Composite blade and method for molding composite blade
AssigneeMitsubishi Heavy Industries, Ltd.
InventorsRyoji OKABE, Masami Kamiya, Kentaro SHINDO
Life of this patent
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Abstract
A composite blade formed by laying up composite layers containing reinforcing fiber and resin, the composite blade comprising: a blade root mounted in a blade groove; an airfoil extending from the blade root to a front end side; and a metal patch mounted between the blade groove and the blade root, and bonded to the blade root.
Claims9
A composite blade formed by laying up composite layers containing reinforcing fiber and resin, the composite blade comprising:
- a blade root mounted in a blade groove;
- an airfoil extending from the blade root to a front end side;
- and
- a metal patch mounted between the blade groove and the blade root, and bonded to the blade root, wherein
- the blade root is a laminate with the laid-up composite layers and includes
- an airfoil laminate continuous from the airfoil,
- a blade root inner laminate mounted on the inner side of the airfoil laminate, and
- a blade root outer laminate mounted on the outer side of the airfoil laminate, and
- the reinforcing fiber is oriented in the blade root inner laminate and the blade root outer laminate so that a linear expansion coefficient of the blade root is approximate to a linear expansion coefficient of the metal patch.
A method for molding a composite blade formed by laying up composite layers containing reinforcing fiber and resin, wherein
- the composite blade includes
- a blade root mounted in a blade groove,
- an airfoil extending from the blade root to a front end side, and
- a metal patch mounted between the blade groove and the blade root and bonded to the blade root, and
- the blade root is a laminate with the laid-up composite layers and includes
- an airfoil laminate continuous from the airfoil,
- a blade root inner laminate mounted on the inner side of the airfoil laminate, and
- a blade root outer laminate mounted on the outer side of the airfoil laminate,
- the method comprises:
- a set process of placing the metal patch on a forming mold for molding the blade root;
- a laying-up process of laying up the composite layers on the metal patch and forming the airfoil laminate, the blade root inner laminate, and the blade root outer laminate;
- and
- a hardening process of heating and hardening the airfoil laminate, the blade root inner laminate, and the blade root outer laminate, and
- at the laying-up process, the reinforcing fiber is oriented in the blade root inner laminate and the blade root outer laminate so that a linear expansion coefficient of the blade root is approximate to a linear expansion coefficient of the metal patch.
Dependencies are inferred from the claim text.