US1183530A - Means for imparting stability to unstable bodies. - Google Patents

Means for imparting stability to unstable bodies. Download PDF

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US1183530A
US1183530A US53631110A US1910536311A US1183530A US 1183530 A US1183530 A US 1183530A US 53631110 A US53631110 A US 53631110A US 1910536311 A US1910536311 A US 1910536311A US 1183530 A US1183530 A US 1183530A
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precession
pressure
valve
force
gyro
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B39/00Equipment to decrease pitch, roll, or like unwanted vessel movements; Apparatus for indicating vessel attitude
    • B63B39/04Equipment to decrease pitch, roll, or like unwanted vessel movements; Apparatus for indicating vessel attitude to decrease vessel movements by using gyroscopes directly
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/18Stabilised platforms, e.g. by gyroscope
    • 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
    • Y10T74/1218Combined
    • 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 methods and devicesfor imparting stability to bodies which are naturally unstable, including such methods as are described in my Patent No. 796893.
  • the present invention also relates to methods which have previously been proposed in my Patent No. 796893 for maintaining equilibrium by effecting shifts of the center of gravity of the unstable body relatively to its supporting means, said shifts being effected, for example, by means of fluid pressure.
  • one or more gyrostats are mounted on the body in such a manner that precession of the gyrostat or gyrostats can take place when the equilibrium of the body is disturbed, and control of the precessional movement is employed so as to cause the gyrostats to restore equilibrium, or the restoration of equilibrium is eflectedby change of the center of gravity.
  • I derive forces one of which is roportional to the couple tending to distur the body, another force proportional to the time integral of the said disturbing couple and a further force to compensate for unavoidable friction occurring in the precessional movement, these forces being employed to control other powerful forces adapted either to influence the precession of the gyrostats or to effect shifts of the center of gravity of the body relatively to its point of support.
  • the above-mentioned force, depending as to its magnitude and duration upon the disturbing couple may conveniently be derived either from the reaction or stress occurring between the gyrostat frame and its support upon the application of the disturbing couple to the said support or from the precessional movement of the gyrostat arising from the application of sai disturbing couple, and that the force depending upon the time integral of the disturbing couple may be derived either from the reaction between the gyrostat frame and its support or f or acceleration of the gyrostat from its central position under application of a disturbing couple; further, that the force depending upon the unavoidable friction occurring in the precessional movement may be derived from the precessional movement of the gyrostat itself by suitable friction coupling means.
  • Figure 1 is an elevation view showing two gyrostats mounted on a common frame and arranged so that their precession about vertical axes can be controlled;
  • Fig. 2 is a part sectional plan showing the precession control devices;
  • Fig. 3 is a cross sectional side elevation view 0 Fig. 1 on the line X X of Fig. 2 showing the arrangement of the precession controlling rack and the pistons operating the same;
  • Fig. 4 shows the valves and the three-armed lever which operates their spindles, also the spring-controlled fulcrum lever;
  • Fig. 5 is a part sectionallview through the viscous fluid coupling showing the temperature controlling devices, safety clutch devices and friction loss compensating devices and the arm applying the controlling forces to the valve.
  • FIG. 6 is a cross sectional view through a modified form of viscous fluid coupling
  • Fig. 7 is a transverse section through the two valves
  • Fig. 8 is a section at right angles to Fig. 7 through one of the valves.
  • I mount on a suitable framework m (see Figs. 1, 2, 3) which is rigid with the vehicle a pair of gyrostats, vertical axes and having I), rotating in opposite directions.
  • the frames 0 0 in which the heavy wheels I) b rotate are provided with gears 11 (1 adapted to engage with a double rack capable of sliding longitudinally, and operated by means of pistons f f moving respectively in cylinders 9 arranged co-axially on opposite sides of the gyrostats.
  • ls b b and The heavy wh electromotors h h by which they are driven are inclosed air-ti ht in casings j 7 in whlch a high degree 0 vacuum is maintained.
  • the pistons f i have spring ers a a arranged to roll on the lower side of the cylinders to reduce friction.
  • valves k (Figs. 4 and 5) connected to the cylinders by pipes 79 p, which valves are adapted to allow an amount of pressure fluid to pass to the working cylinders proportional to the pressure exerted on the valve spindle to operate the valve.
  • the valves is is for the two cylinders are respectively operated by two arms Z Z of a three-armed lever, on the third arm of which a fork n is provided in which the actuating lever 0 works.
  • These valves la, k may be of the known type described in my British Patent N o.
  • valves are connected to the hydraulic cylinders g by pipes 72 connected to the passages p.
  • a hollow cylindrical piston 52 operating in the cylindrical valve casing, at one end of which is provided an annular passage 53, surrounding the piston 52.
  • This passage is connected by a pipe 54 .to a source of high pressure fluid.
  • a valve seat 55 is formed at one end of the cylindrical valve casing is, and a conical valve surface to fit this seat is formed on the cylindrical piston 52. This valve is held on its seat by a light spring 56.
  • the valve opens into the passage p, from which fluid at a regulated pressure is supplied to one of the hydraulic cylinders 9 through he other end of the cylindrical casing of the valve In contains a lift valve 57, which is passed upon a seat formed on the end of the hollow piston 52. This valve opens into the discharge pipe 51.
  • this valve is as follows :Assuming that a pressure is applied to the exhaust valve 57 by means of a rod 58 passing through a gland in the end of the casing of the valve in, this pressure forces the exhaust valve 57 on to its seat on the end of the hollow piston 52, and if the pressure be suflicient, the hollow piston will bethrust inward, and the valve surface at the other end will be moved off its seat 55 against the pressure of the spring 56, plus whatever pressure may be in the pipe p. The fluid under pressure then flows from the supply pipe 54, and is fed to hydrauliccylinder g at a regulated pressure.
  • the spring 56 closes the valve by thrusting the hollow piston along, and at the same time moving the exhaust valve 57 with it. So far the action is that of an ordinary reducing valve. If, however, the pressure upon the discharge valve by the rod 58 be further reduced, the fluid contents supported rollthe pipe p.
  • the pipe 12 and from the receiving chamber will flow through the hollow piston 52, lift the discharge valve 57, and escape to the exhaust pipe 51, until the pressure in the hydraulic cylinder 9 just balances the pressure applied to the discharge valve by the rod 58. In this manner, the pressure within the cylinder 9 rises or falls with the force applied to the spindle 58, which controls both the discharge and piston valves. It will be seen that by this means -the hydraulic cylinder may be maintained at a varying pressure, which rises or falls according as the force acting on the valve through the spindle 58 increases or diminishes.
  • the actuating lever is operated by three separate forces all of which originate in the precessional movement of the gyrostats.
  • the vertical spindle q of one of the gyrostat frames projects upward through its upper bearing and carries a casing 1- (Figs. 5 and 6) having a circular chamber .9 in which a disk I! can rotate.
  • the circular chamber 8 is filled with a viscous fluid, and the spindle u carrying the disk at is thus caused to move by a force whose magnitude is substantially proportional to the velocity of movement of the gyrostat about the vertical axis.
  • the spindle u carries at its upper end a circular disk or drum 1: to which an operating arm 0 by which the valves is k are operated is attached by a friction clutch w composed of blocks tightened on the drum 0 by a spring 3, this clutch being provided to prevent breakage of the valve controlling gear if too rapid movement of the gyrostats occurs.
  • a friction clutch w composed of blocks tightened on the drum 0 by a spring 3, this clutch being provided to prevent breakage of the valve controlling gear if too rapid movement of the gyrostats occurs.
  • the clutch blocks '10 there is provided an arm 01 engaging a projection g on the arm a which is carried by a pair of blocks which bear against a disk 2 attached to the chamber 8 moving with the gyrostats, and by these blocks a force proportional to the unavoidable friction occurring in the precessional movement is impressed on the operating arm 0.
  • This friction clutch is so regulated by adjusting the spring 4 that the friction occurring in the precessional movement is compensated
  • the effect of these springs 6 6 is to cause the gyrostats to exert an electric current the on the operating arm 0 a force proportional to the displacement of the gyrostats from their central position, this force always acting in the direction to bring the gyrostats back to their central position.
  • valves is controlling the admission of pressure fluid to the cylinders g g which operate the rack e controlling the precessional movement are acted on by three forces, one force due to the springs 6 6 and proportional to the displacementof the gyrostats from the central position, a sec- 0 (1 force due to the viscous coupling 8 t which causes to be transmitted to the valves a force proportional to the velocity of precession of the gyrostats or substantially proportional thereto, and a third force proportional to the resistance due to the unavoidable mechanical friction of the parts occurring in the precessional movement of the gyrostat.
  • I line the casing 1' with a nonconducting substance and insert within the casing r and in proximity to the chamber 8 resistance coils 41 controlled by switches 42 and so arranged that by the passage of right degree of temperature may be maintained.
  • the current may be controlled if desired by a thermostat or the like.
  • Fig. 6 illustrates a modified construction of the viscous coupling shown in Fig. 5.
  • a number of plates t are employed, each plate being contained within separate chambers s.
  • the chambers s of this modification are formed. by disks having downwardly turned rims, the width of the rims being so chosen that each disk is supported from the next, such a distance as to form a chamber for one of the disks t.
  • the disks t are keyed to the spindle u while the disks forming the chambers s are secured to the casing r to prevent further rotation.
  • a spindle 43 having a fine thread cut upon its upper end, this thread engaging an internal thread out upon the inside of the spindle u.
  • the spindle 43 carries a handle 44 and is provided at its lower extremity with a reduced portion adapted to bear upon a suitable thrust piece.
  • the spindle u is raised orv lowered the viscous fluid (Fig. 5) at the applied to the gyroscopes with respect to the casing r and when the correct adjustment has been made the spindle 43 is locked in position by means of the locking device 45.
  • Each of the constituent forces is of importance in securing a highly efiicient de vice.
  • a highly accurate and efficient governor is obtained, since the velocity of precession is directly proportional to the disturbing force acting on the body. Again, it is equally important in unstable bodies, that the righting force be increased in proportion to the length of time the disturbing force acts. This is accomplished by governing the righting force according to the amount of precession of the gyro. The destroying of the effect of frie tion around the precession axis is also important, as this always results in the impairment of the righting couple exerted by the gyroscope.
  • gyroscopic apparatus the combination of a gyroscope and a precessional frame therefor, of means for overcoming the effect of friction about the precessional axis comprising a frictional member adapted to be moved by precession of the gyro, and a depp y a positive torque on the gyro about said axis.
  • means for automatically accelerating the precession of said gyro comprising a governing member adapted'to exert a force proportional to the displacement of the gyro from its central position, a second member for exerting a force proportional to the friction about the precessional axis, and a force multiplying'device connected to both of said governing members for applying a torque on the gyro in the direction of the existing precession.
  • means for automatically accelerating the precession of said gyro comprising a governing member adapted to exert a force proportional to the displacement of the gyro from its central position, a second member for exerting a force proportional to the velocity of precession of the gyro, a third member for exerting a force proportional to the friction about the precession axis and a force multiplying device connected to all of said governing members for applying a torque on the gyro in the direction of the existing precession.
  • means for exerting orces to preserve equilibrium of said body including fluid pressure cylinders, and valves allowing an amount of pressure fluid to pass to working cylinders proportional to pressure exerted to operate said valves, and means to exert pressure to operate said valves actuated by said gyrostat or gyrostats, as set forth.
  • a frame rigidly connected to said body, a pair of gyrostats pivotally mounted about vertical axes in said frame, fluid pressure cylinders rigidly mounted in said frame, pistons in said hydraulic cylinders, arack connecting said pistons, segments on said gyrostat frames cooperating with said rack, valves controlling the flow of fluid to said cylinders, in such a manner that the pressure in said cylinders is proportional to the pressure exerted to operate said valves, a member mounted on the precession axle of one of said gyrostats, .a member cooperating with said member, and connected thereto by a viscous coupling, a connection between said second member and said valves,a spring controlled member acting on said valves proportionally to the displacement of sai gyrostats from the central position, and

Description

L. BRENNAN. MEANS FOR IMPARTING STABILITY TO UNSTABLE BODIES. APPLICATION FILED JAN. 4, mo.
1 1 83,530. Patented May 16, 1916.
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L. BRENNAN. MEANS FOR IMPARTING STABILITY T0 UNSTABLE BODIES.
APPLICATION FILED JAN- 4, 19H).
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MEANS FOR IMPARTING STABILITY T0 UNSTABLE BODIESL APPLICATION FILED JAN. 4 I910.
Patented May 16, 1916.
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MEANS FOR IMPARTING STABILITY T0 UNSTABLE BODIES.
APPLICATION FILED IAN. 4,19'0. 1,183,530. Patented May 16, 1916.
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APPLICAIIUN min JAN. 4. mo.
MEANS FOR IMPARTINu STABILITY T0 UNSTABLE BODIES.
LOUIS BRENNAN,
OF GILLINGHAM, ENGLAND.
MEANS FOB IMPAB'IING STABILITY TO UNS'IAJBLE BODIES.
Specification of letters Patent.
Patented May 16, 1916.
Application filed January 4, 1910. Serial No. 536,311.
a subject of the King of Ireland, and residing at lingham, in the county of Kent, England, have invented certain new and useful Improvements in Means for Imparting Stability to Unstable Bodies, of which the following is a specification.
This invention relates to methods and devicesfor imparting stability to bodies which are naturally unstable, including such methods as are described in my Patent No. 796893.
The present invention also relates to methods which have previously been proposed in my Patent No. 796893 for maintaining equilibrium by effecting shifts of the center of gravity of the unstable body relatively to its supporting means, said shifts being effected, for example, by means of fluid pressure.
According to the invention described in my said patent, one or more gyrostats are mounted on the body in such a manner that precession of the gyrostat or gyrostats can take place when the equilibrium of the body is disturbed, and control of the precessional movement is employed so as to cause the gyrostats to restore equilibrium, or the restoration of equilibrium is eflectedby change of the center of gravity.
According to my present invention, I derive forces one of which is roportional to the couple tending to distur the body, another force proportional to the time integral of the said disturbing couple and a further force to compensate for unavoidable friction occurring in the precessional movement, these forces being employed to control other powerful forces adapted either to influence the precession of the gyrostats or to effect shifts of the center of gravity of the body relatively to its point of support. have found that the above-mentioned force, depending as to its magnitude and duration upon the disturbing couple, may conveniently be derived either from the reaction or stress occurring between the gyrostat frame and its support upon the application of the disturbing couple to the said support or from the precessional movement of the gyrostat arising from the application of sai disturbing couple, and that the force depending upon the time integral of the disturbing couple may be derived either from the reaction between the gyrostat frame and its support or f or acceleration of the gyrostat from its central position under application of a disturbing couple; further, that the force depending upon the unavoidable friction occurring in the precessional movement may be derived from the precessional movement of the gyrostat itself by suitable friction coupling means.
Referring now to the accompanying drawings, Figure 1 is an elevation view showing two gyrostats mounted on a common frame and arranged so that their precession about vertical axes can be controlled; Fig. 2 is a part sectional plan showing the precession control devices; Fig. 3 is a cross sectional side elevation view 0 Fig. 1 on the line X X of Fig. 2 showing the arrangement of the precession controlling rack and the pistons operating the same; Fig. 4 shows the valves and the three-armed lever which operates their spindles, also the spring-controlled fulcrum lever; Fig. 5 is a part sectionallview through the viscous fluid coupling showing the temperature controlling devices, safety clutch devices and friction loss compensating devices and the arm applying the controlling forces to the valve.
operating lever; Fig. 6 is a cross sectional view through a modified form of viscous fluid coupling; Fig. 7 is a transverse section through the two valves; while Fig. 8 is a section at right angles to Fig. 7 through one of the valves.
In carrying the invention into effect according to one modification which is described as applied to a monorail vehicle, and in the case in which e uilibrium of the unstable body is maintained by acceleration of the precession of the gyrostat or gyrostats, I mount on a suitable framework m (see Figs. 1, 2, 3) which is rigid with the vehicle a pair of gyrostats, vertical axes and having I), rotating in opposite directions. The frames 0 0 in which the heavy wheels I) b rotate are provided with gears 11 (1 adapted to engage with a double rack capable of sliding longitudinally, and operated by means of pistons f f moving respectively in cylinders 9 arranged co-axially on opposite sides of the gyrostats. ls b b and The heavy wh electromotors h h by which they are driven are inclosed air-ti ht in casings j 7 in whlch a high degree 0 vacuum is maintained.
their heavy wheels free to precess about.
axes are controlled The pistons f i have spring ers a a arranged to roll on the lower side of the cylinders to reduce friction.
The admission and exhaust of compressed air or other working fluid from the cylinders g g to turn the gyrostats about vertical by means of suitable valves is k (Figs. 4 and 5) connected to the cylinders by pipes 79 p, which valves are adapted to allow an amount of pressure fluid to pass to the working cylinders proportional to the pressure exerted on the valve spindle to operate the valve. The valves is is for the two cylinders are respectively operated by two arms Z Z of a three-armed lever, on the third arm of which a fork n is provided in which the actuating lever 0 works. These valves la, k, may be of the known type described in my British Patent N o. 7177 of 1902, two sections at right angles being shown at Figs. 7 and 8. The valves are connected to the hydraulic cylinders g by pipes 72 connected to the passages p. In each valve there is provided a hollow cylindrical piston 52, operating in the cylindrical valve casing, at one end of which is provided an annular passage 53, surrounding the piston 52. This passage is connected by a pipe 54 .to a source of high pressure fluid. A valve seat 55 is formed at one end of the cylindrical valve casing is, and a conical valve surface to fit this seat is formed on the cylindrical piston 52. This valve is held on its seat by a light spring 56. The valve opens into the passage p, from which fluid at a regulated pressure is supplied to one of the hydraulic cylinders 9 through he other end of the cylindrical casing of the valve In contains a lift valve 57, which is passed upon a seat formed on the end of the hollow piston 52. This valve opens into the discharge pipe 51. The operation of this valve is as follows :Assuming that a pressure is applied to the exhaust valve 57 by means of a rod 58 passing through a gland in the end of the casing of the valve in, this pressure forces the exhaust valve 57 on to its seat on the end of the hollow piston 52, and if the pressure be suflicient, the hollow piston will bethrust inward, and the valve surface at the other end will be moved off its seat 55 against the pressure of the spring 56, plus whatever pressure may be in the pipe p. The fluid under pressure then flows from the supply pipe 54, and is fed to hydrauliccylinder g at a regulated pressure.
en the pressure in the cylinder 9 is nearly equal to the pressure applied to the discharge valve, the spring 56 closes the valve by thrusting the hollow piston along, and at the same time moving the exhaust valve 57 with it. So far the action is that of an ordinary reducing valve. If, however, the pressure upon the discharge valve by the rod 58 be further reduced, the fluid contents supported rollthe pipe p.
the pipe 12 and from the receiving chamber will flow through the hollow piston 52, lift the discharge valve 57, and escape to the exhaust pipe 51, until the pressure in the hydraulic cylinder 9 just balances the pressure applied to the discharge valve by the rod 58. In this manner, the pressure within the cylinder 9 rises or falls with the force applied to the spindle 58, which controls both the discharge and piston valves. It will be seen that by this means -the hydraulic cylinder may be maintained at a varying pressure, which rises or falls according as the force acting on the valve through the spindle 58 increases or diminishes.
In order to provide suflicient exhaust from the cylinders when the actuating lever causes the valve to open only a slight distance the three-armed lever carrying the valve tappets operating the valve spindles is' fulcrumed at 40 (see Fig. 4) on a pivoted arm 18 held at one end by a spring 19 so that the fulcrum yields to a slight extent when the operating arm 0 is moved, causing the exhaust to open to a greater extent than would otherwise be the case.
The actuating lever is operated by three separate forces all of which originate in the precessional movement of the gyrostats. The vertical spindle q of one of the gyrostat frames projects upward through its upper bearing and carries a casing 1- (Figs. 5 and 6) having a circular chamber .9 in which a disk I! can rotate. The circular chamber 8 is filled with a viscous fluid, and the spindle u carrying the disk at is thus caused to move by a force whose magnitude is substantially proportional to the velocity of movement of the gyrostat about the vertical axis. The spindle u carries at its upper end a circular disk or drum 1: to which an operating arm 0 by which the valves is k are operated is attached by a friction clutch w composed of blocks tightened on the drum 0 by a spring 3, this clutch being provided to prevent breakage of the valve controlling gear if too rapid movement of the gyrostats occurs. Depending from the clutch blocks '10 there is provided an arm 01 engaging a projection g on the arm a which is carried by a pair of blocks which bear against a disk 2 attached to the chamber 8 moving with the gyrostats, and by these blocks a force proportional to the unavoidable friction occurring in the precessional movement is impressed on the operating arm 0. This friction clutch is so regulated by adjusting the spring 4 that the friction occurring in the precessional movement is compensated There are secured to the of horizontally projecting arms 5 5, the ends of which are attached by springs 6 6 to the clutch blocks w. The effect of these springs 6 6 is to cause the gyrostats to exert an electric current the on the operating arm 0 a force proportional to the displacement of the gyrostats from their central position, this force always acting in the direction to bring the gyrostats back to their central position. It will thus be seen that the valves is controlling the admission of pressure fluid to the cylinders g g which operate the rack e controlling the precessional movement are acted on by three forces, one force due to the springs 6 6 and proportional to the displacementof the gyrostats from the central position, a sec- 0 (1 force due to the viscous coupling 8 t which causes to be transmitted to the valves a force proportional to the velocity of precession of the gyrostats or substantially proportional thereto, and a third force proportional to the resistance due to the unavoidable mechanical friction of the parts occurring in the precessional movement of the gyrostat. The effect of these forces acting on the valves is simply multiplied to the required extent by the elastic fluid cylinders g and caused to act directly on the gyrostats through the rack e and toothed sectors (l d which operate to turn the gyrostats about vertical axes.
In order to maintain contained in the receptacle 8 proper viscosity irrespective of the climate variations I line the casing 1' with a nonconducting substance and insert within the casing r and in proximity to the chamber 8 resistance coils 41 controlled by switches 42 and so arranged that by the passage of right degree of temperature may be maintained. The current may be controlled if desired by a thermostat or the like.
Fig. 6 illustrates a modified construction of the viscous coupling shown in Fig. 5. In the construction shown in Fig. 6 a number of plates t are employed, each plate being contained within separate chambers s. The chambers s of this modification are formed. by disks having downwardly turned rims, the width of the rims being so chosen that each disk is supported from the next, such a distance as to form a chamber for one of the disks t. It is to be understood that the disks t are keyed to the spindle u while the disks forming the chambers s are secured to the casing r to prevent further rotation.
In order to position the disks t at the proper distance from the surfaces on the disks forming the chambers s I provide within the spindle u a spindle 43 having a fine thread cut upon its upper end, this thread engaging an internal thread out upon the inside of the spindle u. The spindle 43 carries a handle 44 and is provided at its lower extremity with a reduced portion adapted to bear upon a suitable thrust piece. By rotating the spindle 43 by means of the handle 44, the spindle u is raised orv lowered the viscous fluid (Fig. 5) at the applied to the gyroscopes with respect to the casing r and when the correct adjustment has been made the spindle 43 is locked in position by means of the locking device 45.
The operation of my invention as applied 70 to the stabilizing of vehicles, such as monorail cars, vessels, aeroplanes and the like is as follows: As soon as the equilibrium of the vehicle becomes disturbe a force is through the vertical pivots g in frames m, causingprecession about said pivots. As soon as this movement starts, the controlling means secured to the end of axle q are brought into action, causing a compound force to be exerted on rod 0, which is the resultant of the force due to the viscosity of the liquid in chamber 8, the force exerted by springs 6 and the force due to friction blocks w. These forces, it will be remembered, are approximately proportional to the velocity of precession, the displacement of the ros from their central position and the friction around the vertical aXes, respectively. The valves K are moved by rod 0 in proportion to the force exerted thereon and govern the fluid pressure cylinders so that they multiply the force and apply it to the gyros, causing acceleration of the precession and the consequent righting of the vehicle.
Each of the constituent forces is of importance in securing a highly efiicient de vice. By employing a righting force on the vehicle which is responsive to the velocity of precession of the gyro, a highly accurate and efficient governor is obtained, since the velocity of precession is directly proportional to the disturbing force acting on the body. Again, it is equally important in unstable bodies, that the righting force be increased in proportion to the length of time the disturbing force acts. This is accomplished by governing the righting force according to the amount of precession of the gyro. The destroying of the effect of frie tion around the precession axis is also important, as this always results in the impairment of the righting couple exerted by the gyroscope.
In'accordance with the provisions of the patent statutes, I have herein described the principle of operation of my invention, together with the apparatus which I now consider to represent the best embodiment therefor, but I desire to have it understood that the apparatus shown is only illustrative and that the. invention can be carried out by other means. Also, while it is designed to use the various features and elements in the combination and relations described, some of these may be altered and others omitted without interfering with the more general results outlined, and the invention extends to such use.
Having now described my invention, what vice controlled by said member for I claim as new and desire to secure by Letters Patent is 1. The combination with a vehicle, of a. stabilizing gyroscope therefor, a variable torque applying means for accelerating the precession of said gyro, and means brought into action by said precession and governed by the velocity of precession for controlling said torque applying means.
2. The combination with a vehicle, of a stabilizing gyroscope mounted thereon, means for automatically accelerating the precession of said gyro comprising a governing member adapted to exert a force proportional to the displacement of the gyro from its central position and a force multiplying device connected to said governing member for applying a torque on the gyro in the direction of the existing precession.
3. In gyroscopic apparatus, the combination of a gyroscope and a precessional frame therefor, of means for overcoming the effect of friction about the precessional axis comprising a frictional member adapted to be moved by precession of the gyro, and a depp y a positive torque on the gyro about said axis.
4. The combination with a vehicle, of a stabilizing gyroscope mounted thereon, means for automatically accelerating the precession of said gyro comprising a governing member adapted to exert a force proportional to the displacement of the gyro from its central position a second member for exerting a force proportional to the velocity of precession of the gyro, and a force multiplying device connected to both of said governing members for applying a torque on the gym in the direction of the existing precession.
5. The combination with a vehicle, of a stabilizing gyroscope mounted thereon, means for automatically accelerating the precession of said gyro comprising a governing member adapted'to exert a force proportional to the displacement of the gyro from its central position, a second member for exerting a force proportional to the friction about the precessional axis, and a force multiplying'device connected to both of said governing members for applying a torque on the gyro in the direction of the existing precession.
6. The combination with a vehicle, of a stabilizing gyroscope mounted thereon, means for automatically accelerating the precession of said gyro comprising a governing member adapted to exert a force proportional to the displacement of the gyro from its central position, a second member for exerting a force proportional to the velocity of precession of the gyro, a third member for exerting a force proportional to the friction about the precession axis and a force multiplying device connected to all of said governing members for applying a torque on the gyro in the direction of the existing precession.
7. The combination with a vehicle, of a stabilizing gyroscope therefor,fluid pressure means for exerting powerful forces about the precession axis of said gyroscope, and controlling means for said first means comprising a valve adapted to vary the pressure of said first means according to the pressure exerted thereon and means responsive to the velocity of precession of the gyro for governing the pressure on said valve.
8. The combination with a vehicle, of a stabilizing gyroscope therefor, fluid pressure means for exerting powerful forces about the precession axis of said gyroscope, and controlling means for said first means comprising a valve adapted to vary the pressure of said first means according to the pressure exerted thereon and a spring controlled member acting on said valves proportionally to the displacement of the gyroscope from its normal position.
9. The combination with a vehicle, of a stabilizing gyroscope therefor, fluid pressure means for exerting powerful forces about the precession axis of said gyroscope, and controlling means for said first means comprising a valve adapted to vary the pressure of said first means according to the pressure exerted thereon and means responsive to the friction developed about the precession axes for governing the pressure on said valve.
10. The combination with a vehicle, of a stabilizing gyroscope therefor, fluid pressure means for exerting powerful forces about the precession axis of said gyroscope, and controlling means for said first means comprising a valve adapted to vary the pressure of said first means according to the pressure exerted thereon and compouund means responsive to the combinative influence of the velocity and amount of precession of the gyro for governing the pressure on said valve.
11. The combination with a vehicle, of a stabilizing gyroscope therefor, fluid pressure means for exerting powerful forces about the precession axis of said gyroscope, and controlling means for said first means comprising a valve adapted to vary the pressure of said first means according to the pressure exerted thereon and compound means responsive to the combinative influence of the velocity of precession and to the friction about the precessional axis of the gyro for governing the pressure on said valve.
12. The combination with a vehicle, of a stabilizinggyroscope therefonfluid pressure means forexerting powerful forces about the precession axis of said gyroscope, and controlling means for said first means comprising a valve adapted to vary the pressure of said first means according to the pressure exerted thereon and compound means responsive to the combinative influence of the velocity and amount of precession and to the friction about the precessional axis of the gyro for governing the pressure on said valve.
13. In an unstable body carrying a rostat or gyrostats, means for exerting orces to preserve equilibrium of said body, including fluid pressure cylinders, and valves allowing an amount of pressure fluid to pass to working cylinders proportional to pressure exerted to operate said valves, and means to exert pressure to operate said valves actuated by said gyrostat or gyrostats, as set forth.
14. In combination, in an unstable body, a frame rigidly connected to said body, a pair of gyrostats pivotally mounted about vertical axes in said frame, fluid pressure cylinders rigidly mounted in said frame, pistons in said hydraulic cylinders, arack connecting said pistons, segments on said gyrostat frames cooperating with said rack, valves controlling the flow of fluid to said cylinders, in such a manner that the pressure in said cylinders is proportional to the pressure exerted to operate said valves, a member mounted on the precession axle of one of said gyrostats, .a member cooperating with said member, and connected thereto by a viscous coupling, a connection between said second member and said valves,a spring controlled member acting on said valves proportionally to the displacement of sai gyrostats from the central position, and
means acting on said valves proportionally to the friction of the precessional movement, as set forth.
15. The combination with a vehicle, of a stabilizing gyroscope therefor, a variable torque applying means for controlling the precession of said yroscope, and means brought into action y said precession and governed by the velocity of precession for controlling said torque applying means.
16. The combination with a vehicle, of a stabilizing gyroscope therefor, a governing member adapted to exert forces proportional to the displacement of the gyroscope from its central position, and a force multiplying device connected to said governing member for applying torques on the gyroscope adapted to control the precession.
17 The combination with stabilizing gyroscope mounted thereon, means for controllmg the precession of said gyro comprising a governing member adapted to exert a force proportional to the displacement of the gyro from its central position, a second member for exerting a force proportional to the velocity of precession of the gyro, and a force multiplying device connected to both of said governing members for applying a torque on the r0 for controlling precession.
In testimony whereof I affix my signature in presence of two witnesses.
LOUIS BRENNAN.
Witnesses:
J. Pnnms CRAWLEY, AUBREY T. Evans.
a vehicle, of a
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2629472A (en) * 1949-11-29 1953-02-24 Russell L Sterner Fluid shear type coupling
US2629859A (en) * 1948-12-18 1953-02-24 Norden Lab Corp Electrical rate generator
US2718149A (en) * 1952-05-23 1955-09-20 John W Bamford Damping control
US3052128A (en) * 1954-03-22 1962-09-04 Globe Ind Inc Auto pilot structure
US3193068A (en) * 1962-04-24 1965-07-06 Ingersoll Rand Co Temperature-responsive coupling means
US3576134A (en) * 1968-02-19 1971-04-27 Tetra Tech Gyroscopic stabilizer having an adjustable spring
US5201392A (en) * 1992-05-15 1993-04-13 Fairchild Space And Defense Corporation Change of state coupling
US20040244513A1 (en) * 2003-06-04 2004-12-09 Adams John D. Gyroscopic roll stabilizer for boats
US20110030604A1 (en) * 2009-04-21 2011-02-10 Mitsubishi Heavy Industries, Ltd. Swing motion reducing apparatus for ship
RU211623U1 (en) * 2022-02-14 2022-06-16 Общество с ограниченной ответственностью "КМЗ" Self balancing monorail car

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2629859A (en) * 1948-12-18 1953-02-24 Norden Lab Corp Electrical rate generator
US2629472A (en) * 1949-11-29 1953-02-24 Russell L Sterner Fluid shear type coupling
US2718149A (en) * 1952-05-23 1955-09-20 John W Bamford Damping control
US3052128A (en) * 1954-03-22 1962-09-04 Globe Ind Inc Auto pilot structure
US3193068A (en) * 1962-04-24 1965-07-06 Ingersoll Rand Co Temperature-responsive coupling means
US3576134A (en) * 1968-02-19 1971-04-27 Tetra Tech Gyroscopic stabilizer having an adjustable spring
US5201392A (en) * 1992-05-15 1993-04-13 Fairchild Space And Defense Corporation Change of state coupling
US20040244513A1 (en) * 2003-06-04 2004-12-09 Adams John D. Gyroscopic roll stabilizer for boats
US6973847B2 (en) 2003-06-04 2005-12-13 Gearloose Engineering, Inc. Gyroscopic roll stabilizer for boats
US20050274210A1 (en) * 2003-06-04 2005-12-15 Gearloose Engineering, Inc., A Maryland Corporation Gyroscopic roll stabilizer for boats
US20110030604A1 (en) * 2009-04-21 2011-02-10 Mitsubishi Heavy Industries, Ltd. Swing motion reducing apparatus for ship
EP2243697A3 (en) * 2009-04-21 2011-11-30 Mitsubishi Heavy Industries, Ltd. Swing motion reducing apparatus for ship
TWI383920B (en) * 2009-04-21 2013-02-01 Mitsubishi Heavy Ind Ltd Swing motion reducing apparatus for ship
RU211623U1 (en) * 2022-02-14 2022-06-16 Общество с ограниченной ответственностью "КМЗ" Self balancing monorail car

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