Semi-active vibration isolator and fine positioning mount

• US 6,029,959 A
• Filed: 01/08/1999
• Issued: 02/29/2000
• Est. Priority Date: 09/27/1996
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: TRW Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Inventors: Bronowicki, Allen J., Gran, Milton H.
• Primary Examiner(s): Oberleitner, Robert J.
• Assistant Examiner(s): Lipka, Pamela J.
• Application Number:
  US09/226,948
• Time in Patent Office: 417 Days
• Field of Search: 267/136, 267/140.14, 188/378, 188/379, 188/380, 248/550, 248/556, 248/562, 248/636, 248/638, 244/164, 244/171
• US Class Current: 267/136
• CPC Class Codes: F16F 15/005 using electro- or magnetostrictive actuation means generating of mechanical vibrations operating with electrostriction B06B1/06, with magnetostriction B06B1/08; vehicle suspension arrangements characterised by use of piezoelectric elements B60G17/01941; piezoelectric, electrostrictive and magnetostrictive devices per se H10N30/00
• CPC Class Codes: F16F 15/02 Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems F16F15/005 takes precedence ; layered products B32B; suppression of vibration in ships B63; relieving load on bearings, using magnetic means F16C39/06
• CPC Class Codes: F16F 2230/34 Flexural hinges

Abstract

A vibration isolation and precision pointing device, and a related method for its operation, for reducing vibrational disturbances on a payload platform, which is subject to vibration transmitted from a base platform and to other possible vibrational disturbances applied directly to the payload itself or to the payload platform. The invention includes a complementary combination of passive isolation and active isolation in parallel between the base and payload platforms, together with a precision positioning system that greatly reduces vibration at very low frequencies. Each isolation device, of which there are three pairs arranged to damp vibration in three axes, includes, in one embodiment, a passive spring to reduce coupling of vibration at higher frequencies and to fulfill a static load bearing function, and an active actuator element, in the form of a voice coil actuator, for applying active compensation over a selected bandwidth of frequencies below that over which passive isolation is most effective. Another disclosed form of each isolation device includes an elastic tube bendable by piezoelectric actuators and having a flexure that transmits the bending force to the payload platform along a single selected axis. In one preferred embodiment of the invention, three pairs of isolation devices are arranged on mutually orthogonal planes that intersect at the center of mass of the payload. As a result, translational vibration in the orthogonal planes is decoupled from rotation of the payload.

Claims

1. A semi-active vibration isolator, comprising:

a plurality of isolator devices connected between a first platform and a second platform which is to be isolated with respect to the first platform, wherein each of the isolator devices includes

a passive isolator element having a first end connected to the first platform and a second end connected to the second platform, wherein the passive isolator element reduces the effect of vibratory disturbances over a limited band of frequencies,

an active isolator element connected to operate in parallel with the passive isolator element, between the first and second platforms, the active isolator element having a first end connected to the first end of the passive isolator element and a second end connected to the second end of the passive isolator element, the active isolator element functioning to compensate for vibratory disturbances over a selected frequency band complementing the effect of the passive isolator element, and

a sensor attached to the isolator device for sensing internal strain or stress in the isolator due to vibratory disturbances;

a damping control circuit responsive to signals from the sensor, for generating signals to control the active isolator element in such a manner as to compensate for the vibratory disturbances; and

an angular positioning control circuit, for generating actuator control signals to correct angular positioning errors in the second platform.

2. A semi-active vibration isolator as defined in claim 1, wherein:

the vibratory disturbances occur primarily in the first platform and are reduced in the second platform.

3. A semi-active vibration isolator as defined in claim 2, wherein:

the passive isolator element is a spring providing support of static load on the second platform and providing vibration isolation at relatively high frequencies; and

the active isolator element is a voice coil actuator providing damping of resonant vibration of the spring and vibration isolation at lower frequencies.

4. A semi-active vibration isolator as defined in claim 3, wherein:

the passive isolator element provides vibration isolation at frequencies above approximately 10 Hz; and

the active isolation element provides vibration isolation at frequencies below approximately 10 Hz and down to approximately 1 Hz.

5. A semi-active vibration isolation system and fine positioning mount, comprising:

a base platform subject to vibrational disturbances;

a payload platform carrying a precision payload to be isolated from the vibrational disturbances and angularly positioned as desired;

at least three pairs of isolator-actuators connected between the base platform and the payload platform, each isolator-actuator including a force sensor, a passive isolator element having a first end connected to the base platform and a second end connected to the payload platform, and an actuator connected to operate in parallel with the passive isolator element, between the base platform and the payload platform, the actuator having first and second ends connected to the respective first and second ends of the passive isolator element;

angular position sensors for generating signals indicative of the angular position of the payload platform; and

a control system for generating actuator control signals in response to sensed vibrations and in response to differences between commanded position signals and the signals indicative of the angular position of the payload platform;

wherein each isolator-actuator provides a parallel and complementary combination of active damping and passive damping, whereby fine positioning precision is maintained even in the presence of low-frequency vibration of the base platform.

6. A semi-active vibration isolation system and fine positioning mount as defined in claim 5, wherein:

the payload platform and payload have a center of mass;

each pair of isolator-actuators has a centerline passing through the center of mass; and

translational vibration transmitted through the pairs of isolator-actuators is not converted into rotation of the payload because the vibrational forces are all applied at the center of mass.

7. A semi-active vibration isolation system and fine positioning mount as defined in claim 6, wherein:

there are three pairs of isolator-actuators; and

each pair of isolator-actuators lies in a plane and the planes of the three pairs of isolator-actuators are mutually orthogonal.

8. A method for isolating a payload platform from vibration, comprising the steps of:

connecting three pairs of vibration isolators between the payload platform and a base platform subject to vibration, each vibration isolator having an active isolation element with a first end connected to the payload platform and a second end connected to the base platform, and having a passive isolation element also with a first end connected to the payload platform and a second end connected to the base platform, wherein each passive isolation element operates in parallel with an active isolation element;

passively isolating the payload platform by using the passive isolation elements to provide isolation over a relatively high band of frequencies;

actively isolating the payload platform by using the active isolation elements to provide isolation over a relatively low band of frequencies complementing those over which the step of passively isolating is effective; and

actively positioning the payload platform to correct differences between desired position angles and sensed position angles;

whereby the last-recited step of actively positioning the payload platform also isolates the payload platform from vibration at very low frequencies.

9. A method as defined in claim 8, wherein the step of actively isolating the payload platform includes:

actuating each pair of isolators in unison to compensate for translational vibration; and

actuating the isolators in each pair independently to compensate for rotational vibration.

10. A method as defined in claim 9, and further comprising the steps of:

selecting an elemental stiffness of the isolators to provide a desired isolation frequency range for control of translational vibration; and

assigning the spacing between each pair of isolators to provide a desired isolation frequency range for control of rotational vibration.

11. A method as defined in claim 8, wherein the step of actively isolating includes:

sensing internal stress or strain in the vibration isolator;

deriving a compensating control signal from the sensed internal stress or strain in the vibration isolator; and

applying the compensating control signal to an actuator attached to the vibration isolator, wherein the compensating control signal results in damping of vibrations in the payload platform.

12. A method as defined in claim 11, and further comprising the steps of:

sensing velocity or acceleration of the payload platform caused by disturbances applied directly to the payload platform;

deriving another compensating signal from the sensed velocity or acceleration signals; and

applying the other compensating signal to the actuator, to reduce the effect of vibrational disturbances applied directly to the payload platform.