Gyroscopic devices

• US 5,490,420 A
• Filed: 05/06/1994
• Issued: 02/13/1996
• Est. Priority Date: 05/24/1991
• Status: Expired due to Fees

• Current Assignee: British Technology Group Ltd.
• Original Assignee: British Technology Group Ltd.
• Inventors: Burdess, James S.
• Primary Examiner(s): NOT, DEFINED
• Assistant Examiner(s): Kwok, Helen C.
• Application Number:
  US08/142,357
• Time in Patent Office: 648 Days
• Field of Search: 73/504, 73/505, 73/510, 73/577 R, 73/577 AV
• US Class Current: 73/504.02
• CPC Class Codes: G01C 19/574 the devices having two sensing masses in anti-phase motion
• CPC Class Codes: G01C 19/5755 the devices having a single sensing mass
• CPC Class Codes: Y02T 10/7072 Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors

Abstract

A gyroscopic device comprising a supporting structure (2; 104) and at least one mass (1; 50, 51; 100-103), the masses being attached to the structure by beams (3-6; 25-28; 52-63; 98-99). Masses, supporting structure and beams lie within a common plane when the device is at rest. A voltage source (V) to generates electromotive forces between such masses and structures to excite the masses into a vibratory primary motion. By simple flexure the beams can permit the masses to make limited motion relative to the structure in response to a rate of turn applied to the device, a measure of that rate being obtained from sensing that relative motion. By appropriate arrangement of the flexural connections (85-88) between the mass and the supporting structure, the device can measure rates of turn about two orthogonal axes. By connecting the supporting structure (104) to further structure (112) with additional flexural members (113) the device may be made capable of measuring rates of turn about three orthogonal axes.

Claims

1. A gyroscopic device comprising:

at least one mass having a first flat surface;

a supporting structure having a second flat surface and encompassing said at least one mass;

a plurality of beams attaching said at least one mass to said supporting structure, said plurality of beams lying within a common plane when said device is at rest, each of said plurality of beams being of elongated shape in a lengthwise direction, said plurality of beams being disposed about said at least one mass such that said first flat surface of said at least one mass is maintained parallel to said common plane and parallel to said second flat surface of said supporting structure at all times; and

electromotive power generating means within the gyroscopic device for generating electromotive forces between said at least one mass and said supporting structure to excite said at least one mass into a vibratory primary motion, said primary motion of said at least one mass flexing said plurality of beams in a manner including torsionless bending in said lengthwise direction permitting said it least one mass to make a limited secondary motion in response to a rate of turn of said device, a measure of said rate of turn being obtained from sensing a relative movement between said at least one mass and said supporting structure.

2. A gyroscopic device according to claim 1, further comprising:

a sensor sensing a deflection of at least one of said plurality of beams to obtain said measure of said rate of turn.

3. A gyroscopic device according to claim 1, further comprising:

a plurality of sensors mounted on said at least one mass and said supporting structure, respectively, said plurality of sensors sensing said relative movement between said at least one mass and said supporting structure.

4. A gyroscopic device according to claim 1, wherein:

said at least one mass includes a first mass and a second mass;

said first mass and said second mass are arranged in said gyroscopic device such that when said first mass and said second mass are excited into respective primary vibration, a first force generated by said first mass is substantially equal to and opposite from a second force generated by said second mass.

5. A gyroscopic device according to claim 1, wherein:

said plurality of beams are arranged symmetrically with respect to a pair of orthogonal axes lying within said common plane.

6. A gyroscopic device according to claim 5, further comprising:

a further supporting structure supporting said supporting structure in a manner analogous to that in which said at least one mass is supported from said supporting structure; and

said gyroscopic device providing said measure of rate of turn as a relative movement between said supporting structure and said further supporting structure.

7. A gyroscopic device according to claim 1, wherein:

said electromotive power generating means generates said electromotive forces electromagnetically.

8. A gyroscopic device according to claim 7, wherein:

said electromotive power generating means generates said electromagnetically generated electromotive forces by a non-contacting interaction between said at least one mass and said supporting structure.

9. A gyroscopic device according to claim 6, wherein:

said further supporting structure presents a third flat surface, a relative movement between said supporting structure and said further supporting structure being such that said first flat surface of said at least one mass, said second flat surface of said supporting structure, and said third flat surface of said further supporting structure all remain parallel at all times.