Aircraft door counterbalance system

Claim 2

A counterbalance system for use with an aircraft door which is rotably mounted about a substantially horizontal axis generally located at the lower portion of the door and opens by swingly outwardly from the aircraft fuselage, said door including connection means for connecting the door to the fuselage, and which door presents a changing moment arm during movement between an opened and closed position, comprising: a varying radius pulley to be mounted on said connection means and which rotates about a substantially horizontal axis upon movement of the door between an opened and closed position; and means to apply a substantially uniform force on the periphery of said pulley to exert a moment on said pulley opposite the moment exerted by said door, to counterbalance forces imposed by the door as it is moved between an opened and closed position.

Claim 3

The counterbalance system of claim 1 wherein the means to apply a substantially uniform force on the varying radius pulley includes a spring-powered reel.

Claim 4

The counterbalance system of claim 2, which further includes: a shaft rotatably mounted within said spring-powered reel; a second pulley mounted upon said shaft; and a cable wrapped about said second pulley and attached to said varying radius pulley.

Claim 5

The counterbalance system of claim 2 wherein said spring-powered reel includes means for attaching said reel to an interior wall of an aircraft.

Claim 6

The counterbalance system of claim 1 wherein the varying radius pulley includes means for attaching said pulley to a door control arm of said door.

Claim 7

The counterbalance system of claim 2 wherein said reel is provided with a lubricant having low temperature operating characteristics.

Claim 8

In an aircraft having a door rotatably mounted in the aircraft fuselage about a substantially horizontal axis generally located at the lower portion of the door, said door including connection means for connecting the door to the fuselage, which door is adapted to swing outwardly from said fuselage about said axis to an opened position and presents a changing moment arm during movement between an opened and closed position, the improvement which comprises: a counterbalance system which includes: a varying radius pulley mounted on said connections means and which rotates about a substantially horizontal axis upon movement of the door between an opened and closed position; and a means to apply a substantially uniform force on the periphery of said pulley to exert a moment on said pulley opposite the moment exerted by said door, to counterbalance forces imposed by the door as it is moved between an opened and closed position.

Claim 9

In an aircraft having a door rotatably mounted in the aircraft fuselage about a substantially horizontal axis generally located at the lower portion of the door, said door including connection means for connecting the door to the fuselage, which door is adapted to swing outwardly from said fuselage about said axis to an opened position and presents a changing moment arm during movement between an opened and closed position, the improvement which comprises: a counterbalance system which includes: a varying radius pulley mounted on said connections means and which rotates about a substantially horizontal axis upon movement of the door between an opened and closed position; and a means to apply a substantially uniform force on the periphery of said pulley to exert a moment on said pulley opposite the moment exerted by said door, to counterbalance forces imposed by the door as it is moved between an opened and closed position.

Claim 10

The improvement of claim 7, wherein the means to apply a substantially uniform force on the varying radius pulley includes a spring-powered reel.

Claim 11

The improvement of claim 8 which further includes: a shaft rotatably mounted within said spring-powered reel; a second pulley mounted upon said shaft; and a cable wrapped about said second pulley and attached to said varying radius pulley.

Claim 12

The improvement of claim 8 wherein said spring-powered reel is attached to an interior wall of said aircraft.

Claim 13

The improvement of claim 7 wherein said varying radius pulley is attached to a door control arm of said door.

Claim 14

The improvement of claim 7 wherein said door and said varying radius pulley are mounted for rotation about a substantially horizontal axis.