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US2200976A - Besetting means fob aib borne - Google Patents

Besetting means fob aib borne Download PDF

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Publication number
US2200976A
US2200976A US2200976DA US2200976A US 2200976 A US2200976 A US 2200976A US 2200976D A US2200976D A US 2200976DA US 2200976 A US2200976 A US 2200976A
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air
casing
gyroscope
vertical
borne
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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
    • 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
    • G01C19/04Details
    • G01C19/06Rotors
    • G01C19/08Rotors electrically driven
    • 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
    • Y10T74/1204Gyroscopes with caging or parking means
    • Y10T74/1211Gyroscopes with caging or parking means and resetting means
    • 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

Definitions

  • This invention relates to gyroscopic directional and similar devices of the air borne type inwhich ordinary oil or ball bearings are replacedby bearings supported entirely by air films.
  • Such gyro- 5 scopes are either used alone or operated in conjunction with a magnetic compass as a gyromagnetic compass unit, as well understood in th art of aircraft navigational instruments.
  • thsingle figure shows a. vertical section of an air borne directional gyroscope with my resetting means applied thereto.
  • the directional-gyroscope is shown as enclosed in a casing l having a front window to for reading the card i and from which air is exhausted through a pipe coupling 2 by means of a pump (not shown).
  • the gyroscope is supported within said casing for freedom about its verticalaxis by means of upper and lower spherical air bearings 23 and t which support and guide the vertical ring a about the vertical axis.
  • the rotor bearing casing e is supported for oscillation about a horizontal axis within said vertical ring on spherical air bearings l and 8.
  • Such air bearings are now well known in the art, as shown in the prior application of Leslie F. Carter, Serial No.
  • Air is shown as supplied to the instrument for lubricating or floating the bearings and spinning the rotor through a bottom screened opening it.
  • a bevel gear 28 adapted to be be brought into mesh with a bevel gear annulus re secured to the cup member IS, the latter beas ing rotatably mounted within the leasing I.
  • a U-shaped member 3i connecting the valve 25 and the push rod 27. As shown, the extension of the rod 21 passes through a hole in the right hand upturned portion 532 of said member so. that said portion is non-slidably held between collars t3 and 33' on said shaft 2?.
  • the sourceof differential air-pressure will be shut oil, thereby frictionally locking the a gyroscope about both its vertical and horizontal axes, and that by rotating the knob 26 the gyroscope may be set about its vertical axis to any desired position.
  • the hearing it is preferably of the ball bearing type so that the rotor remains up spinning even though the gyroscope is locked about another axis.
  • the frame is brought to a position with the gyro spin axis perpendicular to the normally vertical ring, but in case the vertical ring is inclined due to the inclined position of the aircraft at that time, the spin axis of the gyro will also be brought to an inclined position by the former type of setting device.
  • the rotor bearing frame is locked in whatever position with respect to the vertical ring it may be at the time the air is out 011', so that when released again it will remain in that position.
  • a resetting means for directional gyroscopes of the air borne type having a rotor bearing casing, a vertical ring and outer casing, large complementary dry bearing surfaces mounting said casing within said ring and mounting said ring within said outer casing for freedom about horizontal and vertical axes, means for supplying air flow between said surfaces to provide air flow bearings, means for shutting off the supply of air to said bearings, and means for rotating the part of at least the lower vertical bearing in said casing, while the air supply is shut off.
  • a resetting means for directional gyroscopes of the air borne type having a rotor bearing casing, a vertical ring and outer casing, large complementary dry bearing surfaces mounting said casing within said ring and mounting said ring within said outer casing for freedom about horizontal and vertical axes, means for supplying air flow between said surfaces to provide air flow bearings, means for shutting off the air supply to said bearings, means for rotating the lower-vertical bearing in said casing, and a common knob for operating both of said last named means.
  • a rotor bearing casing a rotatably mounted vertical ring, large complementary dry surfaces for supporting said casing for oscillation about a horizontal axis within said ring, means whereby air under pressure is supplied thereto for floating said casing about said axis, means for locking the casing about said axis preparatory to resetting by shutting off the air supply, means. for temporarily cutting off the air supply, and means for resetting said vertical ring and casing in azimuth while said casing is .so locked about said horizontal axis.
  • a directional gyroscope as claimed in claim 4 also having large complementary dry surface bearings supporting said ring for turning about a vertical axis whereby the vertical ring is also looked in azimuth, and means for resetting the position of said vertical ring by utilizing the friction of the dry surfaces of the lower bearing of said vertical ring while the rotor bearing casing of the gyroscope is so locked.

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

Description

ay 9 M. F. BATES RESETTING MEANS FOR AIR BORNE GYROSCOPES Filed Nov. 2, 1935 INVENTO lzgmmm 50155 v HIE AZRN Y.
.ntented M y 14, 1940 BESETTING MEANS FOR AIR BOBNE GYROSQOPES Mortimer r. Bates, Brooklyn, N. Y., assignor to Sperry Gyroscope Company, Inc, Brooklyn, N. Y., a corporation of New York I Application November 2,1935, Serial No. 48,008
Claims.
This invention relates to gyroscopic directional and similar devices of the air borne type inwhich ordinary oil or ball bearings are replacedby bearings supported entirely by air films. Such gyro- 5 scopes are either used alone or operated in conjunction with a magnetic compass as a gyromagnetic compass unit, as well understood in th art of aircraft navigational instruments.
In directional gyroscopes which have three delo grees of freedom, it is occasionally necessary to reset the same to bring the compass card thereon into the desired course or into synchronism with the magnetic compass. For resetting the ordinary type of gyroscope, considerable mechanism to is required because the gyroscope must be locked about its horizontal axis, but by my present invention I have devised an extremely simple device for resetting air borne type directional gyroscopes.
Referring to the drawing, thsingle figure shows a. vertical section of an air borne directional gyroscope with my resetting means applied thereto.
The directional-gyroscope is shown as enclosed in a casing l having a front window to for reading the card i and from which air is exhausted through a pipe coupling 2 by means of a pump (not shown). The gyroscope is supported within said casing for freedom about its verticalaxis by means of upper and lower spherical air bearings 23 and t which support and guide the vertical ring a about the vertical axis. The rotor bearing casing e, in turn, is supported for oscillation about a horizontal axis within said vertical ring on spherical air bearings l and 8. Such air bearings are now well known in the art, as shown in the prior application of Leslie F. Carter, Serial No. 734,619, filed July 11, 1934, and comprise large complementary, close fitting, curved, dry 4g metallic surfaces between which air is caused to normally flow, whereby the supported. member is floated in the supporting member. The rotor 9, in turn, is journalled in said casing for spinning about normally horizontal axis ill on any as suitable type of anti-friction bearing, preferably otherthan the air borne type.
- Air is shown as supplied to the instrument for lubricating or floating the bearings and spinning the rotor through a bottom screened opening it.
in;- The air passes upwardly through apertures t2, t2 and it within a bearing block or cup is, shaped to closely fit the spherical button It on the hottom of the vertical ring. A portion of said air said air passes upwardly, however, through an opening I5 in line with the opening l3, whence it branches into channels l6 and I6 connecting with similar channels I! and I1 and I8 and I8 which finally emerge through the top button l4 5 to supply air for lubricating or floating the same within the complementary shaped cup member I9. A portion of the air from each system of channels is also led horizontally to float the rotor bearing casing buttons 20 and 20' in the spherical 10 to the spinning nozzles 24 for spinning the rotor.
As a locking means'for locking the gyroscope preliminary to resetting or shutting down, I have 20 shown a manually operated shut-off valve 25 I adapted to close the outlet 2 at will. when said valve is closed, the rotor bearing casing becomes immediately locked about its horizontal as well as about its vertical axis because with the air re- 25 moved the large bearing surfaces, as they are not lubricated other than by air, are in frictional contact with each other. I have shown a common knob 26 both for shutting off the air pump and for resetting the gyroscope. As shown, said so knob is mounted on a shaft 21 both slidably and rotatably mounted in casing I. At the inner end of said shaft is a bevel gear 28 adapted to be be brought into mesh with a bevel gear annulus re secured to the cup member IS, the latter beas ing rotatably mounted within the leasing I. There is also shown a U-shaped member 3i connecting the valve 25 and the push rod 27. As shown, the extension of the rod 21 passes through a hole in the right hand upturned portion 532 of said member so. that said portion is non-slidably held between collars t3 and 33' on said shaft 2?. it will readily be apparent that by pushing the handlett in, the sourceof differential air-pressure, will be shut oil, thereby frictionally locking the a gyroscope about both its vertical and horizontal axes, and that by rotating the knob 26 the gyroscope may be set about its vertical axis to any desired position. The hearing it) is preferably of the ball bearing type so that the rotor remains up spinning even though the gyroscope is locked about another axis.
Since the entire weight of the gyroscope is on the lower bearing, it will ordinarily be found sufiicient to turn the lower bearing only. As above cal ring. With the ordinary type of resetting device, the frame is brought to a position with the gyro spin axis perpendicular to the normally vertical ring, but in case the vertical ring is inclined due to the inclined position of the aircraft at that time, the spin axis of the gyro will also be brought to an inclined position by the former type of setting device. In my invention, however, the rotor bearing frame is locked in whatever position with respect to the vertical ring it may be at the time the air is out 011', so that when released again it will remain in that position.
From the foregoing description it will be readily apparent that I have devised anextremely simple caging and resetting device. In the usual type of directional gyroscope, a system of gears and levers has to be employed to cage or look the gyroscope about its horizontal axis to prevent precession when resetting and it is also necessary to actually engage the vertical ring. In my system the caging function is accomplished simply for shutting off the air supply, and the resetting simply by turning the lower vertical bearing.
As many changes could be made in the above construction any many apparently widely different embodiments of this invention could be made without departing from the scope thereof, it is intended that all matter contained in the above description or shown in the accompanying drawing shall be interpreted as illustrative and not in a limiting sense. 4
Having described my invention, what I claim and desire to protect by Letters Patent is as follows:
1. In an air borne gyroscope having large complementary, dry bearing surfaces between the supported and supporting, parts and means for least one of said bearings while the air supply is ofl.
2. A resetting means for directional gyroscopes of the air borne type having a rotor bearing casing, a vertical ring and outer casing, large complementary dry bearing surfaces mounting said casing within said ring and mounting said ring within said outer casing for freedom about horizontal and vertical axes, means for supplying air flow between said surfaces to provide air flow bearings, means for shutting off the supply of air to said bearings, and means for rotating the part of at least the lower vertical bearing in said casing, while the air supply is shut off.
8. A resetting means for directional gyroscopes of the air borne type having a rotor bearing casing, a vertical ring and outer casing, large complementary dry bearing surfaces mounting said casing within said ring and mounting said ring within said outer casing for freedom about horizontal and vertical axes, means for supplying air flow between said surfaces to provide air flow bearings, means for shutting off the air supply to said bearings, means for rotating the lower-vertical bearing in said casing, and a common knob for operating both of said last named means.
4. In a directional gyroscope, a rotor bearing casing, a rotatably mounted vertical ring, large complementary dry surfaces for supporting said casing for oscillation about a horizontal axis within said ring, means whereby air under pressure is supplied thereto for floating said casing about said axis, means for locking the casing about said axis preparatory to resetting by shutting off the air supply, means. for temporarily cutting off the air supply, and means for resetting said vertical ring and casing in azimuth while said casing is .so locked about said horizontal axis.
5. A directional gyroscope as claimed in claim 4, also having large complementary dry surface bearings supporting said ring for turning about a vertical axis whereby the vertical ring is also looked in azimuth, and means for resetting the position of said vertical ring by utilizing the friction of the dry surfaces of the lower bearing of said vertical ring while the rotor bearing casing of the gyroscope is so locked.
MOR'I'IMER F. BATES.
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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2524553A (en) * 1947-02-28 1950-10-03 Gen Electric Gyroscope positioning apparatus
US2644727A (en) * 1949-10-18 1953-07-07 North American Aviation Inc Double-ball gyro precession axis bearing
US2722124A (en) * 1954-05-24 1955-11-01 G M Giannini & Co Inc Caging system for gyroscopes
US2747413A (en) * 1954-12-15 1956-05-29 Bendix Aviat Corp Gyroscope
US2786356A (en) * 1954-05-24 1957-03-26 G M Giannini & Co Inc Caging mechanism for gyroscopes
US2797581A (en) * 1954-05-25 1957-07-02 Sperry Rand Corp Gyroscopic instruments
US2801542A (en) * 1954-10-29 1957-08-06 Gen Electric Gyro setting apparatus
US3102430A (en) * 1960-05-20 1963-09-03 Sanders Associates Inc Gyroscope
US3287982A (en) * 1960-02-23 1966-11-29 Sanders Associates Inc Gyroscope

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2524553A (en) * 1947-02-28 1950-10-03 Gen Electric Gyroscope positioning apparatus
US2644727A (en) * 1949-10-18 1953-07-07 North American Aviation Inc Double-ball gyro precession axis bearing
US2722124A (en) * 1954-05-24 1955-11-01 G M Giannini & Co Inc Caging system for gyroscopes
US2786356A (en) * 1954-05-24 1957-03-26 G M Giannini & Co Inc Caging mechanism for gyroscopes
US2797581A (en) * 1954-05-25 1957-07-02 Sperry Rand Corp Gyroscopic instruments
US2801542A (en) * 1954-10-29 1957-08-06 Gen Electric Gyro setting apparatus
US2747413A (en) * 1954-12-15 1956-05-29 Bendix Aviat Corp Gyroscope
US3287982A (en) * 1960-02-23 1966-11-29 Sanders Associates Inc Gyroscope
US3102430A (en) * 1960-05-20 1963-09-03 Sanders Associates Inc Gyroscope

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