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
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