Methods and Apparatuses for Decoupling a Fuselage from a Mandrel

    公开(公告)号:US20240181583A1

    公开(公告)日:2024-06-06

    申请号:US18436732

    申请日:2024-02-08

    IPC分类号: B23Q3/12 B64F5/10

    CPC分类号: B23Q3/12 B64F5/10

    摘要: In an example, a system is disclosed. The system comprises a one-piece mandrel, a fuselage coupled to the one-piece mandrel, and a strongback apparatus positioned on the fuselage. The strongback apparatus comprises an arcuate central body comprising a front end, a rear end, and a plurality of elongated members that connect the front end to the rear end, and actuators mounted to the plurality of elongated members. The actuators are configured to move in a radially outward direction from extended positions to retracted positions and comprise (i) proximal ends mounted to the plurality of elongated members and (ii) distal ends having vacuum suction cups. In the extended positions, the vacuum suction cups engage the fuselage on which the strongback apparatus is positioned. As the actuators moves from the extended positions to the retracted positions, the vacuum suction cups pull the fuselage away from the one-piece mandrel.

    Methods and apparatuses for decoupling a fuselage from a mandrel

    公开(公告)号:US11931845B2

    公开(公告)日:2024-03-19

    申请号:US17548704

    申请日:2021-12-13

    IPC分类号: B29C70/44 B23Q3/12 B64F5/10

    CPC分类号: B23Q3/12 B64F5/10

    摘要: In an example, a system is disclosed. The system comprises a one-piece mandrel, a fuselage coupled to the one-piece mandrel, and a strongback apparatus positioned on the fuselage. The strongback apparatus comprises an arcuate central body comprising a front end, a rear end, and a plurality of elongated members that connect the front end to the rear end, and actuators mounted to the plurality of elongated members. The actuators are configured to move in a radially outward direction from extended positions to retracted positions and comprise (i) proximal ends mounted to the plurality of elongated members and (ii) distal ends having vacuum suction cups. In the extended positions, the vacuum suction cups engage the fuselage on which the strongback apparatus is positioned. As the actuators moves from the extended positions to the retracted positions, the vacuum suction cups pull the fuselage away from the one-piece mandrel.

    ROTARY TOOL
    4.
    发明申请

    公开(公告)号:US20220395911A1

    公开(公告)日:2022-12-15

    申请号:US17779125

    申请日:2020-11-27

    摘要: Provided is a rotary tool with a compact tip tool holding portion (80). The rotary tool is provided with a sleeve (81) attached to an output shaft (41) to switch a tip tool (70) between a fixed state and a detachable state. The output shaft (41) has a through hole (46) formed therein radially penetrating from the inside to the outside of a mounting hole thereof. The through hole (46) has a steel ball (85) provided therein such that at least a part of the steel ball (85) overlaps at least a part of a case (10). The sleeve (81) defines a first position in the outward direction of the steel ball (85), while the case (10) regulates a second position on the radially outer side of the first position.

    Anterior Spindle Device for Use on a Machine Tool

    公开(公告)号:US20220355429A1

    公开(公告)日:2022-11-10

    申请号:US17622655

    申请日:2020-07-17

    IPC分类号: B23Q3/12 B23B37/00 B23Q11/00

    摘要: The present invention relates to an anterior spindle device for use on a machine tool, comprising a clamping interface 12 for clamping the anterior spindle device on a work spindle of the machine tool, an anterior spindle unit 14 with a spindle 14a for driving a drilling tool clamped on the spindle 14a, a drive 15 for exerting a force on the anterior spindle unit 14, and an electromagnetic actuator 16 for exerting a counterbalancing force opposite to the force of the drive 15 on the anterior spindle unit 14.

    HOLE SAW ARBOR HAVING AN ADJUSTABLE CONNECTION MECHANISM

    公开(公告)号:US20220314342A1

    公开(公告)日:2022-10-06

    申请号:US17844106

    申请日:2022-06-20

    发明人: Bryan C. Ward

    IPC分类号: B23B51/04 B23B51/12 B23Q3/12

    摘要: An arbor for a hole saw an arbor stem, an actuator, and at least one post. The arbor stem includes at least one arm having a threaded portion configured to engage the hole saw. The actuator is rotatable about a central axis of the arbor to move the at least one arm. The actuator includes a surface facing the at least one arm and a track. The track is recessed from the surface of the actuator. The at least one post extends from the at least one arm to engage the track. The arm is movable in a radial direction in response to rotation of the actuator to vary a circumference of the arbor stem.

    Assembling and centering structure for processing tool

    公开(公告)号:US11453067B2

    公开(公告)日:2022-09-27

    申请号:US16979282

    申请日:2019-03-04

    发明人: Li-Cheng Chen

    IPC分类号: B23C5/10 B23B29/12 B23Q3/12

    摘要: Disclosed is an assembling and centering structure for a processing tool, the structure having a clamping handle (10), a processing head (20), and a fastening member (30) for connecting and fixing the clamping handle (10) and the processing head (20). An end face accommodation groove (100) of the clamping handle (10) is formed with a concave part (11) and a centering hole (12). The processing head (20) is formed with a convex part (211) and a centering post (222), the convex part (211) matches the concave part (11), and the centering post (222) matches the centering hole (12). Thus, it can be ensured that after assembly, the central axis of rotation of the clamping handle (10) is in a straight line with the central axis of rotation of the processing head (20).

    Methods And Apparatuses For Decoupling A Fuselage From A Mandrel

    公开(公告)号:US20220184760A1

    公开(公告)日:2022-06-16

    申请号:US17548704

    申请日:2021-12-13

    IPC分类号: B23Q3/12 B64F5/10

    摘要: In an example, a system is disclosed. The system comprises a one-piece mandrel, a fuselage coupled to the one-piece mandrel, and a strongback apparatus positioned on the fuselage. The strongback apparatus comprises an arcuate central body comprising a front end, a rear end, and a plurality of elongated members that connect the front end to the rear end, and actuators mounted to the plurality of elongated members. The actuators are configured to move in a radially outward direction from extended positions to retracted positions and comprise (i) proximal ends mounted to the plurality of elongated members and (ii) distal ends having vacuum suction cups. In the extended positions, the vacuum suction cups engage the fuselage on which the strongback apparatus is positioned. As the actuators moves from the extended positions to the retracted positions, the vacuum suction cups pull the fuselage away from the one-piece mandrel.