公开(公告)号：US06394392B1

公开(公告)日：2002-05-28

申请号：US09691930

申请日：2000-10-18

申请人： Patrick A. Lafferty

发明人： Patrick A. Lafferty

IPC分类号： B64C100

CPC分类号： B64C1/10 ,  B64C1/1415 ,  B64C2001/0036 ,  B64C2001/0045 ,  B64C2001/0072 ,  B64D7/08 ,  Y02T50/12 ,  Y02T50/43

摘要： The present invention relates to an aircraft having a plurality of fuselages for increased payload. More specifically, the aircraft has a central fuselage, and first and second side-saddle fuselages mounted on opposite sides of the central fuselage. The first and second side-saddle fuselages further are provided with a mechanism for opening and each of the side-saddle fuselages define a launch tube such that each launch tube is adapted for transporting and launching a large or oversize missile.

摘要翻译： 本发明涉及具有多个用于增加有效载荷的机身的飞行器。 更具体地说，飞机具有中央机身，第一和第二侧鞍机身安装在中央机身的相对两侧。 第一和第二侧鞍机身还设置有用于打开的机构，并且每个侧鞍机身限定发射管，使得每个发射管适于传送和发射大型或超大型导弹。

公开(公告)号：US06047923A

公开(公告)日：2000-04-11

申请号：US372390

申请日：1995-01-13

申请人： Patrick A. Lafferty

发明人： Patrick A. Lafferty

IPC分类号： B64C1/00 ,  B64C1/10 ,  B64D11/00

CPC分类号： B64C1/10 ,  B64D11/00 ,  B64C2001/0036

摘要： An aircraft having a central fuselage, a first side fuselage positioned immediately adjacent to and independent of the central fuselage, and a second side fuselage positioned immediately adjacent to and independent of the central fuselage located on the opposite side of the first side fuselage is disclosed. All of the engines powering the aircraft are located either on the wings outboard of the side fuselages or in the rear of the aircraft aft of the wings. Further, the aircraft may include wings positioned laterally from both side fuselages which may be partially retracted during flight.

摘要翻译： 公开了一种具有中央机身的第一侧机身，与第一侧机身紧邻且独立于中央机身的第一机身以及紧邻第一侧机身相对侧并独立于中央机身定位的第二侧机身。 所有为飞机提供动力的发动机都位于机身外侧的机翼或机翼后方的机翼后方。 此外，飞机可以包括从两侧机身侧向设置的翼，其可以在飞行期间部分地缩回。