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Rotor wing prefabricated part, self-rotating rotor wing and forming method

A molding method and technology for prefabricated parts, which are applied in the field of rotor prefabricated parts and their forming, autogyrocopter, and autorotator forming fields, can solve the problems of increasing the mass of the rotor, reducing the reliability of the force transmission performance, affecting the strength of the rotor, etc. The effect of reducing production cost, excellent integrity, and ensuring balance

Pending Publication Date: 2021-12-28
ANHUI YUNYI AVIATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The rotor of the autogyro is generally made into prefabricated parts or filler blocks in advance, and then the subsequent molding is carried out. Specifically, the traditional rotor blade is made of uncured parts such as skins and girder belts and cured parts. The rotor prefabricated parts, counterweights, blade root caps, dynamic balance lead pipes and foam fillers are put into the mould, heated and pressurized for one-time molding. Although this method reduces the number of parts of the rotor blade and improves the molding efficiency , but the integrity of its structure is still not good, especially after a long flight, due to the poor integrity, the reliability of force transmission performance is reduced, which affects the balance and stability of the autogyro
[0005] In view of the above problems, in the production process of the rotor, the adhesive film is generally used to improve the integrity and tightness of the autorotating rotor. However, the use of the film has many disadvantages: first, it increases the production cost; second, it affects the quality of the rotor. The quality control of the raw materials in the rotor is related to the quality of the blade molding, so it is necessary to strictly control the quality of the raw materials. Quality, if the quality of other raw materials remains unchanged, increasing the film will increase the mass of the rotor, which will affect the flying height and speed of the autogyro; if the quality of the rotor is strictly controlled, increasing the film will reduce the quality of other raw materials , will inevitably affect the strength of the rotor and reduce the fatigue life of the rotor; the third is that the autogyro generally requires a flight altitude of about 100-5000m, and the commonly used flight altitude is 3000-5000m. The membrane is prone to brittle cracks, which affects the balance and stability of the rotor

Method used

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  • Rotor wing prefabricated part, self-rotating rotor wing and forming method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0049] Preparation of rotor preforms

[0050] Calculate the quality of the required prepreg according to the volume of the mold and the density of the glass fiber prepreg, take out the epoxy chopped fiber mixture (DS3233 toughened prepreg) from the cold storage at -18°C, and place it for more than 6 hours , after reaching the ambient temperature, open the packaging bag, take out the glass fiber prepreg, the epoxy resin content in the glass fiber prepreg is 35%;

[0051] Soften the glass fiber prepreg at a temperature of 80°C for 8 minutes;

[0052] Quickly fill the softened glass fiber prepreg into the required mold, compact it manually, then lock the mold up and down with screws or positioning pins, and put it on a hydraulic press for molding. Under the pressure of 10MPa, the temperature Set at 55°C, when the upper and lower molds of the hydraulic press rise to 75°C, heat and hold pressure for 30 minutes, after forging and pressing, take out the mold; cool to room temperat...

Embodiment 2

[0056] Preparation of rotor preforms

[0057] Calculate the quality of the required prepreg according to the volume of the mold and the density of the glass fiber prepreg, take out the epoxy chopped fiber mixture (DS3233 toughened prepreg) from the cold storage at -18°C, and place it for more than 6 hours , after reaching the ambient temperature, open the packaging bag, take out the glass fiber prepreg, the epoxy resin content in the glass fiber prepreg is 40%;

[0058] Soften the glass fiber prepreg at a temperature of 70°C for 7 minutes;

[0059] Quickly fill the softened glass fiber prepreg into the required mold, compact it manually, then lock the mold up and down with screws or positioning pins, and put it on a hydraulic press for molding. Under the pressure of 7MPa, the temperature Set at 70°C, when the upper and lower molds of the hydraulic press rise to 75°C, heat and hold pressure for 40 minutes, after forging and pressing, take out the mold; cool down to room temp...

Embodiment 3

[0063] Preparation of rotor preforms

[0064] Calculate the quality of the required prepreg according to the volume of the mold and the density of the glass fiber prepreg, take out the epoxy chopped fiber mixture (DS3233 toughened prepreg) from the cold storage at -18°C, and place it for more than 6 hours , after reaching the ambient temperature, open the packaging bag, take out the glass fiber prepreg, the epoxy resin content in the glass fiber prepreg is 50%;

[0065] Soften the glass fiber prepreg at a temperature of 90°C for 5 minutes;

[0066] Quickly fill the softened glass fiber prepreg into the required mold, compact it manually, then lock the mold up and down with screws or positioning pins, and put it on a hydraulic press for molding. Under the pressure of 2MPa, the temperature Set at 50°C, when the upper and lower molds of the hydraulic press rise to 80°C, heat and hold pressure for 60 minutes, after forging and pressing, take out the mold; cool down to room temp...

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Abstract

The invention discloses a rotor wing prefabricated part, a self-rotating rotor wing and a forming method. The forming method of the rotor wing prefabricated part comprises the following steps that glass fiber prepreg is provided; the glass fiber prepreg is softened to obtain a prepreg softened material; and a mold is filled with the prepreg softened material, the prepreg softened material is semi-cured and formed, and the rotor wing prefabricated part is obtained. By obtaining the rotor wing prefabricated part made of a semi-cured-body glass fiber composite material, in the the following process of forming the rotor wing prefabricated part with a skin, a girder belt and other parts to obtain the self-rotating rotor wing, the obtained self-rotating rotor wing has excellent integrity, centrifugal loads can be well transmitted in the working process, and therefore the balance, the stability, the strength and the service life of the self-rotating rotor wing are remarkably improved.

Description

technical field [0001] The invention belongs to the technical field of autorotors, and in particular relates to a rotor prefabricated part and a forming method thereof, and also relates to an autorotor comprising the rotor prefabricated part and a forming method of the autorotor. Background technique [0002] Autogyro, referred to as autogyro, is a kind of rotorcraft, between airplanes and helicopters. Its design varies, but most of the basic elements of the design are the same, usually including: fuselage, power plant, rotor system, empennage and landing gear five parts. When the autogyro works, the tail rotor is generally used to provide power to advance, and the tail rudder is used to control the direction. Its rotor is not driven by a power device, and it only relies on the relative airflow when it advances to blow the rotor to rotate to generate lift. [0003] Among them, the rotor is an important part that provides the necessary lift and control ability for autogyro f...

Claims

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Application Information

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IPC IPC(8): B29C70/46B29C70/54B64C27/32
CPCB29C70/46B29C70/54B64C27/32
Inventor 于天池刘曼莉
Owner ANHUI YUNYI AVIATION TECH CO LTD
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