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US2348604A - Horizon gyro - Google Patents

Horizon gyro Download PDF

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Publication number
US2348604A
US2348604A US472609A US47260943A US2348604A US 2348604 A US2348604 A US 2348604A US 472609 A US472609 A US 472609A US 47260943 A US47260943 A US 47260943A US 2348604 A US2348604 A US 2348604A
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United States
Prior art keywords
gyro
cap
weight
air
spindle
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Expired - Lifetime
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US472609A
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Bert G Carlson
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Jack and Heintz Inc
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Jack and Heintz Inc
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Priority to US472609A priority Critical patent/US2348604A/en
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Publication of US2348604A publication Critical patent/US2348604A/en
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02Rotary gyroscopes
    • G01C19/34Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
    • G01C19/38Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/12Gyroscopes
    • Y10T74/1229Gyroscope control
    • Y10T74/1232Erecting
    • Y10T74/1243Erecting by weight

Definitions

  • This invention relates in general to gyros and more particularly to erection device therefor.
  • the primary object of the invention is to provide an improved gyro erection device that will be simple in construction and assembly-and positive and efiicient in operation.
  • a cap rotatably mounted on the lower compartment of the gyro box to cover the air exhaust apertures and having an aperture to the atmosphere.
  • the cap is provided with a weight arranged eccentrically and near the periphery of the cap. Any deviation of the gyro box with respect to the vertical results in the weight seeking the lower side and acting as a pendulum to bring about the erection of the gyro.
  • Figure 1 is a view in elevation, partly in section of an horizon gyro assembly with the improved erection device, showing the gyro in vertical position;
  • Figure 2 is a view in cross section, taken along line 22 of Figure 1;
  • Figure 3 is a bottom plan View of the erection device.
  • Figure 4 is a partial view in elevation of the gyro box and erection device with the gyro box slightly tilted to the left.
  • Figure 1 shows an horizon gyro assembly in normal vertical position with a gyro wheel I havin trunnions 2 engaging bearings 3 in a gyro box, the rotor compartment of which is indicated at 4.
  • the box has suitable trunnions 5 to be carried by a suitable gimbal support.
  • Coextensive with the rotor compartment 4 is a lower compartment 5 to the lower end of which is secured a plate 6 by means of screws 1.
  • a cap l2 secured by a pin l3 to a spindle M which is mounted for rotation in bearing assemblies 15 and IS in such a manner that the edges of plate 6 and cap I2 overlap to form a compartment IT.
  • the cap I2 is provided with a single tangentially disposed aperture 20 so that as viewed in Figure 3 a rotation of cap 12 in a counterclockwise direction i imparted as air is exhausted from compartment l1.
  • a weight I! Secured to 'cap l2 by a screw I8 is a weight I! that is arranged eccentrically of spindle l4 and near the periphery of cap l2.
  • the force of the air exhausting through the aperture 20 causes cap l2 and its weight [9 to rotate slowly in a counterclockwise direction.
  • the weight seeks the lower side of the tilt. This is illustrated in Figure 4 where the gyro is tilted to the left and the rotative force of the air exhaust through the tangential aperture an, arranged at approximately ninety degrees to the weight, is insuificient to cause the weight to climb up the hill.
  • the maintenance of this position by the weight causes a pendulous effect upon the gyro resulting in its becoming erected.
  • the cap resume its normal slow rotation.
  • a spindle rotatably mounted in bearings in said casing below said rotor coaxially with the spin axis of said rotor, a cap secured to said spindle and forming a compartment in communication with said casing and provided with an air discharge outlet port in the periphery of said cap and at right angles to the axis of rotation of said rotor, said cap being adapted to be rotated by the discharge of air as said casing is being evacuated, a weight secured to said cap eccentrically of the axis of said spindle and adapted, upon tilt of said gyro, to overcome the rotative force created in the chamber enclosed by said rotative cap and pendulously apply an erective efiect upon said gyro assembly until said gyro is erected and automatically resume normal rotation when said erection is completed.

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  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Description

y 1944. B. G. CARLSON 2,348,604
HORIZON GYRO Filed Jan. I6, 1943 INVENTOR.
.Bzer 6f Chemo/v. BY
Patented May 9, 1944 HORIZON GYRO Bert G. Carlson, Erieside, Ohio, assignor to Jack & Heintz, Inc., Bedford, Ohio, a corporation of Ohio Application January 16, 1943, Serial No. 472,609
2 Claims.
This invention relates in general to gyros and more particularly to erection device therefor.
The primary object of the invention is to provide an improved gyro erection device that will be simple in construction and assembly-and positive and efiicient in operation.
To this end it is proposed to provide a cap rotatably mounted on the lower compartment of the gyro box to cover the air exhaust apertures and having an aperture to the atmosphere. Besides being rotatably mounted, the cap is provided with a weight arranged eccentrically and near the periphery of the cap. Any deviation of the gyro box with respect to the vertical results in the weight seeking the lower side and acting as a pendulum to bring about the erection of the gyro.
With the foregoing and other objects in View, the invention resides in the combination of parts and in the details of construction hereinafter set forth in the following specification and appended claims, certain embodiments thereof being illustrated in the accompanying drawing, in which:
Figure 1 is a view in elevation, partly in section of an horizon gyro assembly with the improved erection device, showing the gyro in vertical position;
Figure 2 is a view in cross section, taken along line 22 of Figure 1;
Figure 3 is a bottom plan View of the erection device; and
Figure 4 is a partial view in elevation of the gyro box and erection device with the gyro box slightly tilted to the left.
Referring more particularly to the drawing, Figure 1 shows an horizon gyro assembly in normal vertical position with a gyro wheel I havin trunnions 2 engaging bearings 3 in a gyro box, the rotor compartment of which is indicated at 4. The box has suitable trunnions 5 to be carried by a suitable gimbal support. Coextensive with the rotor compartment 4 is a lower compartment 5 to the lower end of which is secured a plate 6 by means of screws 1.
As is usual practice, air is drawn in by suction through ports 8 to jets 9 to impinge on the rotor buckets "J. In order to evacuate this air after it has spent its force in spinning the gyro wheel, apertures l i are provided to lead the air from the upper compartment 4 into the lower compartment 5, the lower plate 5 of which has a series of apertures I Departing from the usual practice of employing a plurality of pendulum shutters for regulatin the opening and closing of the exhaust ports, it is proposed to use a single exhaust port and a single shiftable gravity responsive weight. To this end there is provided a cap l2 secured by a pin l3 to a spindle M which is mounted for rotation in bearing assemblies 15 and IS in such a manner that the edges of plate 6 and cap I2 overlap to form a compartment IT. The cap I2 is provided with a single tangentially disposed aperture 20 so that as viewed in Figure 3 a rotation of cap 12 in a counterclockwise direction i imparted as air is exhausted from compartment l1.
Secured to 'cap l2 by a screw I8 is a weight I!) that is arranged eccentrically of spindle l4 and near the periphery of cap l2. In normal operation when the gyro is vertical the force of the air exhausting through the aperture 20 causes cap l2 and its weight [9 to rotate slowly in a counterclockwise direction. When, however, the gyro becomes tilted, the weight seeks the lower side of the tilt. This is illustrated in Figure 4 where the gyro is tilted to the left and the rotative force of the air exhaust through the tangential aperture an, arranged at approximately ninety degrees to the weight, is insuificient to cause the weight to climb up the hill. The maintenance of this position by the weight causes a pendulous effect upon the gyro resulting in its becoming erected. When the erection is completed the cap resume its normal slow rotation.
By this simple expedient the construction and assembly is greatly simplified and the operation dependable and enicient. This is because there is eliminated the provision of pendulum shutters which by reason of their hinges may not properly regulate their respective exhaust ports which latter may also become partially closed by sediment.
I claim:
1. In combination in a vertical axis gyro assembly including an air spun gyro and a casing therefor, a spindle rotatably mounted in bearings in said casing below said rotor coaxially with the spin axis of said rotor, a cap secured to said spindle and forming a compartment in communication with said casing and provided with an air discharge outlet port in the periphery of said cap and at right angles to the axis of rotation of said rotor, said cap being adapted to be rotated by the discharge of air as said casing is being evacuated, a weight secured to said cap eccentrically of the axis of said spindle and adapted, upon tilt of said gyro, to overcome the rotative force created in the chamber enclosed by said rotative cap and pendulously apply an erective efiect upon said gyro assembly until said gyro is erected and automatically resume normal rotation when said erection is completed.
semblies arranged respectively in said partition 10 and plate and a spindle extending therethrough, a cap secured to the lower end of said spindle, said spindle having a shoulder resting on the inner race of said lower bearing assembly for sustaining the entire vertical load of said spindle and cap carried thereby, said cap and plate having their inner faces spaced to provide an air chamber, an exhaust port in the periphery of the cap and in a plane at right angles to the axis of rotation of said gyro wheel, whereby an exhaust of air through said port in said cap imparts a rotary motion to the cap, said cap having secured thereto on its lower surface a weight near its periphery and eccentric of the axis of rotation of its spindle, said weight being adapted, upon tilt of said gyro, to overcome the rotative force created in the chamber enclosed by said rotative cap and pendulously apply an erective effect upon said gyro assembly until said gyro is erected and automatically resume normal rota- 15 tion when said erection i completed.
BERT Gr. CARLSON.
US472609A 1943-01-16 1943-01-16 Horizon gyro Expired - Lifetime US2348604A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2556097A (en) * 1949-09-08 1951-06-05 Norden Lab Corp Searching cage erection system for gyroscopes

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2556097A (en) * 1949-09-08 1951-06-05 Norden Lab Corp Searching cage erection system for gyroscopes

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