F16M1/04

Rotary imaging system and method of rotary device and rotary device
11971129 · 2024-04-30 ·

The present invention relates to the field of rotary imaging, in particular to a rotary imaging system, a rotary imaging method and a rotary device. A rotary imaging system of a rotary device comprises a rotating body with a lamp belt module group; a circuit board installed on the rotating body, the circuit board rotating synchronously with the rotating body; an acceleration detection component installed at a predetermined position on the circuit board for acquiring acceleration detection data at the predetermined position when the circuit board rotates; and a control module used for obtaining an acceleration value of the predetermined position based on the acceleration detection data, further obtaining a rotation speed value of the circuit board based on the acceleration value and a position parameter corresponding to the predetermined position, and driving the lamp belt module group to realize rotary imaging based on the rotation speed value.

Molded housing with a reinforcement element

A molded housing for a machine includes a shaft, a first region, a second region, and a third region, a first passage for the shaft and a second passage. The first passage includes a first molded edge and the second passage includes a second molded edge. The second passage includes a reinforcement element running from a first connection point connected to the second molded edge to an opposite second connection point connected to the second molded edge. The second molded edge includes a first securing device at a third connection point and a second securing device at a fourth connection point. The second passage has an opening in a wall of the molded housing and a projection of an imaginary line connecting the third connection point to the fourth connection point into the opening intersects a projection of the reinforcement element into the opening at an acute angle.

Molded housing with a reinforcement element

A molded housing for a machine includes a shaft, a first region, a second region, and a third region, a first passage for the shaft and a second passage. The first passage includes a first molded edge and the second passage includes a second molded edge. The second passage includes a reinforcement element running from a first connection point connected to the second molded edge to an opposite second connection point connected to the second molded edge. The second molded edge includes a first securing device at a third connection point and a second securing device at a fourth connection point. The second passage has an opening in a wall of the molded housing and a projection of an imaginary line connecting the third connection point to the fourth connection point into the opening intersects a projection of the reinforcement element into the opening at an acute angle.

Elastomeric shock absorbers for gas turbine transportation

This application provides elastomeric shock absorbers for turbine transportation. Example engine mounts may include a first plate, a second plate, and an elastomeric bearing positioned between the first plate and the second plate. The engine mount may be configured to absorb or dampen vibration along an X-axis, a Y-axis, and a Z-axis of a turbine during transportation.

Elastomeric shock absorbers for gas turbine transportation

This application provides elastomeric shock absorbers for turbine transportation. Example engine mounts may include a first plate, a second plate, and an elastomeric bearing positioned between the first plate and the second plate. The engine mount may be configured to absorb or dampen vibration along an X-axis, a Y-axis, and a Z-axis of a turbine during transportation.

ROTARY ELECTRIC MACHINE STATOR AND MANUFACTURING METHOD THEREFOR
20190305614 · 2019-10-03 · ·

A rotary electric machine stator according to the present invention includes: a frame that includes: a tube portion; and a flange portion that is disposed so as to be integrated with the tube portion so as to protrude radially outward from a first axial end of the tube portion; a stator core that is configured into an annular shape, and that is fitted together with and held inside the tube portion; coils that are mounted to the stator core; and a plurality of positioning members that are mounted to the flange portion so as to be movable radially and circumferentially around an axial center of the stator core.

ROTARY ELECTRIC MACHINE STATOR AND MANUFACTURING METHOD THEREFOR
20190305614 · 2019-10-03 · ·

A rotary electric machine stator according to the present invention includes: a frame that includes: a tube portion; and a flange portion that is disposed so as to be integrated with the tube portion so as to protrude radially outward from a first axial end of the tube portion; a stator core that is configured into an annular shape, and that is fitted together with and held inside the tube portion; coils that are mounted to the stator core; and a plurality of positioning members that are mounted to the flange portion so as to be movable radially and circumferentially around an axial center of the stator core.

ASSEMBLY FOR AN AIRCRAFT ENGINE MOUNTING COMPRISING AN ARTICULATION AXIS SUPPORTED BY A YOKE JOINT AND TRANSLATIONALLY IMMOBILE
20190241272 · 2019-08-08 ·

An assembly for an aircraft engine mounting comprising an articulation axis supported by two plain bearings and a blocking device blocking the translation of the articulation axis in a direction which comprises a blocking screw that is screwed, in operation, into a first, tapped internal portion of a tubular extension secured to one of the two plain bearings, a first blocking system comprising an internal elastic stop ring housed in a groove formed in the tubular extension, and a second blocking system comprising a blocking screw which passes through first orifices passing through the second section of the blocking screw and second orifices passing through the tubular extension.

ASSEMBLY FOR AN AIRCRAFT ENGINE MOUNTING COMPRISING AN ARTICULATION AXIS SUPPORTED BY A YOKE JOINT AND TRANSLATIONALLY IMMOBILE
20190241272 · 2019-08-08 ·

An assembly for an aircraft engine mounting comprising an articulation axis supported by two plain bearings and a blocking device blocking the translation of the articulation axis in a direction which comprises a blocking screw that is screwed, in operation, into a first, tapped internal portion of a tubular extension secured to one of the two plain bearings, a first blocking system comprising an internal elastic stop ring housed in a groove formed in the tubular extension, and a second blocking system comprising a blocking screw which passes through first orifices passing through the second section of the blocking screw and second orifices passing through the tubular extension.

Mounting and aligning a vehicle side door motor within the current bill of process

A mounting assembly for a vehicle side door motor includes an upper hinge element configured for receiving a side door motor drive shaft and a motor mounting bracket configured to receive the side door motor drive shaft and to allow a radial adjustment of the drive shaft for alignment of an axis of the motor with a side door hinge axis. The upper hinge element may define a clevis including a lower clevis portion having a motor drive shaft mounting aperture dimensioned to allow the radial adjustment feature. The motor mounting bracket includes one or more mounting apertures dimensioned to allow a vehicle fore/aft adjustment and in/out adjustment of the side door motor element. The motor mounting assembly is further configured to allow a vehicle up/down adjustment of the side door motor.