Counterbalanced hinge assembly

Claim 2

In combination with a door of the type adapted to be shifted outwardly and inwardly to open and close an ingress/egress opening in a structural member during door opening and closing operations, respectively, about a generally vertical but inwardly canted hinge axis defined by a torque tube mounted in said structural member with freedom for rotation about said axis and drivingly coupled to said door by hinge link defining means, and wherein said door is required to move in an upslope direction through an angle β and thereafter in a downslope direction through an angle θ during door opening movement and upslope through an angle θ and thereafter downslope through an angle β during door closing movement as a direct result of pivotal door movement about said generally vertical inwardly canted hinge axis, the improvement in a counterbalanced hinge assembly comprising: (a) radially extending cam means non-rotatably mounted on said torque tube, said cam means defining an arcuate profiled cam face having an included angle at least equal to the sum of the angles β and θ and wherein the radius of said cam means is smallest at the juncture of said angles β and θ; and, (b) compressible/expandable energy storage means mounted on said structural member adjacent said cam means on said torque tube, said energy storage means including a first end bottomed on said structural member, a cam follower mounted on the opposite end thereof in engagement with said arcuate profiled cam face, and compressible/expandable means interposed between said first end and said cam follower for continuously biasing said cam follower into engagement with said arcuate profiled cam face; so that when said door is at the highpoint in its path of movement between fully opened and fully closed positions, said cam follower engages said arcuate profiled cam face at the juncture of said angles β and θ so that: (i) as said door moves in a downslope direction through said angle β towards a fully closed position, said torque tube and said cam means rotate through said angle β and said cam follower traverses the portion of said arcuate profiled cam face coincident with said angle β for compressing said compressible/expandable means and storing energy therein; and (ii), as said door moves in a downslope direction through said angle θ towards a fully opened position, said torque tube and said cam means rotate through said angle θ and said cam follower traverses the portion of said arcuate profiled cam face coincident with said angle θ for compressing said compressible/expandable means and storing energy therein; whereby when said door is manually shifted from either a fully closed position moving upslope through said angle β or a fully opened position moving upslope through said angle θ, said compressible/expandable means expands and the energy stored therein imparts a counterbalancing rotational torque to said torque tube through said cam follower/cam face combination for counterbalancing the hinge moment attributable to the weight of said door and minimizing the amount of manually applied torque required to move said door along said upslope paths.

Claim 3

The combination as set forth in claim 1 wherein said compressible/expandable means comprises at least one coil spring.

Claim 4

The combination as set forth in claim 1 wherein said compressible/expandable energy storage means includes a cylindrical housing closed at one end thereof and a piston slidably mounted in said housing; said compressible/expandable means comprises spring means bottomed at one end on said closed housing end and at the oppsite end on said piston; and, said cam follower is mounted on said piston.

Claim 5

The combination as set forth in claim 3 wherein said compressible/expandable spring means comprises coaxial, concentric coil springs.

Claim 6

The combination as set forth in claim 3 wherein said piston comprises an annular piston mounted on an axially extending reciprocable yoke member, and said cam follower comprises a roller journaled for rotation in said yoke member.

Claim 7

The combination as set forth in claim 4 wherein said piston comprises an annular piston mounted on an axially extending reciprocable yoke member, and said cam follower comprises a roller journaled for rotation in said yoke member.

Claim 8

The combination as set forth in claim 1 wherein said door is a plug-type aircraft door.

Claim 9

The combination as set forth in claim 1 wherein said inwardly canted hinge axis defines an acute included angle α on the order of about 10° with a vertical plane.

Claim 10

The combination as set forth in claim 1 wherein said angle β is on the order of about 123° and said angle θ is on the order of about 50°.

Claim 11

The combination as set forth in claim 1 wherein said door weighs on the order of 300 pounds.

Claim 12

The combination as set forth in claim 10 wherein the hinge moment attributable to the weight of said door ranges between about 1300 in./lbs. and about 0 in./lbs. as said fully closed door is manually moved upslope through said angle 62 and between about 1400 in./lbs. and about 0 in./lbs. as said door is manually moved upslope through said angle θ; and, wherein said counterbalanced hinge assembly reduces the amount of manually applied torque required: (i) to move said door in an upslope direction through said angle β from a maximum of about 700 in./lbs. when said door is fully closed to about 0 in./lbs.; and (ii), to move said door in an upslope direction through said angle θ from a maximum of about 400 in./lbs. when said door is fully open to about 0 in./lbs.

Claim 13

The combination as set forth in claim 1 wherein said counterbalancing rotational torque imparted to said torque tube during upslope movement of said door is non-linear and wherein the required manually generated rotational torque necessary to manually move said door along an upslope path progressively and smoothly decreases non-linearly as said door moves upslope from a fully closed or open position towards its highpoint.

Claim 14

The combination as set forth in claim 11 wherein said counterbalancing rotational torque imparted to said torque tube during upslope movement of said door is non-linear and wherein the required manually generated rotational torque necessary to manually move said door along an upslope path progressively and smoothly decreases non-linearly as said door moves upslope from a fully closed or open position towards its highpoint.

Claim 15

In combination with an aircraft plug-type door adapted to be shifted outwardly and inwardly to open and close an ingress/egress opening in the aircraft fuselage during door opening and closing operations, respectively, about a generally vertical but inwardly canted hinge axis defined by a torque tube mounted in said fuselage with freedom for rotation about said axis and drivingly coupled to said door by hinge link defining means, and wherein said door is required to move in an upslope direction through an angle β and thereafter in a downslope direction through an angle θ during door opening movement and upslope through an angle θ and thereafter downslope through an angle β during door closing movement as a direct result of pivotal door movement about said generally vertical inwardly canted hinge axis, the improvement in a counterbalanced hinge assembly comprising: (a) radially extending cam means non-rotatably mounted on said torque tube, said cam means defining an arcuate profiled cam face having an included angle at least equal to the sum of the angles β and θ and wherein the radius of said cam means is smallest at the juncture of said angles β and θ; and, (b) compressible/expandable energy storage means mounted on said aircraft fuselage adjacent said cam means on said torque tube, said energy storage means including a first end bottomed on said aircraft fuselage, a cam follower mounted on the opposite end thereof in engagement with said arcuate profiled cam face, and compressible/expandable means interposed between said first end and said cam follower for continuously biasing said cam follower into engagement with said arcuate profiled cam face; so that when said door is at the highpoint in its path of movement between fully opened and fully closed positions, said cam follower engages said arcuate profiled cam face at the juncture of said angles β and θ so that: (i) as said door moves in a downslope direction through said angle β towards a fully closed position, said torque tube and said cam means rotate through said angle β and said cam follower traverses the portion of said arcuate profiled cam face coincident with said angle β for compressing said compressible/expandable means and storing energy therein; and (ii), as said door moves in a downslope direction through said angle θ towards a fully opened position, said torque tube and said cam means rotate through said angle θ and said cam follower traverses the portion of said arcuate profiled cam face coincident with said angle θ for compressing said compressible/expandable means and storing energy therein; whereby when said door is manually shifted from either a fully closed position moving upslope through said angle β or a fully opened position moving upslope through said angle θ, said compressible/expandable means expands and the energy stored therein imparts a counterbalancing rotational torque to said torque tube through said cam follower/cam face combination for counterbalancing the hinge moment attributable to the weight of said door and minimizing the amount of manually applied torque required to move said door along said upslope paths.

Claim 16

In combination with an aircraft plug-type door adapted to be shifted outwardly and inwardly to open and close an ingress/egress opening in the aircraft fuselage during door opening and closing operations, respectively, about a generally vertical but inwardly canted hinge axis defined by a torque tube mounted in said fuselage with freedom for rotation about said axis and drivingly coupled to said door by hinge link defining means, and wherein said door is required to move in an upslope direction through an angle β and thereafter in a downslope direction through an angle θ during door opening movement and upslope through an angle θ and thereafter downslope through an angle β during door closing movement as a direct result of pivotal door movement about said generally vertical inwardly canted hinge axis, the improvement in a counterbalanced hinge assembly comprising: (a) radially extending cam means non-rotatably mounted on said torque tube, said cam means defining an arcuate profiled cam face having an included angle at least equal to the sum of the angles β and θ and wherein the radius of said cam means is smallest at the juncture of said angles β and θ; and, (b) compressible/expandable energy storage means mounted on said aircraft fuselage adjacent said cam means on said torque tube, said energy storage means including a first end bottomed on said aircraft fuselage, a cam follower mounted on the opposite end thereof in engagement with said arcuate profiled cam face, and compressible/expandable means interposed between said first end and said cam follower for continuously biasing said cam follower into engagement with said arcuate profiled cam face; so that when said door is at the highpoint in its path of movement between fully opened and fully closed positions, said cam follower engages said arcuate profiled cam face at the juncture of said angles β and θ so that: (i) as said door moves in a downslope direction through said angle β towards a fully closed position, said torque tube and said cam means rotate through said angle β and said cam follower traverses the portion of said arcuate profiled cam face coincident with said angle β for compressing said compressible/expandable means and storing energy therein; and (ii), as said door moves in a downslope direction through said angle θ towards a fully opened position, said torque tube and said cam means rotate through said angle θ and said cam follower traverses the portion of said arcuate profiled cam face coincident with said angle θ for compressing said compressible/expandable means and storing energy therein; whereby when said door is manually shifted from either a fully closed position moving upslope through said angle β or a fully opened position moving upslope through said angle θ, said compressible/expandable means expands and the energy stored therein imparts a counterbalancing rotational torque to said torque tube through said cam follower/cam face combination for counterbalancing the hinge moment attributable to the weight of said door and minimizing the amount of manually applied torque required to move said door along said upslope paths.

Claim 17

The combination as set forth in claim 14 wherein said compressible/expandable means comprises at least one coil spring.

Claim 18

The combination as set forth in claim 14 wherein said compressible/expandable energy storage means includes a cylindrical housing closed at one end thereof and a piston slidably mounted in said housing; said compressible/expandable means comprises spring means bottomed at one end on said closed housing end and at the opposite end on said piston; and, said cam follower is mounted on said piston.

Claim 19

The combination as set forth in claim 16 wherein said compressible/expandable spring means comprises coaxial, concentric coil springs.

Claim 20

The combination as set forth in claim 16 wherein said piston comprises an annular piston mounted on an axially extending reciprocable yoke member, and said cam follower comprises a roller journaled for rotation in said yoke member.

Claim 21

The combination as set forth in claim 17 wherein said piston comprises an annular piston mounted on an axially extending reciprocable yoke member, and said cam follower comprises a roller journaled for rotation in said yoke member.

Claim 22

The combination as set forth in claim 14 wherein said inwardly canted hinge axis defines an acute included angle α on the order of about 10° with a vertical plane.

Claim 23

The combination as set forth in claim 14 wherein said angle β is on the order of about 123 ° and said angle θ is on the order of about 50°.

Claim 24

The combination as set forth in claim 14 wherein said door weighs on the order of 300 pounds.

Claim 25

The combination as set forth in claim 22 wherein the hinge moment attributable to the weight of said door ranges between about 1300 in./lbs. and about 0 in./lbs. as said fully closed door is manually moved upslope through said angle β and between about 1400 in./lbs. and about 0 in./lbs. as said door is manually moved upslope through said angle θ; and, wherein said counterbalanced hinge assembly reduces the amount of manually applied torque required: (i) to move said door in an upslope direction through said angle β from a maximum of about 700 in./lbs. when said door is fully closed to about 0 in./lbs.; and (ii), to more said door in an upslope direction through said angle θ from a maximum of about 400 in./lbs. when said door is fully open to about 0 in./lbs.

Claim 26

The combination as set forth in claim 14 wherein said counterbalancing rotational torque imparted to said torque tube during upslope movement of said door is non-linear and wherein the required manually generated rotational torque necessary to manually move said door along an upslope path progressively and smoothly decreases non-linearly as said door moves upslope from a fully closed or open position towards its highpoint.

Claim 27

The combination as set forth in claim 23 wherein said counterbalancing rotational torque imparted to said torque tube during upslope movement of said door is non-linear and wherein the required manually generated rotational torque necessary to manually move said door along an upslope path progressively and smoothly decreases non-linearly as said door moves upslope from a fully closed or open position towards its highpoint.