cavity is arranged between the left stop block and the right stop block.
4. The rotor blade foam rib pre-cure molding tooling of claim 1, wherein: the frame is provided with a plurality of lightening holes.
5. The rotor blade foam rib pre-cure molding tooling of claim 1, wherein: pulleys are arranged on two sides of the frame.
6. The rotor blade foam rib pre-cure molding tooling of claim 1, wherein: the frame is provided with a threaded hole which is used for installing curing equipment.
CN202322306426.7U 2023-08-28 2023-08-28 Pre-curing forming tool for foam reinforcing rib of rotor blade Active CN220534991U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202322306426.7U CN220534991U (en) 2023-08-28 2023-08-28 Pre-curing forming tool for foam reinforcing rib of rotor blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202322306426.7U CN220534991U (en) 2023-08-28 2023-08-28 Pre-curing forming tool for foam reinforcing rib of rotor blade

Publications (1)

Publication Number Publication Date
CN220534991U true CN220534991U (en) 2024-02-27

Family

ID=89973307

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202322306426.7U Active CN220534991U (en) 2023-08-28 2023-08-28 Pre-curing forming tool for foam reinforcing rib of rotor blade

Country Status (1)

Country Link
CN (1) CN220534991U (en)

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