US2597361A - Hydraulic servomotor and the like - Google Patents

Hydraulic servomotor and the like Download PDF

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US2597361A
US2597361A US164759A US16475950A US2597361A US 2597361 A US2597361 A US 2597361A US 164759 A US164759 A US 164759A US 16475950 A US16475950 A US 16475950A US 2597361 A US2597361 A US 2597361A
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collapsible
movement
collapse
spring
input member
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US164759A
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Mott Lawrence Farnell
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HM Hobson Ltd
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HM Hobson Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B9/00Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/14Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with rotary servomotors

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  • Certain types of hydraulic jacks and motors are controlled by a control valve, which controls the rate and direction of the supply of liquid under pressure to produce movement of an output member in a direction and to an extent determined by the movement imparted to the control valve by a manually operable input member.
  • a control valve which controls the rate and direction of the supply of liquid under pressure to produce movement of an output member in a direction and to an extent determined by the movement imparted to the control valve by a manually operable input member.
  • Provision for this may be made by connection of the manually operable input member, by which movement is imparted to the control valve, to a collapsible link which will collapse under the extra force applied to the input member in the event of seizure of the control valve, and thereby actuate mechanism for rendering the servomotor ineffective, despite continued seizure of its control valve, to prevent movement of the output member to the desired position, either manually or by means of another servomotor.
  • United States application Serial No. 164,654 there is described an arrangement of this character, in which collapse of the collapsible link operates a valve to cut off the pressure supply to the'control valve and establish a connection between the opposite ends of the jack or motor.
  • two identical servomotors with separate sources of pressure supply may be coupled to a single output member, the control valves of both servomotors being controlled by a common input member and each control valve being associated with a collapsible link arranged, when it collapses, to render the associated servomotor ineifective to prevent positioning of the output member by the other servomotor.
  • the associated servomotor loses its irreversibility. Operation of the remaining collapsible link, again as a result of valve seizure, will result in a complete loss of irreversibility and, where the output forces are so large as to render manual force insignificant, loss of control.
  • the invention accordingly provides the com- .bination, with a manually operable input member and an output member, of a pair of hydraulic actuators (i. e. jacksor motors) arranged normally to cooperate in maving the output member in a direction and to a position determined by the movement imparted to the input member, each actuator having a control device linked to the input member and a collapsible member arranged to collapse on seizure of the control device, torender the actuator inefiective to prevent movement of the output member by the other'actuator, and means operative on collapse of either member to lock the other member against collapse.
  • a pair of hydraulic actuators i. e. jacksor motors
  • each actuator having a control device linked to the input member and a collapsible member arranged to collapse on seizure of the control device, torender the actuator inefiective to prevent movement of the output member by the other'actuator, and means operative on collapse of either member to lock the other member against collapse.
  • control devices of the actuators are constituted by control valves.
  • the actuators may be controlled byvariable stroke hydraulic pumps so as I to position the output member in accordance with the position assumed by the input member.
  • the jacks may derive pressurefrom the same source, provided provision is'made, in the-event of collapse of either member, for-cutting off the pressure supply from the control valve of the aifected jack. I prefer, however, to provide a separate source of pressurefor each jack.
  • Fig. 1 shows a purely mechanical interlock between the two collapsible members
  • Fig. 2 shows an electromagnetically operated interlock between the two collapsiblemembers.
  • Figs; 3 and-3a are diagrams showing the application or the interlock of Fig. 1 tea system embodying duplicated hydraulicmotors.
  • two hydraulic motors 83, 83 serve to operate a control surface.
  • Parts associated with the servomotor 83 bear the same reference numerals as corresponding parts associated with the servomotor 83, with the addition of the suflix a.
  • the pilot's input member 29 is connected to a link 84 which, on movement of the input member, turns about a pivot 85 to shift a linkage 88, 81, 81, I81, I81, thereby moving the two control valves 36, 36 in the same direction.
  • the motor 83 comprises a shaft 88, carrying a pair of eccentrics 89, 90 spaced at 180 (1. e. in antiphase) on the shaft.
  • a pair of eccentrics 89, 90 spaced at 180 (1. e. in antiphase) on the shaft.
  • Associated with the eccentric 89 is a set of six cylinders, each containing a piston 9
  • a similar set of six cylinders each containing a piston 92, is associated with the eccentric 90.
  • Associated with each aligned pair of cylinders is one of six distributing valves 93, each of which is held by a spring 94 in contact with a swashplate 95 on the shaft 88.
  • Fig. 3 For simplicity but one pair of aligned cylinders, containing pistons 9
  • the motor has a drain connection I83 for leading :away liquid which may leak past the pistons 9
  • Pressure is supplied, from an inlet 31,via a normally open valve I80 to an inlet port 40 associated with the control valve 36.
  • the valve 38 also controls outlet ports 41 connected to an exhaust outlet 46.
  • gear wheels 98, 98 a common gear wheel 99 connected, by bevel gearing I to a threaded sleeve IOI, engaging a pair of screw jacks I02 which are moved inwards or outwards, according to the direction of rotation of the member IN, to impart movement to the two portions of the control surface, not shown.
  • a follow-up rod I03 In screw threaded engagement with the boss of the gear wheel 99 is a follow-up rod I03 which operates, by rocking the link 84 about its pivotal attachment I04 to the input member 29, to return the control valves 36, 36 to neutral position.
  • the collapsible member 23 is of the construction described in United States application Serial No. 164,653 and comprises a tube mounted to slide in a housing 22, a number of balls 53 which project through holes in the tube and into holes 56 in the housing, and a plunger 52 having a conical head 51 which is held by a compression spring 54 in position to hold the balls 53 in the position shown.
  • a catch 65 on the tube 5I coacts with a catch 11 associated with the valve I60 to hold the valve open against the action of its spring 18 as shown.
  • valve 36 should seize, the force exerted by the pilot on the input member 29 will cause the member 23 to collapse, as described in United States application Serial No. 164,653. The follow ing sequence of events will then occur:
  • the catch 11 will be freed, allowing the valve I60 to be closed by the spring 18. This cuts off pressure from the control valve 35, and also from a line I05. As long as there is pressure in the line I05, a plunger I00 is held, against the action of a spring I91, to maintain contacts I08, I09 closed. When the pressure is cut off, the spring I01 causes the contacts I08, I09 to be separated, thereby lighting a warning lamp.
  • valve I68 When the valve I68 closes, its stem I It) moves into position to open a connection between the lines 98, 91, thereby allowing the hydraulic motor 83 to run freely, as it is driven through the gears 99, 98, on continued operation of the still effective motor 83 On seizure of the control valve 30 a precisely similar action takes place.
  • the member 23 collapses and the valve I60 closes, to cut off pressure from the valve 36*, to energize the associated warning lamp, and to connect together the lines 98, 91
  • Interlocking bolts I I I, III extend between plungers H2, 2 constituting extensions of the tubes 5I, 5
  • Within the plungers II2, 2 are disposed resetting plungers 58, 58 for the collapsible members which operate as described in United States application Serial No.
  • Each of the plungers II2, I I 2 may be normally prevented from moving in relation to the housing 22 by a shear pin, instead of by a resettable collapsible member of the kind shown in Fig. 3.-
  • the two locking bolts III, III are of identical construction. One only will therefore be described.
  • the plunger I II has, at one end, a rounded head 4 which is held by a spring 5 in engagement with a rounded groove 8 in the plunger I I2 and at the other end a square head 1 which is held, by the spring 5, clear of a square groove 8* in the plunger I I 2.
  • the rounded heads 4, 4 of the two bolts face in opposite directions,
  • interlock can only conveniently be usedwhere the two actuators are actuated (fairly close together. If it is desired to place the actuators further apart, e. g. at opposite ends of an aircraft control surface, the interlock may be efiected'electrically, as shown in Fig. 2.
  • each of the locking bolts is divided into two parts.
  • the locking bolt comprises a part 2 havinga rounded head 4 urged by the spring 5 into engagement with the square groove 8 in the other plunger 12, and a part 3H having a square head I which is normally held by a spring l5 out of engagement with the square groove 8 in the other plunger 2
  • the part 3 abuts at its upper end against a core '60, disposed in a solenoid SI and attached to the part 3 is a rod l2 of insulat-i-ng material which passes upwardly through the core 60.
  • the core 60 and rod 12 each carry one of a pair of contacts l9 which are normally held closed by a spring l5.
  • each of said actuators comprising a control device linked to the input member and movable by said input member in opposite directions to efiect through the agency of the actuator movement of said output member in a dimotion and to an extent determined by the movement imparted to the input member, a collapsible member linked to the input member and arranged to collapse, on seizure of the control device, as the result of abnormal manual efiort applied to the input member, means responsive to collapse of said collapsible member for rendering the actuator ineffective to prevent continued actuation of the output member by the other actuator under control of the input member, and means operative on collapse of the collapsible member associated with either actuator to lock against collapse the collapsible member associated with the other actuator.
  • each of said actuators comprising a control valve linked to the input member and movable thereby to efiect alternative pressure and exhaust connections tosaid actuator and thereby to effect movement of said output member in a direction and to an extent determined by the movement imparted to the input member, a collapsible member linked to the input member and arranged to collapse, on seizure of the control valve, as the result of abnormal manual effort applied to the input member, means responsive to collapse of said collapsible member for rendering the actuator ineffective to prevent continued actuation of the output member by the other actuator under control of the input member, and means operative on collapse of the collapsible member associated with either actuator to lock against collapse the collapsible member associated with the other actuator.
  • each of said actuators comprising a control valve linked to the input member and movable thereby to eifect alternative pressure and exhaust connections to said actuator and thereby to effect movement of said output member in a direction and to an extent deter mined by the movement imparted to the input member,- a collapsible member linked to the input member and arranged to collapse, on seizureof the control valve, as the result of abnormal manual efiort appliedto the input member, a condu it for allowing of free circulation of liquid within the actuator, a valve normally closing said conduit, means responsive to collapse of said collapsible member for efiecting automatic opening of said valve, and means operative on collapse of the collapsible member associated with either actuator to lock against collapse the collapsible member associated with the other actuator- 4.
  • a combination as claimed in claim 1, comprising a housing having parallel bores, a member mounted to slide in each bore, said members being coupled respectively to the collapsible members of the two actuators and each of said sliding members being normally restrained by its associated collapsible member against movement in its bore but being arranged to slide in said bore on collapse of said collapsible member, a pair of locking bolts mounted to slide in bores in said housing extending transversely to the bores containing said slidable members, and a spring acting on each locking bolt, each of said locking bolts having a head normally held by its associated spring in engagement with a correspondingly shaped groove in one of said slidable members and being adapted to be displaced against its spring, by sliding movement of said member in relation to the housing, into position to lock the other slidable member positively against sliding movement in relation to the housing.
  • a combination as claimed in claim 1, comprising a housing having parallel bores, a member mounted to slide in each bore, said members being coupled respectively to the collapsible members of the two actuators and each of said sliding members being normally restrained by its associated collapsible member against movement in its bore but being arranged to slide in said bore on collapse of said collapsible member, a pair of locking bolts mounted to slide in bores in said housing extending transversely to the bores containing said slidable members, and a spring acting on each locking bolt, each of said locking bolts having a head normally held by its associated spring in engagement with a correspondingly shaped groove in one of said slidable members, having a square head at its other end and being adapted to be displaced against its spring, by sliding movement of said grooved slidable member, ,to engage its square head with a square groove in the other slidable member and so look said other slidable member positively against movement in relation to said housing.
  • a combination as claimed in claim 1, comprising a housing having parallel bores, a member mounted to slide in each bore, said members being coupled respectively to the collapsible members of the two actuators and each of said sliding members being normally restrained by its associated collapsible member against movement in its bore but being arranged to slide in said bore on collapse of said collapsible member, a pair of locking bolts mounted to slide in bores in said housing extending transversely to the bores containing said slidable members, a spring acting on each locking bolt, each of said locking bolts having a head normally held by its associated spring in engagement with a correspondingly shaped groove in one of said slidable members and being adapted to be displaced against its spring, by sliding movement of said member in relation to the housing, into position 'to lock the other slidable member positively against sliding movement in relation to the housing, and a pair of spring loaded latches for respectively latching said bolts against movement from their displaced positions.
  • a combination as claimed in claim 1, comprising, in association with each collapsible member, a, displaceable bolt engaging a groove in said member, a locking bolt, a spring normally holding said locking bolt out of engagement with another groove in said collapsible member, normally ineffective electromagnetic means for moving said locking bolt to locking position, and a switch associated with the displaceable bolt, said switch being actuated on displacement of said displaceable bolt as a result of collapse of its associated collapsible member, to complete a circuit to energize the electromagnetic device associated with the other collapsible member and thereby cause movement into locking position of the locking bolt associated with said other collapsible memher.
  • a combination as claimed in claim 1, comprising, in association with each collapsible member, a displaceable bolt engaging a groove in said member, a locking bolt, a spring normally holding said locking bolt out of engagement with another groove in said collapsible member, normally inefiective electromagnetic means for moving said locking bolt to locking position, and a switch associated with the displaceable bolt, said switch being actuated on displacement of said displaceable bolt as a result of collapse of its associated collapsible member, to complete a circuit to energize the electromagnetic device associated with the other collapsible member and thereby cause movement into locking position of the locking bolt associated with said other collapsible member, and further comprising a pair of spring loaded latches for respectively latching said looking bolts against movement from their locking positions.

Description

May 20, 1952 F. MOTT 3 3 HYDRAULIC SERVOMOT OR AND THE LIKE Filed May 27, 1950 4 Sheets-Sheet 1 ZIIXI ms y 20, 1952 L. F. MOTT 2,597,361
HYDRAULIC SERVOMOTOR AND THE LIKE Filed May 27, 1950 4 Sheets-Sheet 2 May 20, 1952 F. MOTT 2,597,361
HYDRAULIC SERVOMOTOR AND THE LIKE Filed May 27, 1950 4 Sheets-Sheet 5 y 20, 1952 F. MOTT HYDRAULIC SERVOMO'I'OR AND THE'LIKE 4 Sheets-Sheet 4 Filed May 27, 1950 Patented May 20, 1952 UNITED STATES ATENT OFFICE HYDRAULIC SE'RVOMOTOR, AND THE LIKE Application May'27, 1950, Serial'No. 164,759 In Great Britain JuneZ, 1949 8 Claims. 1
Certain types of hydraulic jacks and motors are controlled by a control valve, which controls the rate and direction of the supply of liquid under pressure to produce movement of an output member in a direction and to an extent determined by the movement imparted to the control valve by a manually operable input member. When such servomotors are used for the directional control of aircraft, ships or vehicles it is necessary to take precautions against failure of the servomotor to move in response to the operators signal, or continued movement in a contrary direction to that desired by the operator, as a result of seizure of the. control valve. Provision for this may be made by connection of the manually operable input member, by which movement is imparted to the control valve, to a collapsible link which will collapse under the extra force applied to the input member in the event of seizure of the control valve, and thereby actuate mechanism for rendering the servomotor ineffective, despite continued seizure of its control valve, to prevent movement of the output member to the desired position, either manually or by means of another servomotor. In United States application Serial No. 164,654 there is described an arrangement of this character, in which collapse of the collapsible link operates a valve to cut off the pressure supply to the'control valve and establish a connection between the opposite ends of the jack or motor.
As a precaution against loss of control due'to failure of the supply of liquid under pressure, or any functional defect except seizure of the output member, two identical servomotors with separate sources of pressure supply may be coupled to a single output member, the control valves of both servomotors being controlled by a common input member and each control valve being associated with a collapsible link arranged, when it collapses, to render the associated servomotor ineifective to prevent positioning of the output member by the other servomotor. When, however, either of the collapsible links operates, the associated servomotor loses its irreversibility. Operation of the remaining collapsible link, again as a result of valve seizure, will result in a complete loss of irreversibility and, where the output forces are so large as to render manual force insignificant, loss of control.
The probability of the two collapsible links collapsing in succession during a fiight of an aircraft is small, but as the results are soserious it is probably less hazardous to prevent the second link from collapsing and to rely on thepilots ability to free the second seized valve by appli- '2 cation of manual force to the input member. If this procedure isadopted, the pilot at least has a chance of remedying matters if the second control valve seize partially.
The invention accordingly provides the com- .bination, with a manually operable input member and an output member, of a pair of hydraulic actuators (i. e. jacksor motors) arranged normally to cooperate in maving the output member in a direction and to a position determined by the movement imparted to the input member, each actuator having a control device linked to the input member and a collapsible member arranged to collapse on seizure of the control device, torender the actuator inefiective to prevent movement of the output member by the other'actuator, and means operative on collapse of either member to lock the other member against collapse.
In the cases hereinafter described with reference to the drawings, the control devices of the actuators are constituted by control valves. In some cases, however, the actuators may be controlled byvariable stroke hydraulic pumps so as I to position the output member in accordance with the position assumed by the input member.
Where hydraulic jacks are used of the type described in United States application No. 785,887., now Pat. No. 2,566,273 issued August 28, 1951 ,v so that they are irreversible in the event of pressure failure, the jacks may derive pressurefrom the same source, provided provision is'made, in the-event of collapse of either member, for-cutting off the pressure supply from the control valve of the aifected jack. I prefer, however, to provide a separate source of pressurefor each jack.
some embodiments of the invention will now be described in detail, byway of example, with reference to the accompanying drawings, in
which:
Fig. 1 shows a purely mechanical interlock between the two collapsible members,
Fig. 2 shows an electromagnetically operated interlock between the two collapsiblemembers.
Figs; 3 and-3a are diagrams showing the application or the interlock of Fig. 1 tea system embodying duplicated hydraulicmotors.
Like reference numerals indicate like. parts throughout the figures.
It will be convenient first to describe the system shown in Figs. 3 and 3 thereafter to describe in detail the forms of interlock shown in Figs. 1 and 2. p
In the arrangement shown in Fig. 3, two hydraulic motors 83, 83 serve to operate a control surface. Parts associated with the servomotor 83 bear the same reference numerals as corresponding parts associated with the servomotor 83, with the addition of the suflix a.
The pilot's input member 29 is connected to a link 84 which, on movement of the input member, turns about a pivot 85 to shift a linkage 88, 81, 81, I81, I81, thereby moving the two control valves 36, 36 in the same direction.
But one of the hydraulic motors, 83, will be described, the other 83 being of precisely similar construction. The motor 83 comprises a shaft 88, carrying a pair of eccentrics 89, 90 spaced at 180 (1. e. in antiphase) on the shaft. Associated with the eccentric 89 is a set of six cylinders, each containing a piston 9|, these cylinders being located radially in relation to the shaft 88. A similar set of six cylinders each containing a piston 92, is associated with the eccentric 90. Associated with each aligned pair of cylinders is one of six distributing valves 93, each of which is held by a spring 94 in contact with a swashplate 95 on the shaft 88. For simplicity but one pair of aligned cylinders, containing pistons 9|, 92, and but one associated distributing'valve 93, are shown in Fig. 3 The motor has a drain connection I83 for leading :away liquid which may leak past the pistons 9|,
92 or the distributing valves 93.
Pressure is supplied, from an inlet 31,via a normally open valve I80 to an inlet port 40 associated with the control valve 36. The valve 38 also controls outlet ports 41 connected to an exhaust outlet 46.
'leading'to each of the distributing valves 93.
This results in sympathetic movement of the pistons Ill, 92 thereby actuating the eccentrics 89,90 to rotate the shaft 88 in a direction determined by the direction of movement of the control valve 38. Thus, if line 98 is connected to pressure, and line 91 to exhaust, the piston 92 will be caused to move in and the piston 9| to move out. As the shaft 88 rotates, the swashplate 95 imparts continuous reciprocating movement to all of the valves 93 so that the associated pistons BI, 92 will be alternately connected, at the proper times, to pressure and exhaust.
The shafts 88, 88 of the two motorsdrive,
through gear wheels 98, 98 a common gear wheel 99 connected, by bevel gearing I to a threaded sleeve IOI, engaging a pair of screw jacks I02 which are moved inwards or outwards, according to the direction of rotation of the member IN, to impart movement to the two portions of the control surface, not shown.
In screw threaded engagement with the boss of the gear wheel 99 is a follow-up rod I03 which operates, by rocking the link 84 about its pivotal attachment I04 to the input member 29, to return the control valves 36, 36 to neutral position.
The collapsible member 23 is of the construction described in United States application Serial No. 164,653 and comprises a tube mounted to slide in a housing 22, a number of balls 53 which project through holes in the tube and into holes 56 in the housing, and a plunger 52 having a conical head 51 which is held by a compression spring 54 in position to hold the balls 53 in the position shown. Normally a catch 65 on the tube 5I coacts with a catch 11 associated with the valve I60 to hold the valve open against the action of its spring 18 as shown.
If the valve 36 should seize, the force exerted by the pilot on the input member 29 will cause the member 23 to collapse, as described in United States application Serial No. 164,653. The follow ing sequence of events will then occur:
The catch 11 will be freed, allowing the valve I60 to be closed by the spring 18. This cuts off pressure from the control valve 35, and also from a line I05. As long as there is pressure in the line I05, a plunger I00 is held, against the action of a spring I91, to maintain contacts I08, I09 closed. When the pressure is cut off, the spring I01 causes the contacts I08, I09 to be separated, thereby lighting a warning lamp. When the valve I68 closes, its stem I It) moves into position to open a connection between the lines 98, 91, thereby allowing the hydraulic motor 83 to run freely, as it is driven through the gears 99, 98, on continued operation of the still effective motor 83 On seizure of the control valve 30 a precisely similar action takes place. The member 23 collapses and the valve I60 closes, to cut off pressure from the valve 36*, to energize the associated warning lamp, and to connect together the lines 98, 91
Interlocking bolts I I I, III extend between plungers H2, 2 constituting extensions of the tubes 5I, 5| of the two collapsible members and their function and operation will now be described with reference to Fig. 1. Within the plungers II2, 2 are disposed resetting plungers 58, 58 for the collapsible members which operate as described in United States application Serial No.
contained in housings 25, 25 by linkages 281,
281 Each of the plungers II2, I I 2 may be normally prevented from moving in relation to the housing 22 by a shear pin, instead of by a resettable collapsible member of the kind shown in Fig. 3.- The two locking bolts III, III are of identical construction. One only will therefore be described. The plunger I II has, at one end, a rounded head 4 which is held by a spring 5 in engagement with a rounded groove 8 in the plunger I I2 and at the other end a square head 1 which is held, by the spring 5, clear of a square groove 8* in the plunger I I 2. The rounded heads 4, 4 of the two bolts face in opposite directions,
the head 4 of the bolt III normally engaging the roundedgroove 6 in the plunger H2 When either plunger I I2, II2 moves axially, in response to an excessive load, the rounded head 4 or 4 of the bolt engaging it is forced out of the rounded groove 6 or 8 in the plunger, and the square end 1 or 1 of that bolt engages the corresponding groove 8 or 8 in the other plunger to lock the other plunger against axial movement. When either bolt is so moved into locking position, a pin 9 or 9 loaded by a spring In or I0. snaps into a recess II or II in the bolt to hold .it in locking position. 7
Thus, while both plungers I I2, I I 2 are initially free to collapse, collapse of either will move one by de-energising the solenoid 6|.
g or the locking bolts to hold the other against collapse.
This type of interlock can only conveniently be usedwhere the two actuators are actuated (fairly close together. If it is desired to place the actuators further apart, e. g. at opposite ends of an aircraft control surface, the interlock may be efiected'electrically, as shown in Fig. 2.
In this arrangement, each of the locking bolts is divided into two parts. As the locking bolts are of identical construction, but one will be described. Corresponding parts of the other are given the same reference numerals, plus the sufiix a. The locking bolt comprises a part 2 havinga rounded head 4 urged by the spring 5 into engagement with the square groove 8 in the other plunger 12, and a part 3H having a square head I which is normally held by a spring l5 out of engagement with the square groove 8 in the other plunger 2 The part 3 abuts at its upper end against a core '60, disposed in a solenoid SI and attached to the part 3 is a rod l2 of insulat-i-ng material which passes upwardly through the core 60. The core 60 and rod 12 each carry one of a pair of contacts l9 which are normally held closed by a spring l5.
When the plungerllZ is displaced axially, it forces the part 2 inwards, against its spring 5, into position to make a pair of contacts l3,
the-part 2H being locked in this position by entry, into a groove M in it, of a bolt l8 loaded by a spring 11.
Closure of the contacts 13 completes a circuit between leads l8, and normally closed contacts 19, 20 to energise the solenoid 6|. This attracts the core 60 and forces the part 3 outwardly to the locking position in which its head 1 engages the groove 8 in the plunger 2 A bolt 2| is then forced inwards, by a blade spring 320 supporting one of the contacts 28, to engage a groove l2| in the part 3 to hold the latter in looking position. Movement of the bolt 2| to locking position opens the contacts 20, there- The core 69 of the solenoid will then be moved, by its spring H5, to carry its associated contact l9 away from the other contact l9 which is mounted on the rod l2 fixed to the member 3| I. This prevents restoration of the flow of current through the solenoid should partial contact subsequently take place at the contacts 20.
What I claim as my invention and desire to secure by Letters Patent is:
l. The combination, with a manually operable input member and an output member, of a pair of hydraulic actuators coupled to said output member, each of said actuators comprising a control device linked to the input member and movable by said input member in opposite directions to efiect through the agency of the actuator movement of said output member in a dimotion and to an extent determined by the movement imparted to the input member, a collapsible member linked to the input member and arranged to collapse, on seizure of the control device, as the result of abnormal manual efiort applied to the input member, means responsive to collapse of said collapsible member for rendering the actuator ineffective to prevent continued actuation of the output member by the other actuator under control of the input member, and means operative on collapse of the collapsible member associated with either actuator to lock against collapse the collapsible member associated with the other actuator.
2-; The combination, with a manually operable input member and an output member, of a pair of hydraulic actuators coupled to said output member, each of said actuators comprising a control valve linked to the input member and movable thereby to efiect alternative pressure and exhaust connections tosaid actuator and thereby to effect movement of said output member in a direction and to an extent determined by the movement imparted to the input member, a collapsible member linked to the input member and arranged to collapse, on seizure of the control valve, as the result of abnormal manual effort applied to the input member, means responsive to collapse of said collapsible member for rendering the actuator ineffective to prevent continued actuation of the output member by the other actuator under control of the input member, and means operative on collapse of the collapsible member associated with either actuator to lock against collapse the collapsible member associated with the other actuator.
3. The combination, with a manually operable input member and an output member, of a pair of hydraulic actuators directly coupled to said output member, each of said actuators comprising a control valve linked to the input member and movable thereby to eifect alternative pressure and exhaust connections to said actuator and thereby to effect movement of said output member in a direction and to an extent deter mined by the movement imparted to the input member,- a collapsible member linked to the input member and arranged to collapse, on seizureof the control valve, as the result of abnormal manual efiort appliedto the input member, a condu it for allowing of free circulation of liquid within the actuator, a valve normally closing said conduit, means responsive to collapse of said collapsible member for efiecting automatic opening of said valve, and means operative on collapse of the collapsible member associated with either actuator to lock against collapse the collapsible member associated with the other actuator- 4. A combination as claimed in claim 1, comprising a housing having parallel bores, a member mounted to slide in each bore, said members being coupled respectively to the collapsible members of the two actuators and each of said sliding members being normally restrained by its associated collapsible member against movement in its bore but being arranged to slide in said bore on collapse of said collapsible member, a pair of locking bolts mounted to slide in bores in said housing extending transversely to the bores containing said slidable members, and a spring acting on each locking bolt, each of said locking bolts having a head normally held by its associated spring in engagement with a correspondingly shaped groove in one of said slidable members and being adapted to be displaced against its spring, by sliding movement of said member in relation to the housing, into position to lock the other slidable member positively against sliding movement in relation to the housing.
5. A combination as claimed in claim 1, comprising a housing having parallel bores, a member mounted to slide in each bore, said members being coupled respectively to the collapsible members of the two actuators and each of said sliding members being normally restrained by its associated collapsible member against movement in its bore but being arranged to slide in said bore on collapse of said collapsible member, a pair of locking bolts mounted to slide in bores in said housing extending transversely to the bores containing said slidable members, and a spring acting on each locking bolt, each of said locking bolts having a head normally held by its associated spring in engagement with a correspondingly shaped groove in one of said slidable members, having a square head at its other end and being adapted to be displaced against its spring, by sliding movement of said grooved slidable member, ,to engage its square head with a square groove in the other slidable member and so look said other slidable member positively against movement in relation to said housing.
6. A combination as claimed in claim 1, comprising a housing having parallel bores, a member mounted to slide in each bore, said members being coupled respectively to the collapsible members of the two actuators and each of said sliding members being normally restrained by its associated collapsible member against movement in its bore but being arranged to slide in said bore on collapse of said collapsible member, a pair of locking bolts mounted to slide in bores in said housing extending transversely to the bores containing said slidable members, a spring acting on each locking bolt, each of said locking bolts having a head normally held by its associated spring in engagement with a correspondingly shaped groove in one of said slidable members and being adapted to be displaced against its spring, by sliding movement of said member in relation to the housing, into position 'to lock the other slidable member positively against sliding movement in relation to the housing, and a pair of spring loaded latches for respectively latching said bolts against movement from their displaced positions.
'7. A combination as claimed in claim 1, comprising, in association with each collapsible member, a, displaceable bolt engaging a groove in said member, a locking bolt, a spring normally holding said locking bolt out of engagement with another groove in said collapsible member, normally ineffective electromagnetic means for moving said locking bolt to locking position, and a switch associated with the displaceable bolt, said switch being actuated on displacement of said displaceable bolt as a result of collapse of its associated collapsible member, to complete a circuit to energize the electromagnetic device associated with the other collapsible member and thereby cause movement into locking position of the locking bolt associated with said other collapsible memher.
8. A combination as claimed in claim 1, comprising, in association with each collapsible member, a displaceable bolt engaging a groove in said member, a locking bolt, a spring normally holding said locking bolt out of engagement with another groove in said collapsible member, normally inefiective electromagnetic means for moving said locking bolt to locking position, and a switch associated with the displaceable bolt, said switch being actuated on displacement of said displaceable bolt as a result of collapse of its associated collapsible member, to complete a circuit to energize the electromagnetic device associated with the other collapsible member and thereby cause movement into locking position of the locking bolt associated with said other collapsible member, and further comprising a pair of spring loaded latches for respectively latching said looking bolts against movement from their locking positions.
LAWRENCE FARNELL MO'I'I.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,315,110 Dornier Mar. 30, 1943 FOREIGN PATENTS Number Country Date 582,380 Great Britain Nov. 13, 1946
US164759A 1949-06-02 1950-05-27 Hydraulic servomotor and the like Expired - Lifetime US2597361A (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2706886A (en) * 1950-06-14 1955-04-26 Honeywell Regulator Co Coordinated hydraulic control apparatus
US2821068A (en) * 1955-02-09 1958-01-28 British Messier Ltd Servo systems
US2984212A (en) * 1959-09-02 1961-05-16 Western Electric Co Positioning device for moving a member to selected positions
US2995014A (en) * 1960-04-26 1961-08-08 Bell Aerospace Corp Dual electro-hydraulic servo actuator system
US3003719A (en) * 1957-09-27 1961-10-10 Sperry Gyroscope Co Ltd Control apparatus for aircraft
US3011740A (en) * 1954-10-25 1961-12-05 Honeywell Regulator Co Hydraulic control apparatus for aircraft flight control apparatus
US3070071A (en) * 1960-03-11 1962-12-25 North American Aviation Inc Failure protected signal translating system
US3240275A (en) * 1963-12-03 1966-03-15 Curtiss Wright Corp Hydraulically operable pitch aircraft propeller
US3641833A (en) * 1969-09-30 1972-02-15 Boeing Co Mechanical amplifier

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2315110A (en) * 1938-09-14 1943-03-30 Dornier Claude Control apparatus for aircraft
GB582380A (en) * 1944-09-28 1946-11-14 Fairey Aviat Co Ltd Improvements in or relating to means for controlling the synchronous operation of a plurality of hydraulic jacks

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2315110A (en) * 1938-09-14 1943-03-30 Dornier Claude Control apparatus for aircraft
GB582380A (en) * 1944-09-28 1946-11-14 Fairey Aviat Co Ltd Improvements in or relating to means for controlling the synchronous operation of a plurality of hydraulic jacks

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2706886A (en) * 1950-06-14 1955-04-26 Honeywell Regulator Co Coordinated hydraulic control apparatus
US3011740A (en) * 1954-10-25 1961-12-05 Honeywell Regulator Co Hydraulic control apparatus for aircraft flight control apparatus
US2821068A (en) * 1955-02-09 1958-01-28 British Messier Ltd Servo systems
US3003719A (en) * 1957-09-27 1961-10-10 Sperry Gyroscope Co Ltd Control apparatus for aircraft
US2984212A (en) * 1959-09-02 1961-05-16 Western Electric Co Positioning device for moving a member to selected positions
US3070071A (en) * 1960-03-11 1962-12-25 North American Aviation Inc Failure protected signal translating system
US2995014A (en) * 1960-04-26 1961-08-08 Bell Aerospace Corp Dual electro-hydraulic servo actuator system
US3240275A (en) * 1963-12-03 1966-03-15 Curtiss Wright Corp Hydraulically operable pitch aircraft propeller
US3641833A (en) * 1969-09-30 1972-02-15 Boeing Co Mechanical amplifier

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