Aircraft attitude display instrument

Claim 2

An attitude indicator instrument for aircraft comprising: gyroscopic first means having a spin axis which is capable of angular movement, relative to said aircraft, about a further axis, second means comprising a strip of material suitable for bearing visible markings, said strip containing perforations and being formed into a closed loop, third means for supporting, and allowing movement of, said second means, said third means defining a path around which said second means may travel, fourth means for engaging said perforations, and fifth means for coupling said fourth means with said first means such that angular movement of the spin axis relative to the aircraft causes movement of said fourth means which in turn drives the second means around its path in a direction opposite to the angular movement of the spin axis.

Claim 3

An instrument as defined in claim 1 wherein said strip of material comprises a strip of substantially flat material.

Claim 4

An instrument as defined in claim 1 or 2 wherein said fourth means comprises a plurality of teeth suitable for coupling into said perforations, and said fifth means comprises a member attached to said first means, and said teeth are located on said fifth means.

Claim 5

An instrument as defined in claim 3 wherein said fifth means comprises at least a portion of a wheel having a rim on which said teeth are located.

Claim 6

An instrument as defined in claim 1 or 2 and including a sixth means for providing a viewable reference indication indicative of a reference attitude of said aircraft about said further axis, and wherein said strip bears a viewable indication which moves with said strip and cooperates with said reference indication for indicating the attitude of said aircraft relative to said reference attitude.

Claim 7

An instrument as defined in claim 1 or 2 wherein said further axis is now designated as a second axis, and wherein said spin axis is also capable of angular movement, relative to said aircraft, about a third axis, said second and third axes being substantially perpendicular to one another.

Claim 8

An instrument as defined in claim 6 wherein angular movement of said spin axis about said second axis results from a change in aircraft pitch, and wherein angular movement of said spin axis about said third axis results from a change in aircraft roll.

Claim 9

An instrument as defined in claim 3 and including a sixth means for providing a viewable reference indication indicative of a reference attitude of said aircraft about said further axis, and wherein said strip bears a viewable indication which moves with said strip and cooperates with said reference indication for indicating the attitude of said aircraft relative to said reference attitude.

Claim 10

An instrument as defined in claim 8 wherein said further axis is now designated as a second axis, and wherein said spin axis is also capable of angular movement, relaive to said aircraft, about a third axis, said second and third axes being substantially perpendicular to one another.

Claim 11

An instrument as defined in claim 9 wherein angular movement of said spin axis about said second axis results from a change in aircraft pitch, and wherein angular movement of said spin axis about said third axis results from a change in aircraft roll.

Claim 12

A gyroscopic instrument for aircraft comprising: a gyroscope comprising (i) a gyro wheel having a vertical spin axis and (ii) pitch and roll gimbals supporting said gyro wheel and permitting both pitch and roll movement of said spin axis relative to said aircraft, a closed loop of flat tape bearing one or more viewable indications and containing a plurality of perforations, a tape carrier means for supporting said tape and defining a closed path over which the tape may travel, said tape carrier means being supported by the roll gimbal, sprocket wheel means comprising at least a portion of a wheel having sprocket teeth suitable for meshing with said perforations, said sprocket wheel means being attached to said pitch gimbal so as to drive said tape perforations and thus said tape in response to pitch movement of the spin axis.

Claim 13

A gyroscopic instrument for aircraft comprising: a gyroscope comprising (i) a gyro wheel having a vertical spin axis and (ii) pitch and roll gimbals supporting said gyro wheel and permitting both pitch and roll movement of said spin axis relative to said aircraft, a closed loop of flat tape bearing one or more viewable indications and containing a plurality of perforations, a tape carrier means for supporting said tape and defining a closed path over which the tape may travel, said tape carrier means being supported by the roll gimbal, sprocket wheel means comprising at least a portion of a wheel having sprocket teeth suitable for meshing with said perforations, said sprocket wheel means being attached to said pitch gimbal so as to drive said tape perforations and thus said tape in response to pitch movement of the spin axis.