Torque adjusting type hinge
A torque adjusting hinge capable of easily and precisely controlling its frictional torque, being totally downsized and free from wear in its pivot pin. The hinge employs a cylindrical drive element is between the pivot pin and a sleeve-like bearing of a stationary wing and a sleeve-like bearing of a movable wing; a frictional element is disposed between a sleeve-like bearing of the stationary wing and a sleeve-like bearing of the movable wing; a swash plate-like surface formed in the cylindrical drive element is provided and abuts against a swash plate-like surface formed in the cylindrical friction element; and a nut threadably engaged with a threaded pin portion of the pivot pin when tightened, causes axial movement of the cylindrical drive element in a longitudinal direction of the pivot pin, whereby a controlled friction torque is produced between an outer peripheral surface of the cylindrical friction element and an inner peripheral surface of the sleeve-like bearing.
1. In a torque adjusting type hinge comprising: a stationary wing plate ( 1 ) fixedly mounted on a stationary frame element ( 3 ); a movable wing plate ( 5 )fixedly mounted on a wing element ( 7 ); and, a pivot pin ( 9 ), which is inserted into both sleeve-like bearing portion ( 4 ) of said stationary wing plate ( 1 ) and a sleeve-like bearing portion ( 8 ) of said movable wing plate ( 5 ) so as to rotatably connect said movable wing plate ( 5 ) with said stationary wing plate ( 1 ); the improvement wherein,
a pair of cylindrical drive element ( 14 ), each of said cylindrical drive elements ( 14 ) is radially interposed between said pivot pin ( 9 ) and at least a portion of one of said sleeve-like bearing portion ( 4 ), of said stationary wing plate ( 1 ), and a small diameter portion of each of said cylindrical drive elements ( 14 ) is radically interposed between said pivot pin ( 9 ) and at least a portion of said sleeve-like bearing portion ( 8 ) of said movable wing plate ( 5 ) in a radius direction of said pivot pin ( 9 );
a cylindrical friction element ( 15 ), is radially interposed between said pivot pin ( 9 ) and the remaining portions of said sleeve-like bearing portion ( 4 , 8 ) of said stationary wing plate and said sleeve-like bearing portion ( 8 ) of said movable wing plate ( 5 ) in a radius direction of said pivot pin ( 9 );
a swash plate-like surface ( 17 ) formed in a respective axial end portion of each of said cylindrical drive elements ( 14 ) is abutted against a swash plate-like surface ( 18 ) formed in a respective axial end portion of said cylindrical friction element ( 15 );
a nut ( 19 ), is threadably engaged with a threaded pin portion ( 12 ) formed in an end portion of said pivot pin ( 9 ), and said nut ( 19 ) is tightened to axially move each of said cylindrical drive elements ( 14 ) towards each other in a longitudinal direction of said pivot pin ( 9 ), so that said swash plate-like surfaces ( 17 , 18 ) perform a guiding operation to move said cylindrical friction element ( 15 ) radially outwardly in a radius direction of said pivot pin ( 9 ), whereby said cylindrical friction element ( 15 ) has its outer peripheral surface brought into press-contact with an inner peripheal surface of at least one of the sleeve-like bearing portions ( 4 , 8 ) causing said inner peripheral surface of said sleeve-like bearing portions ( 4 , 8 ) to produce a friction torque between said outer peripheral surface of said cylindrical friction element ( 15 ) and said inner peripheal surface, whereby said friction torque is controlled with reference to both a desired weight of and an angular position of said wing element ( 7 ).
2. In a torque adjusting type hinge comprising: a stationary wing plate ( 1 ) fixedly mounted on a stationary frame element ( 3 ); a movable wing plate ( 5 ) fixedly mounted on a wing element ( 7 ); and, a pivot pin ( 9 ), which is inserted into both a pair of sleeve-like bearing portions ( 4 ) of said stationary wing plate ( 1 ) and a sleeve-like portion ( 8 ) of said movable wing plate ( 5 ) so as to rotatably connect said movable wing plate ( 5 ) with said stationary wing plate ( 1 ); the improvement wherein,
a pair of cylindrical drive elements ( 14 ); said cylindrical drive elements ( 14 ) being radically interposed between said pivot pin ( 9 ) and each of said sleeve-like bearing portion ( 8 ) of said movable wing plate ( 5 ) in a radius direction of said pivot pin ( 9 );
a cylindrical friction element ( 15 ); said cylindrical friction element ( 15 ) is radially interposed between said pivot pin ( 9 ) and said sleeve-like bearing portion ( 8 ) of said movable wing plate ( 5 ) in a radius direction of said pivot pin ( 9 ), said cylindrical friction element ( 15 ) being axially interposed between said pair of cylindrical drive elements ( 14 ) in a longitudinal direction of said pivot pin ( 9 );
a swash plate-like surface ( 17 ) formed in one of opposite end portions of each of said cylindrical drive elements ( 14 ) is abutted against a swash plate-like surface ( 18 ) formed in each of opposite end portions of said cylindrical friction element ( 15 );
a nut ( 19 ), said nut 19 , is threadably engaged with a threaded pin portion ( 12 ) formed in an end portion of said pivot pin ( 9 ), and is tightened to axially move each of said cylindical drive elements ( 14 ) towards each other in a longitudinal direction of said pivot pin ( 9 ), so that said swash plate-like surfaces ( 17 , 18 ) perform a guiding operation to move said cylindrical friciton element ( 15 ) radically outwardly in a radius direction of said pivot pin ( 9 ), whereby said cylindrical friction element ( 15 ) has its outer peripheral surface brought into press-contact with an inner peripheal surface at least one of the sleeve-like bearing portion ( 4 , 8 ), causing said inner peripheral surface of said sleeve-like bearing portion ( 8 ) of said movable wing plate ( 5 ) to produce a friction torque between said outer peripheral surface of said cylindrical friction element ( 15 ) and said inner peripheral surface of said sleeve-like bearing portion ( 8 ) of said movable wing plate ( 5 ), wherein said friction torque of the hinge is controlled with reference to both a weight and angular position of said wing element ( 7 ).