Claims
- 1. Method of making a high stability quartz crystal oscillator from a quartz crystal plate, said method including the steps of
- (A) cutting the quartz crystal plate at the angles that result in a resonator having a turnover temperature below the lowest operating temperature of the equipment in which the oscillator is to be used,
- (B) fabricating a resonator from the cut quartz crystal plate,
- (C) connecting the resonator into a high stability oscillator circuit, and
- (D) placing the oscillator-circuit/resonator combination into a temperature controlled environment wherein the temperature is maintained at below the lowest operating temperature of the equipment in which the oscillator is to be used.
- 2. Method according to claim 1 wherein the quartz crystal resonator is an SC cut resonator with angles of cut of .phi.=21.degree.56' and .sigma.=35.degree.43' and a turnover temperature of -65.degree. C.
- 3. Method according to claim 1 wherein the temperature controlled environment is maintained by a small refrigerated enclosure.
- 4. Method according to claim 3 wherein the small refrigerated enclosure is a closed cyle refrigerator.
- 5. Method according to claim 3 wherein the small refrigerated enclosure is a thermoelectrically cooled refrigerator.
- 6. Method according to claim 1 wherein the low temperature can be obtained in a space vehicle by placing the oscillator into a portion of the vehicle that faces away from the sun and which portion is thermally insulated from the rest of the vehicle.
- 7. Method according to claim 1 wherein the oscillator operating temperature range is in the range starting from the lowest operating temperature of the equipment in which the oscillator is to be used to about -250.degree. C.
- 8. Method of making a high stability quartz crystal oscillator for use in a navigation receiver capable of operating any place on earth over a temperature range of -55.degree. C. to +85.degree. C. from an SC-cut quartz crystal plate, said method including the steps of
- (A) cutting the SC-cut quartz crystal plate with angles of cut of .phi.=21.degree.56' and .sigma.=35.degree.43',
- (B) fabricating a resonator from the cut quartz crystal plate,
- (C) connecting the resonator into a high stability oscillator circuit,
- (D) placing the oscillator-circuit/resonator combination into a closed cycle refrigerator maintained at -65.degree. C., and
- (E) placing the whole assembly from step (D) into the naviagation receiver.
- 9. Method of making a high stability quartz crystal oscillator for use in a communications satellite capable of operating continuously and reliably for at least ten years while maintaining as stable a frequency as possible from an SC-cut quartz crystal plate said method including the steps of
- (A) cutting the SC-cut quartz crystal plate with angles of cut of .phi.=21.degree.56' and .sigma.=36.degree.50'
- (B) fabricating a resonator from the cut quartz crystal plate,
- (C) connecting the resonator into a high stability oscillator circuit,
- (D) placing the oscillator circuit/resonator combination into a high stability temperature controlled enclosure maintained at about -100.degree. C., and
- (E) placing the whole assembly from Step (D) into the communication satellite.
- 10. Method of making a high stability quartz crystal oscillator from an SC-cut quartz crystal plate wherein the oscillator is for use as an ultrahigh stability frequency standard for a strategic communications system terminal to be incorporated into a tracked vehicle and wherein the standard must be stable to .+-.1.times.10.sup.-11 per month, said method including the steps of
- (A) cutting the SC-cut quartz crystal plate with angles of cut of .phi.=21.degree.56' and .sigma.=38.degree.50'
- (B) fabricating a resonator from the quartz crystal plate
- (C) connecting the resonator into a high stability oscillator circuit,
- (D) placing th oscillator-circuit/resonator combination into a microminiature refrigerator maintained at about -185.degree. C., and
- (E) placing the whole assembly from Step (D) into the tracked vehicle.
Government Interests
The invention described herein may be manufactured, used and licensed by or for the Government for governmental purposes without the payment to me of any royalty thereon.
US Referenced Citations (1)
Number |
Name |
Date |
Kind |
4259606 |
Vig |
Mar 1981 |
|