公开(公告)号：US3782220A

公开(公告)日：1974-01-01

申请号：US3782220D

申请日：1972-05-18

Applicant: BENDIX CORP

Inventor： DITLINGER R

IPC: B64C27/35 ,  F16C7/00 ,  F16F1/52 ,  F16C7/04

CPC classification number: F16C7/026 ,  F16F1/52 ,  F16F2236/12 ,  Y10T74/2142 ,  Y10T74/2144

Abstract: A laminated tie bar or coupling particularly adapted to interconnect a helicopter rotor arm and rotor blade is provided with a pair of spaced-apart end bushings interconnected by an endless belt. A pair of annular clips encircle the belt adjacent the bushings to draw opposite sides of the belt into parallel alignment. Each clip abuts an associated transverse bar or pin extending between the belt sides and attached to an adjacent end bushing by a layer of flexible strands or wires wound around the end bushing and bar or pin. The bars or pins hold the clips apart and permit twisting of the coupling about an axis extending through the end bushings.

Abstract translation: 特别适合于连接直升机转子臂和转子叶片的层压连接杆或联接器设置有由环形带相互连接的一对间隔开的端部衬套。 一对环形夹子围绕衬套附近的带子，以将带的相对侧平行排列。 每个夹子邻接在带侧面之间延伸的相关联的横向杆或销，并且通过缠绕在端部衬套和杆或销周围的柔性股线或电线层附接到相邻的端部衬套。 杆或销将夹子分开，并允许联接器围绕延伸穿过端部衬套的轴线扭转。

公开(公告)号：US3844388A

公开(公告)日：1974-10-29

申请号：US40098773

申请日：1973-09-26

Applicant: BENDIX CORP

Inventor： DITLINGER R ,  BROOKS P

IPC: F16D65/54

CPC classification number: F16D65/543

Abstract: A brake adjuster and reset device particularly adapted for multiple disc aircraft disc brakes and provided with telescoping first and second cylinder portions containing concentric first and second crushable tubular portions, respectively, the first of which crushable tubular portions is compressed axially by a piston actuated brake applying pressure plate to provide a first range of adjusted brake positions thereof and the second of which crushable tubular portions is compressed axially by the first cylinder telescoping relative to the second cylinder to provide a second range of adjusted portions of the pressure plate. A first stop member is engaged by the second cylinder portion in a brake applying direction and a spring bearing against second cylinder portion urges the same off the first stop member into engagement with a second fixed stop member spaced apart from the first fixed stop member when the brake is released to establish a predetermined brake reset or running clearance.

Abstract translation: 一种制动调节器和复位装置，特别适用于多个盘式飞机盘式制动器，并且分别设置有包含同心的第一和第二可压缩管状部分的可伸缩的第一和第二圆筒部分，其中第一个可挤压的管状部分通过活塞致动的制动施加 以提供第一范围的调节的制动位置，其中第二范围的可压缩管状部分通过第一气缸相对于第二气缸伸缩而轴向压缩，以提供压板的第二范围的调节部分。 第一止动构件在制动施加方向上被第二气缸部分接合，并且抵靠第二气缸部分的弹簧轴承将第一止动构件推向与第一固定止动构件间隔开的第二固定止动构件接合， 释放制动器以建立预定的制动复位或运行间隙。

公开(公告)号：US3768334A

公开(公告)日：1973-10-30

申请号：US3768334D

申请日：1972-06-26

Applicant: BENDIX CORP

Inventor： DITLINGER R

IPC: B64C27/35 ,  B29C53/56 ,  B29C70/56 ,  B29C70/86 ,  B64C27/32 ,  F16C7/00 ,  F16C7/04

CPC classification number: F16C7/026 ,  B29C53/564 ,  B29C70/56 ,  B29C70/86 ,  B64C27/327 ,  F16C2326/43 ,  Y10T74/2142

Abstract: A laminated tie bar or coupling particularly adapted to interconnect a helicopter rotor arm and rotor blade is provided with a pair of spaced apart end bushings interconnected by an endless belt. A pliable material interposed between the belt and each end bushing provides a bearing surface therebetween which deforms under unequal pressure or load distribution as a result of angular movement of an end bushing causing a bending moment on the belt which deformation redistributes and equalizes the pressure or load imposed on the belt.

Abstract translation: 特别适用于连接直升机转子臂和转子叶片的层压连接杆或联接器设置有由环形带相互连接的一对间隔开的端部衬套。 介于皮带和每个端部衬套之间的柔韧材料提供了一个在其间的支承表面，由于端部衬套的角度运动导致在带上的弯曲力矩的不平等压力或负荷分布下变形，该变形重新分布并使压力或负载平衡 施加在皮带上。