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    • 4. 发明授权
    • Switchgear with top mounted vertical takeoff tripping and spring release
interlock
    • 开关柜具有顶部安装的垂直起飞跳闸和弹簧释放互锁
    • US5628394A
    • 1997-05-13
    • US621570
    • 1996-03-25
    • James J. BenkeFrancois MarchandJohn J. Hoegle
    • James J. BenkeFrancois MarchandJohn J. Hoegle
    • H02B11/133H01H5/00
    • H02B11/133
    • Switchgear with a closing spring release and an opening release accessible from a front face is further provided with top mounted closing and opening spring releases. In order to avoid interference with internal parts of the switchgear and to follow the movement of the trip mechanisms to which they are connected, these top mounted spring releases are flexible elongated members preferably in the form of flat stainless spring steel straps. The flat strap of the top mounted opening spring release has a slot engaging the opening trip lever and is sized so as not to engage the trip lever when the front accessible spring release is otherwise actuated. As the horizontal pivot axis of the closing spring trip lever moves transversely, the flat strap of the top mounted closing spring release is oriented to bend in the same direction while the lower end section is twisted 90.degree. to receive a coupling pin on the trip lever.
    • 具有闭合弹簧释放和从前表面接近的开口释放的开关装置还设置有顶部安装的关闭和打开弹簧释放。 为了避免干扰开关柜的内部部件并跟随其连接的脱扣机构的移动,这些顶部安装的弹簧释放件是柔性细长构件,优选地为扁平的不锈钢弹簧钢带的形式。 顶部安装的开启弹簧释放装置的平坦带具有接合开启跳闸杆的狭槽,并且其尺寸设计成当另外可操作前部可弹性释放件时不接合脱扣杆。 当闭合弹簧跳闸杆的水平枢转轴线横向移动时,顶部安装的关闭弹簧释放件的平坦带被定向成在相同方向上弯曲,同时下端部分扭转90°以接收脱扣杆上的联接销 。
    • 6. 发明申请
    • ROTOR BLADE AND AN AIRCRAFT
    • 转子叶片和飞机
    • US20130177422A1
    • 2013-07-11
    • US13534172
    • 2012-06-27
    • Laurent BianchiJacques GaffieroAlain CharreyreFrancois Marchand
    • Laurent BianchiJacques GaffieroAlain CharreyreFrancois Marchand
    • F01D5/14F01D25/00
    • F01D5/147B29D99/0028B64C11/26B64C27/48B64C2027/4736F01D25/00
    • A rotor blade (1) provided with an outer covering (2) and with at least one load take-up spar (10) associated with at least one pin-receiving bushing (3). Each spar (10) is a compartmentalized spar comprising centrifugal force take-up means (20) incorporated within a twisting stress take-up casing (30), said centrifugal force take-up means (20) comprising at least two boxes (21, 22), each having said pin-receiving bushing (3) of the spar (10) passing therethrough, each box (21, 22) including a closed retention belt (23) extending in the spanwise direction of the blade, the retention belt (23) of one box (22) surrounding the retention belt (23) of another box (21), each retention belt (23) being provided with unidirectional fibers (24) wound around said pin-receiving bushing (3), said casing (30) being provided with inclined fibers (31) presenting an angle relative to said unidirectional fibers (24).
    • 转子叶片(1)设置有外覆盖件(2)和至少一个与至少一个销接收衬套(3)相关的负载牵引翼梁(10)。 每个翼梁(10)是包括在扭转应力卷取壳体(30)内的离心力牵引装置(20)的分隔翼梁,所述离心力牵引装置(20)包括至少两个箱体 每个具有所述翼梁(10)的销接收衬套(3)穿过其中的每个箱体(21,22)包括沿所述叶片的翼展方向延伸的封闭的保持带(23),所述保持带 每个保持带(23)设置有缠绕在所述销接收衬套(3)周围的单向纤维(24),所述壳体(23)包围围绕另一箱(21)的保持带(23)的一个盒(22) 30)设置有相对于所述单向纤维(24)呈角度的倾斜纤维(31)。
    • 9. 发明授权
    • Rotor blade and an aircraft
    • 转子叶片和飞机
    • US09045986B2
    • 2015-06-02
    • US13534172
    • 2012-06-27
    • Laurent BianchiJacques GaffieroAlain CharreyreFrancois Marchand
    • Laurent BianchiJacques GaffieroAlain CharreyreFrancois Marchand
    • F01D5/14B29D99/00B64C11/26F01D25/00B64C27/473B64C27/48
    • F01D5/147B29D99/0028B64C11/26B64C27/48B64C2027/4736F01D25/00
    • A rotor blade (1) provided with an outer covering (2) and with at least one load take-up spar (10) associated with at least one pin-receiving bushing (3). Each spar (10) is a compartmentalized spar comprising centrifugal force take-up means (20) incorporated within a twisting stress take-up casing (30), said centrifugal force take-up means (20) comprising at least two boxes (21, 22), each having said pin-receiving bushing (3) of the spar (10) passing therethrough, each box (21, 22) including a closed retention belt (23) extending in the spanwise direction of the blade, the retention belt (23) of one box (22) surrounding the retention belt (23) of another box (21), each retention belt (23) being provided with unidirectional fibers (24) wound around said pin-receiving bushing (3), said casing (30) being provided with inclined fibers (31) presenting an angle relative to said unidirectional fibers (24).
    • 转子叶片(1)设置有外覆盖件(2)和至少一个与至少一个销接收衬套(3)相关的负载牵引翼梁(10)。 每个翼梁(10)是包括在扭转应力卷取壳体(30)内的离心力牵引装置(20)的分隔翼梁,所述离心力牵引装置(20)包括至少两个箱体 每个具有所述翼梁(10)的销接收衬套(3)穿过其中的每个箱体(21,22)包括沿所述叶片的翼展方向延伸的封闭的保持带(23),所述保持带 每个保持带(23)设置有缠绕在所述销接收衬套(3)周围的单向纤维(24),所述壳体(23)包围围绕另一箱(21)的保持带(23)的一个盒(22) 30)设置有相对于所述单向纤维(24)呈角度的倾斜纤维(31)。