Japanese Patent JPS499782

B1

1,219,165. Measuring gravitational field gradient electrically. HUGHES AIRCRAFT CO. Oct.29, 1968 [Feb. 2, 1968], No.51181/68. Heading G1N. Apparatus for measuring static gravitational field gradient is as described in Specification 1,105,491 but a modification of the sensor head, employing two mass dipoles and a single strainsensitive transducer, is described. A torsionally resonant gravity gradient sensor head 10 comprises two orthogonally disposed mass dipoles 11 and 13 formed by arms 23, each supporting masses, 21, at either end. The arms are connected at their centres by a torsionally flexible spring member 19, attached to which is a strain-sensitive transducer 25. In use the head is rotated at a constant angular velocity by a servo loop 57-67, the velocity feedback signal from photo-electric detector 61 being employed also as a frequency and phase reference in the detector 73. The gravitational field induces forces in the dipoles at harmonics of the rotation frequency the sensor head being made resorant at one of the harmonic frequencies, the second in the embodiments described. The second harmonic frequency i.e. the resonant frequency of the sensor, then produces from the transducer 25 and output signal which is proportional in amplitude and of similar phase sense to the magnitude and direction of a corresponding gravitational field gradient, frequency selection being aided by a resonant circuit, tuned to the second harmonic, arranged in parallel with a low-noise preamplifier 51. The output signal is transmitted to the detector 73 by an FM link 53, 69, 71. The transducer may be a Piezo-electric crystal, or a capacitive or magneto-strictive type. In an alternative sensor construction Fig. 3 (not shown) a non-metallic flexible spring member (191) comprises two spaced cylinders (101, 103) carrying respective sleeves (105, 107) between which are connected two flexible links (109) (one only shown). A strain sensitive transducer (251) is attached to one of the links. A third embodiment Fig. 5 (not shown) employs a sensor housing (203) which rotates with the head (101) thus giving windage reduction and electrostatic and electromagnetic shielding. The mass dipoles (111, 131) are supported by two torsional support springs (201), the inevtia of a dipole being matched to the resonant frequency of its associated spring so that in use a given torque produces equal dipole deflections which therefore cancel out. The housing is coupled to a rotor shaft (205) in a bearing 207 and bearing cup (209), rotation being from a motor assembly (671) comprising a rotor (211) on the other end of the shaft (205) in a stator (213). Low noise bearings e.g. air or magnetic types are used. Some mathematical analysis is given and it is shown that for an exemplory sensor a gravitational gradient of about 10-11 sec-2 may be detected.

JP7966368A

March 06, 1974

November 02, 1968

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G01V7/00; G01L5/00; G01V7/10

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