Mapping apparatus employing two input axis gyroscopic means

Claim 2

In mapping apparatus, the combination comprising: (a) a gyroscope and a carrier frame therefor, and primary means including a housing supporting the gyroscope and carrier frame for lengthwise travel along a travel axis extending lengthwise of a bore hole, (b) the gyroscope characterized as having a spinning rotor and torsion structure defining a gimbal, and wherein the rotor spin frequency has a predetermined relation to a resonant frequency of said structure, (c) the gyroscope further characterized as having two input axes, and an output axis about which the spin rotor rotates, said output axis extending generally in the direction of said travel axis, (d) drive means operatively connected with said frame to rotate the frame about one of said axes, and (e) the gyroscope having means to detect rotor pivoting about one of said two input axes in response to said rotation of the frame.

Claim 3

The combination of claim 1 wherein the gyroscope frame is rotated about said output axis by the drive means.

Claim 4

The combination of claim 1 wherein the gyroscope frame is rotated about one of said input axes by the drive means.

Claim 5

The combination of claim 1 wherein said two input axes extend generally normal to said one axis,.

Claim 6

The combination of claim 1 wherein the gyroscope includes torque motor means and the rotor includes armature means to magnetically interact with said means to block gimbaling about the other of said two input axes.

Claim 7

The combination of claim 5 wherein said housing also supports and contains said drive means which comprises a drive motor.

Claim 8

The combination of claim 1 wherein said means to detect rotor pivoting includes circuitry for producing an output which varies as a function of azimuth orientation of said output axis relative to the earth's spin axis.

Claim 9

The combination of claim 1 including a tilt sensing device associated with the gyroscope to be rotated in conjunction with said rotation of the gyroscope carrier frame, and to produce an output which varies as a function of said rotation of the gyroscope carrier frame and of tilt thereof from vertical.

Claim 10

The combination of claim 7 including a tilt sensing device associated with the gyroscope to be rotated in conjunction with said rotation of the gyroscope carrier frame, and to produce an output which varies as a function of said rotation of the gyroscope carrier frame and of tilt thereof from vertical.

Claim 11

The combination of claim 5 wherein said housing is suspended within a bore-hole in the earth to be traveled lengthwise of said hole.

Claim 12

The combination of claim 1 wherein the gyroscope includes a motor to rotate the spinning rotor, and said torsion structure includes mutually orthogonally extending primary and secondary torsion members through which rotation is transmitted from the motor to the rotor, said primary and secondary members defining said two input axes.

Claim 13

In mapping apparatus, the combination comprising (a) a first gyroscope and a first frame therefor, and a second gyroscope and a second frame therefor, (b) each of the two gyroscopes characterized as having a spinning rotor and torsion structure defining a gimbal, and wherein the rotor spin frequency has a predetermined relation to a resonant frequency of such structure, (c) each gyroscope further characterized having two input axes and an output axis about which the spin rotor rotates, said axes orthogonally related, (d) drive means operatively connected with the gyroscope frames to rotate the frames about axes which are orthogonally related relative to the gyroscopes, the output axis of the first gyroscope extending orthogonally relative to the output axis of the second gyroscope, (e) each gyroscope having means to detect rotor pivoting about one of said two input axes in response to said rotation of the gyroscope frame.

Claim 14

In mapping apparatus, the combination comprising (a) a first gyroscope and a first frame therefor, and a second gyroscope and a second frame therefor, (b) each of the two gyroscopes characterized as having a spinning rotor and torsion structure defining a gimbal, and wherein the rotor spin frequency has a predetermined relation to a resonant frequency of such structure, (c) each gyroscope further characterized having two input axes and an output axis about which the spin rotor rotates, said axes orthogonally related, (d) drive means operatively connected with the gyroscope frames to rotate the frames about axes which are orthogonally related relative to the gyroscopes, the output axis of the first gyroscope extending orthogonally relative to the output axis of the second gyroscope, (e) each gyroscope having means to detect rotor pivoting about one of said two input axes in response to said rotation of the gyroscope frame.

Claim 15

The combination of claim 12 wherein said frames of the two gyroscope are interconnected to be simultaneously rotated about the same axis by the drive means.

Claim 16

The combination of claim 12 wherein each gyroscope includes a motor to rotate the spinning rotor, and said torsion structure includes mutually orthogonally extending primary and secondary torsion members through which rotation is transmitted from the motor to the rotor, said primary and secondary torsion members defining said two input axes.

Claim 17

The combination of claim 12 including primary means supporting the gyroscopes and carrier frames for lengthwise travel along a travel axis which is parallel to said one axis.

Claim 18

The combination of claim 15 wherein said primary means includes a housing supporting and containing said gyroscopes and carrier frames, and each gyroscope includes means to block gimballing about the other of said two input axes.

Claim 19

The combination of claim 16 wherein said housing also supports and contains said drive means which comprises a drive motor.

Claim 20

The combination of claim 12 wherein said means to detect rotor pivoting includes circuitry for producing an output which varies as a function of azimuth orientation of said output axis relative to the earth's spin axis.

Claim 21

The combination of claim 1 including tilt sensing apparatus associated with the gyroscopes to be rotated in conjunction with said rotation of the gyroscope carrier frames, and to produce an output which varies as a function of said rotation of the gyroscope carrier frames and of tilt thereof from vertical.

Claim 22

The combination of claim 18 including a tilt sensing device associated with the gyroscope to be rotated in conjunction with said rotation of the gyroscope carrier frame, and to produce an output which varies as a function of said rotation of the gyroscope carrier frame and of tilt thereof from vertical.

Claim 23

The apparatus of claim 20 wherein said tilt sensing apparatus includes two tilt sensing devices arranged to sense tilt about respective orthogonal axes.

Claim 24

The combination of claim 16 wherein said housing is suspended within a bore-hole in the earth to be traveled lengthwise of said hole.

Claim 25

In the method of mapping a remote zone, the steps that include: (a) suspending at said zone a gyroscope and a housing therefor, the gyroscope characterized as having a spinning rotor and torsion structure defining a gimbal, the rotor spin frequency having a predetermined relation to a resonant frequency of said structure, the housing having a travel axis, (b) the gyroscope further characterized as having two input axes and an output axis about which the spin rotor rotates, the gyroscope also having a carrier frame, said suspending carried out to locate said output axis in the generaly direction of said travel axis, (c) rotating the carrier frame about said output axis, and (d) detecting rotor pivoting about one of said two input axes in response to said rotation of the frame to produce a signal as a function of azimuth orientation of said output axis relative to the earth's spin axis.

Claim 26

In the method of mapping a remote zone, the steps that include: (a) suspending at said zone a gyroscope and a housing therefor, the gyroscope characterized as having a spinning rotor and torsion structure defining a gimbal, the rotor spin frequency having a predetermined relation to a resonant frequency of said structure, the housing having a travel axis, (b) the gyroscope further characterized as having two input axes and an output axis about which the spin rotor rotates, the gyroscope also having a carrier frame, said suspending carried out to locate said output axis in the generaly direction of said travel axis, (c) rotating the carrier frame about said output axis, and (d) detecting rotor pivoting about one of said two input axes in response to said rotation of the frame to produce a signal as a function of azimuth orientation of said output axis relative to the earth's spin axis.

Claim 27

The method of claim 23 including also suspending at said zone a tilt sensing device and rotating said device in conjunction with said rotation of the gyroscope carrier frame thereby to produce signals indicative of degree of tilt of said zone from vertical.

Claim 28

The method of claim 24 wherein said zone is located in a bore-hole, and including the step of intermittently traveling said housing, said gyroscope and said tilt sensitive device lengthwise of said bore-hole, and to different of said zones therein.

Claim 31

The method of claim 26 wherein said rotation of the carrier frames is carried out simultaneously and at the same angular rate, and also about a common axis of rotation.

Claim 32

The method of claim 27 wherein said detection is carried out to produce, for each gyroscope, a signal as a function of azimuth orientation of the gyroscope output axis relative to the earth's spin axis, and including also suspending at said zone a tilt sensitive apparatus and rotating said apparatus in conjunction with said rotation of the gyroscope frames thereby to produce signals indicative of degree of tilt of said zone from vertical.

Claim 33

The method of claim 23 including substantially blocking rotor pivoting about the other of said input axes during said rotor pivoting about the one input axis.

Claim 34

The method of claim 26 including, for each gyroscope, substantially blocking rotor pivoting about the other of said input axes during said rotor pivoting about the one input axis.

Claim 35

The combination of claim 11 wherein the gyroscope includes means to effect blocking of rotor pivoting about the other of said input axes during said rotor pivoting about said one input axis.

Claim 36

The combination of claim 14 wherein each gyroscope includes means to effect blocking of rotor pivoting about the other of said input axes during said rotor pivoting about said one input axis.

Claim 37

In mapping apparatus, the combination comprising (a) a first gyroscope and a first frame therefor, and a second gyroscope and a second frame therefor, (b) each of the two gyroscopes characterized as having a spinning rotor and a gimbal, (c) each gyroscope further characterized having two input axes and an output axis about which the spin rotor rotates, said axes orthogonally related, (d) drive means operatively connected with the gyroscope frames to simultaneously rotate each frame about one of said axes, the output axis of the first gyroscope extending parallel to said one axis, and the output axis of the second gyroscope extending normal to said one axis, (e) each gyroscope having means to detect rotor pivoting about one of said two input axes in response to said rotation of the gyroscope frame.

Claim 38

In mapping apparatus, the combination comprising (a) a first gyroscope and a first frame therefor, and a second gyroscope and a second frame therefor, (b) each of the two gyroscopes characterized as having a spinning rotor and a gimbal, (c) each gyroscope further characterized having two input axes and an output axis about which the spin rotor rotates, said axes orthogonally related, (d) drive means operatively connected with the gyroscope frames to simultaneously rotate each frame about one of said axes, the output axis of the first gyroscope extending parallel to said one axis, and the output axis of the second gyroscope extending normal to said one axis, (e) each gyroscope having means to detect rotor pivoting about one of said two input axes in response to said rotation of the gyroscope frame.

Claim 39

The combination of claim 33 wherein said frames of the two gyroscopes are interconnected to be simultaneously rotated about said one axis by the drive means, a housing for said gyroscopes and drive means, and means to travel said housing lengthwise in a bore-hole.

Claim 40

In mapping apparatus, the combination comprising (a) a first gyroscope and a first frame therefor, and a second gyroscope and a second frame therefor, (b) each of the two gyroscopes characterized as having a spinning rotor and a gimbal, (c) each gyroscope further characterized having two input axes and an output axis about which the spin rotor rotates, said axes orthogonally related, (d) drive means operatively connected with the gyroscope frames to simultaneously rotate each frame about one of said axis, the output axis of the first gyroscope having a component extending parallel to said one axis, and the output axis of the second gyroscope having a component extending normal to said one axis, (e) such gyroscope having means to detect rotor pivoting about one of said two input axes in response to said rotation of the gyroscope frame.

Claim 41

In mapping apparatus, the combination comprising (a) a first gyroscope and a first frame therefor, and a second gyroscope and a second frame therefor, (b) each of the two gyroscopes characterized as having a spinning rotor and a gimbal, (c) each gyroscope further characterized having two input axes and an output axis about which the spin rotor rotates, said axes orthogonally related, (d) drive means operatively connected with the gyroscope frames to simultaneously rotate each frame about one of said axis, the output axis of the first gyroscope having a component extending parallel to said one axis, and the output axis of the second gyroscope having a component extending normal to said one axis, (e) such gyroscope having means to detect rotor pivoting about one of said two input axes in response to said rotation of the gyroscope frame.

Claim 42

The combination of claim 35 wherein said frames of the two gyroscopes are interconnected to be simultaneously rotated about said one axis by the drive means, a housing for said gyroscopes and drive means, and means to travel said housing lengthwise in a bore-hole.

Claim 43

In mapping apparatus, the combination comprising: (a) a gyroscope and a carrier frame therefor, and a housing for said gyroscope and carrier frame, the housing adapted to be suspended in a bore hole for lengthwise travel therealong, (b) the gyroscope characterized as having a spinning rotor and torsion structure defining a gimbal, and wherein the rotor spin frequency has a predetermined relation to a resonant frequency of said structure, (c) the gyroscope further characterized as having two input axes, and an output axis about which the spin rotor rotates, (d) drive means operatively connected with said frame to rotate the frame about one of said axes, (e) the gyroscope having means to detect rotor pivoting about one of said two input axes in response to said rotation of the frame, (f) the gyroscope including a motor to rotate the spinning rotor and said torsion structure including mutually orthogonally extending primary and secondary torsion members through which rotation is transmitted from the motor to the rotor, said primary and secondary members defining said two input axes, (g) the gyroscope including means to block gimbaling about the other of said input axes.

Claim 44

In mapping apparatus, the combination comprising: (a) a gyroscope and a carrier frame therefor, and a housing for said gyroscope and carrier frame, the housing adapted to be suspended in a bore hole for lengthwise travel therealong, (b) the gyroscope characterized as having a spinning rotor and torsion structure defining a gimbal, and wherein the rotor spin frequency has a predetermined relation to a resonant frequency of said structure, (c) the gyroscope further characterized as having two input axes, and an output axis about which the spin rotor rotates, (d) drive means operatively connected with said frame to rotate the frame about one of said axes, (e) the gyroscope having means to detect rotor pivoting about one of said two input axes in response to said rotation of the frame, (f) the gyroscope including a motor to rotate the spinning rotor and said torsion structure including mutually orthogonally extending primary and secondary torsion members through which rotation is transmitted from the motor to the rotor, said primary and secondary members defining said two input axes, (g) the gyroscope including means to block gimbaling about the other of said input axes.