发明名称 |
Poly-component blade for a gas turbine |
摘要 |
A lightweight, impact-resistant gas turbine blade, such as an aircraft engine fan blade, has an airfoil portion (14). The airfoil portion includes a metallic section (28) consisting essentially of metal and at least one panel section (38) not consisting essentially of metal. The metallic section extends from generally the blade root to generally the blade tip. Each panel section is an elastomeric section. Preferably, the metallic section and the at-least-one panel section only together define a generally airfoil shape. <IMAGE> |
申请公布号 |
EP0808990(A1) |
申请公布日期 |
1997.11.26 |
申请号 |
EP19970303325 |
申请日期 |
1997.05.16 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
FITZGERALD, JOHN JAMES;LIN, WENDY WEN-LING;BACHRACH, WILLIAM ELLIOT;FINN, SCOTT ROGER |
分类号 |
F01D5/14;F01D5/28;F02K3/04;F04D29/02;F04D29/32 |
主分类号 |
F01D5/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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