公开(公告)号：WO0020765A9

公开(公告)日：2001-11-15

申请号：PCT/US9920876

申请日：1999-09-21

Applicant: SCALED COMPOSITES INC

Inventor： RUTAN ELBERT

IPC: B25G3/34 ,  F16B20060101 ,  F16B5/00

CPC classification number: B64C1/068 ,  B29C65/483 ,  B29C65/5042 ,  B29C65/5057 ,  B29C65/562 ,  B29C65/565 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/114 ,  B29C66/5221 ,  B29C66/532 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/73756 ,  B29C66/7392 ,  B29C66/7394 ,  B29L2031/3082 ,  B64C1/10 ,  F16B9/00 ,  F16B11/006 ,  Y10T403/472 ,  Y10T403/7073 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2277/10

Abstract: A joint structure, such as a bulkhead (22) joined to an annular shell (20), is formed by providing a conformed pattern of ridges (30, 32 & 38) and valleys (39a & 39b) on the facing portions of the elements to be joined. A tensioned band (46) is applied to the external surface of the annular shell (20) overlying one of the ridges in the annular shell (20). The tensioned band (46) stresses the joint in compression, offsetting subsequently applied shear stress so as to negate peeling failure forces. The joint loadings are sustained with a mechanical interlocking, making the use of an adhesive optional.

Abstract translation: 通过在元件的相对部分上提供隆起（30,32＆38）和谷（39a和39b）的一致的图案来形成接合结构（例如连接到环形壳体20的隔板22） 加入。 张紧带（46）被施加到覆盖在环形壳体（20）中的一个脊上的环形壳体（20）的外表面上。 张紧带（46）在压缩时对接头施加应力，随后施加剪切应力，抵消剥离破坏力。 通过机械联锁来维持联合载荷，从而可以使用粘合剂。

公开(公告)号：WO0020765A2

公开(公告)日：2000-04-13

申请号：PCT/US9920876

申请日：1999-09-21

Applicant: SCALED COMPOSITES INC

Inventor： RUTAN ELBERT

IPC: B25G3/34 ,  F16B20060101 ,  F16B5/00 ,  F16B

CPC classification number: B64C1/068 ,  B29C65/483 ,  B29C65/5042 ,  B29C65/5057 ,  B29C65/562 ,  B29C65/565 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/114 ,  B29C66/5221 ,  B29C66/532 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/73756 ,  B29C66/7392 ,  B29C66/7394 ,  B29L2031/3082 ,  B64C1/10 ,  F16B9/00 ,  F16B11/006 ,  Y10T403/472 ,  Y10T403/7073 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2277/10

Abstract: A joint structure, such as a bulkhead (22) joined to an annular shell (20), is formed by providing a conformed pattern of ridges (30, 32 & 38) and valleys (39a & 39b) on the facing portions of the elements to be joined. A tensioned band (46) is applied to the external surface of the annular shell (20) overlying one of the ridges in the annular shell (20). The tensioned band (46) stresses the joint in compression, offsetting subsequently applied shear stress so as to negate peeling failure forces. The joint loadings are sustained with a mechanical interlocking, making the use of an adhesive optional.

Abstract translation: 通过在元件的面对部分上提供适形图案的脊（30,32和38）和谷（39a和39b）来形成接合结构，例如连接到环形壳（20）的隔壁（22） 加入。 张紧带（46）施加到覆盖环形壳体（20）中的一个脊的环形壳体（20）的外表面上。 张紧带（46）使接头处于压缩状态，抵消随后施加的剪切应力，从而抵消剥离失效力。 联合装载通过机械联锁持续进行，从而可选择使用粘合剂。

公开(公告)号：WO0020273A2

公开(公告)日：2000-04-13

申请号：PCT/US9920875

申请日：1999-09-21

Applicant: SCALED COMPOSITES INC

Inventor： RUTAN ELBERT

IPC: B64C39/02 ,  B64C

CPC classification number: B64C39/02 ,  B64C2211/00

Abstract: An aircraft (20) includes a forward fuselage segment (24), an aft fuselage segment (26), a wing structure (28) supported from the aft fuselage segment, a tail structure (34) supported from either the aft fuselage segment or the wing structure, and an engine (52) supported from either the aft fuselage segment or the wing structure. A payload module (54) is disposed between and connects the forward fuselage segment and the aft fuselage segment, so as to form the structural attachment between the forward fuselage segment and the aft fuselage segment. The payload module is disconnectable from the forward fuselage segment and the aft fuselage segment such that the forward fuselage segment and the aft fuselage segment are not connected to each other when the payload module is disconnected from the forward fuselage segment and the aft fuselage segment.

Abstract translation: 飞机（20）包括前机身部分（24），后机身段（26），从后机身段支撑的机翼结构（28），尾部结构（34），其从后机身段或 机翼结构，以及从后部机身段或机翼结构支撑的发动机（52）。 有效载荷模块（54）设置在前部机身段和后部机身段之间并连接其前部机身段和后部机身段之间的结构连接。 有效载荷模块可从前机身段和后机身段断开，使得当有效载荷模块与前机身段和后机身段断开时，前机身段和后机身段都不相互连接。