Low profile accelerometer

• US 4,881,408 A
• Filed: 02/16/1989
• Issued: 11/21/1989
• Est. Priority Date: 02/16/1989
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Sundstrand Data Control, Inc.
• Inventors: Hulsing, Rand H. II, Peters, Rex B., Norling, Brian L.
• Primary Examiner(s): Chapman, John
• Application Number:
  US07/313,289
• Time in Patent Office: 278 Days
• Field of Search: 73/516 R, 73/517 R, 73/517 AV, 73/651, 73/862.59, 73/DIG. 1, 73/DIG. 4, 310/329
• US Class Current: 73/514.12
• CPC Class Codes: G01P 15/097 by vibratory elements
• CPC Class Codes: G01P 2015/0828 the mass being of the paddle type being suspended at one of its longitudinal ends

Abstract

A compact, low g range accelerometer comprising a support (22), a proof mass (20), flexures (24, 26) for mounting the proof mass to the support, and a force sensing element (40). The proof mass has a single rotational degree of freedom about a hinge axis (H) perpendicular to the accelerometer'"'"'s sensitive axis (S). The force sensing element is positioned along a line that is normal to the hinge axis and that lies in a plane that is normal to the hinge axis and that passes through the center of gravity (46) of the proof mass. The perpendicular distance between the hinge axis and the force sensing element is less than the distance between the hinge axis and the center of the proof mass. The force sensing element may be parallel to the pendulous axis, to produce an extremely compact accelerometer, or may be oriented at an acute angle with respect to the pendulous axis, such that the line along which the force sensing element is positioned passes through the center of percussion of the proof mass.

Claims

1. An accelerometer for measuring acceleration along a sensitive axis, the accelerometer comprising:

a support;

a proof mass, the proof mass and the support having a coefficient of thermal expansion different from the coefficient of thermal expansion of crystalline quartz;

mounting means for mounting the proof mass to the support such that the proof mass has a rotational degree of freedom about a hinge axis perpendicular to the sensitive axis;

force sensing means comprising one or more force sensing elements, each force sensing element comprising a vibrating beam transducer having a beam consisting essentially of crystalline quartz, each force sensing element being connected between the proof mass and the support, each force sensing element being positioned along a line that is parallel to a pendulous axis defined as an axis normal to the hinge axis and passing through the hinge axis and the center of mass of the proof mass, the force sensing means being symmetrically positioned with respect to a plane that is normal to the hinge axis and that passes through the center of mass of the proof mass, all force sensing elements being connected between the proof mass and support such that rotation of the proof mass in a given direction about the hinge axis puts all force sensing elements in tension or all forces sensing elements in compression, the force sensing means and the mounting means being the only constraints on rotation of the proof mass about the hinge axis; and

the perpendicular distance between the hinge axis and each line being less than the distance between the hinge axis and the center of mass of the proof mass.

2. The accelerometer of claim 1, wherein the force sensing means comprises only a single force sensing element, the force sensing element lying in said plane.

3. The accelerometer of claim 2, wherein the mounting means comprises a circular arc flexure having a profile defining a portion of a circle, and wherein the force sensing element is positioned approximately as a diameter of said circle.

4. The accelerometer of claim 3, wherein the force sensing element comprises a quartz crystal in the form of a double ended tuning fork.

5. The accelerometer of claim 1, wherein the proof mass has upper and lower proof mass surfaces that are substantially normal to the sensitive axis, and wherein the support further comprises upper and lower plates positioned on opposite sides of the proof mass adjacent to but spaced apart from the respective upper and lower surfaces by gaps, the gaps being dimensioned such that the upper and lower plates function to form damping gaps and to restrict the travel of the proof mass to prevent breakage of the force sensing elements under an overload.

6. The accelerometer of claim 1, wherein the support and proof mass comprise beryllium-copper.

7. An accelerometer for measuring acceleration along a sensitive axis, the accelerometer comprising:

a support;

a proof mass;

mounting means for mounting the proof mass to the support such that the proof mass has a rotational degree of freedom about a hinge axis perpendicular to the sensitive axis;

force sensing means comprising a force sensing element connected between the proof mass and the support, the force sensing element being positioned along aline that lies in a plane that is normal to the hinge axis and that passes through the center of mass of the proof mass, the line, when extended, passing through the center of percussion of the proof mass and forming an acute angle with a pendulous axis defined as an axis lying in said plane and passing through the hinge axis and the center of mass of the proof mass; and

the perpendicular distance between the hinge axis and said line being less than the distance between the hinge axis and the center of mass of the proof mass.