Shock force compensating system

Claim 2

A shock force compensating system for flying magnetic heads comprising: a stationary base subject to shock forces, a shock absorbing means on said stationary base for delaying shock forces several milliseconds, a chassis mounted on said shock absorbing means, a rotatable magnetic storage device mounted on said chassis, a flying head mounted on said chassis opposite said rotatable magnetic storage device for movement relative to said magnetic storage device, an accelerometer mounted on said stationary base for sensing shock forces and for immediately generating a signal indicative of the magnitude of said shock force, control means connected to said accelerometer for generating a control signal indicative of the magnitude of said shock force, and transducer means responsive to said control signal for moving said flying head relative to said magnetic storage device in anticipation of said shock force being transmitted to said chassis.

Claim 3

A shock force compensating system as set forth in claim 1 wherein said transducer means further comprises fluid valve means for regulating the pneumatic pressure of a gas being supplied to said flying head, said flying head further comprising a chamber connected to said regulated gas from said fluid valve for determining the height of said flying head from said magnetic media, and pneumatic pressure supply means comprising a vacuum line and a pressure line connected to said fluid valve means.

Claim 4

A shock force compensating system as set forth in claim 2 wherein said control means further comprises means for actuating said fluid valve means to control the pressure of the gas being supplied to said chamber in said flying head.

Claim 5

A shock force compensating system as set forth in claim 3 which further includes a head support carriage mounted on said chassis for linear movement relative thereto, and a head support arm mounted on said head support carriage for flexibly supporting said flying head.

Claim 6

A shock force compensating system as set forth in claim 1 which further includes, a support carriage mounted for linear movement on said chassis, a head support arm pivotally mounted on said head support carriage for supporting said flying head, said transducer means further comprising a rotary electric motor mounted on said head support carriage and adapted to move said head support arm in response to rotary movement of said electric motor, and said control means being connected to said rotary electric motor to provide electrical signals for moving said electric motor in response to signals from said accelerometer.

Claim 7

A shock force compensating system as set forth in claim 5 wherein said electric motor comprises a high torque printed circuit motor.

Claim 8

A shock force compensating system as set forth in claim 6 wherein said printed circuit motor is provided with screw means cooperating with a threaded aperture on said head support arm.

Claim 9

A shock force compensated flying magnetic head system comprising: a stationary mounting base, shock absorbing means mounted on said stationary mounting base for absorbing and delaying transmitted shock forces several milliseconds, a chassis mounted on said shock absorbing means, magnetic media means mounted for rotational movement on said chassis, a head support carriage mounted for linear movement on said chassis, a head support arm mounted on said head support carriage for linear movement therewith, a flying head mounted on said head support arm for movement relative to said magnetic media means, an accelerometer mounted on said stationary mounting base for providing an immediate output signal indicative of the application of a shock force to said stationary mounting base, signal control means connected to the output signal of said accelerometer, pressure control means mounted on said head support carriage and actuated by said signal control means, air chamber means in said flying head means opposite said magnetic media means, and said air chamber means being connected to said pressure control means, whereby, a shock force applied to said accelerometer causes said pressure control means to raise or lower said flying head relative to said magnetic media in anticipation of said shock force being applied to said chassis.

Claim 10

A shock force compensated flying magnetic head system comprising: a stationary mounting base, shock absorbing means mounted on said stationary mounting base for absorbing and delaying transmitted shock forces several milliseconds, a chassis mounted on said shock absorbing means, magnetic media means mounted for rotational movement on said chassis, a head support carriage mounted for linear movement on said chassis, a head support arm mounted on said head support carriage for linear movement therewith, a flying head mounted on said head support arm for movement relative to said magnetic media means, an accelerometer mounted on said stationary mounting base for providing an immediate output signal indicative of the application of a shock force to said stationary mounting base, signal control means connected to the output signal of said accelerometer, pressure control means mounted on said head support carriage and actuated by said signal control means, air chamber means in said flying head means opposite said magnetic media means, and said air chamber means being connected to said pressure control means, whereby, a shock force applied to said accelerometer causes said pressure control means to raise or lower said flying head relative to said magnetic media in anticipation of said shock force being applied to said chassis.