发明名称 |
Highly swept canard with low sweep wing supersonic aircraft configuration |
摘要 |
An aircraft, comprising a fuselage having an elongated, narrow forward portion, a main wing carried by a rear portion of the fuselage, a canard wing carried by said fuselage forward portion and having swept back leading and trailing edges tapering toward a tip or tips, the canard wing having less lifting surface than the main wing.
|
申请公布号 |
US2004140395(A1) |
申请公布日期 |
2004.07.22 |
申请号 |
US20030746744 |
申请日期 |
2003.12.23 |
申请人 |
TRACY RICHARD R.;CHASE JAMES D.;KROO ILAN |
发明人 |
TRACY RICHARD R.;CHASE JAMES D.;KROO ILAN |
分类号 |
B64C3/10;B64C3/16;B64C5/04;B64C30/00;B64C39/12;(IPC1-7):B64C3/38 |
主分类号 |
B64C3/10 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|