US1806669A - Remote control mechanism - Google Patents

Remote control mechanism Download PDF

Info

Publication number
US1806669A
US1806669A US335956A US33595629A US1806669A US 1806669 A US1806669 A US 1806669A US 335956 A US335956 A US 335956A US 33595629 A US33595629 A US 33595629A US 1806669 A US1806669 A US 1806669A
Authority
US
United States
Prior art keywords
valve
starting
stop
maneuvering
ports
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US335956A
Inventor
Charles A Campbell
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
New York Air Brake LLC
Original Assignee
New York Air Brake LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by New York Air Brake LLC filed Critical New York Air Brake LLC
Priority to US335956A priority Critical patent/US1806669A/en
Application granted granted Critical
Publication of US1806669A publication Critical patent/US1806669A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • 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
    • Y10T74/19Gearing
    • Y10T74/19219Interchangeably locked
    • Y10T74/19293Longitudinally slidable
    • Y10T74/19298Multiple spur gears
    • Y10T74/19326Fluid operated

Definitions

  • This invention relates to remote control devices and embodies features of general applicability in remote control installations, but will be described as applied to a remote (5 control for marine Diesel engines.
  • the control is of the pneumatic type which is peculiarly suitable for use with Diesel engines because compressed air is customarily used to start such engines, and consequently is usually available.
  • the present remote control mechanism is so contrived as to permit alternative control from a plurality'of stations, three being i1- lustrated in the drawings, one, for example,
  • the device is applicable in the form shown to any engine or engines having a five-position maneuvering gear.
  • gears there is a neutral or mid-position in which the engine stops, a forward starting position and a rearward starting position in which the engine is put into motion in respectively opposite directions by compressed air admitted directly to one or more of the cylinders, and a forward running position and a reverse running position in which fuel is admitted to all the cylinders in relatively reverse sequences according to the firing order of the cylinders.
  • Starting gears for internal combustion engines, and particularly Diesel en ines differ among themselves in the num r of engine cylinders which receive starting air and in the manner in which the valve action is modified to distribute the starting air, and in other details; but these features are not elements of the resent invention, the present control gear eing available, in the specific form illustrated, for use with any fiveposition starter regardless of how this starter may function, or for use to control any five position device.
  • the invention contem- I plates a movable elementwhich is shifted to five different positions by the concurrent action of two opposed sets each comprising two fluid pressure ex ansible chamber motors (for example cy inders with pistons).
  • two opposed sets each comprising two fluid pressure ex ansible chamber motors (for example cy inders with pistons).
  • one cylinder of each set is fixed and the other cylinder is mounted on the piston of the first cylinder.
  • a spring mechanism shifts the starting mechanism to stop position.
  • both cylinders of either pair are subject to pressure the starting mechanism is shifted to one or the other starting position, and when thereafter one of the cylinders of the energized pair is exhausted the starting mechanism is shifted to the corresponding running position.
  • the above mechanism is controlled by any one of a plurality of control valves.
  • Each of the control valves has four positions in which the four cylinders are charged or exhausted in different relations as'just outlined and a lap position in which all portsin the valve are blanked so that the pressure condition last established is permanently maintained. It is contemplated that each.
  • control valve will be equipped to receive a removable handle or actuator, and'that a guard will be provided so that this handle can be removed and applied only when the valve 18 in lap position. From this it follows that any control valve which is put out of action by the removal of its handle must be left in lap position, so. as not to interfere with the controlling action of other control valves. By limiting the number of handles to one or two the chance of conflicting manipulation of control valves may be eliminated or reduced as occasion may reuire.
  • the motion of the valve to lap position does not stop the engme, but the controlling handle is so arranged that in lap position, and in lap positiononly, it ma be manipulated to open a vent valve associated with the control valve wh ch exhausts any 0 linder or cylinders which may be charged and thus stops the engme.
  • Fig. l is a vertical axial section of a starter shifting mechanism equipped with one control valve adjacent the mechanism and two remote control valves, the parts hein shown in astern starting position.
  • Fig. 2 is a vertical axial section of the double check valve controlling the exhaust.
  • Fig. 3 is a vertical axial section of a quick exhaust valve used, on the motor cylinders of the device.
  • Fig. 4 is a plan view partly in section showing one of the remote control valves.
  • Fig. 5 is a vertical axial section of one of the remote control valves showing it in lap position.
  • Fig. 6 is a fragmentary view of the rotary valve and valve seat forming parts of the valve of Fig. 5 but showing them in the astern starting position.
  • Fig. 7 is a similar 1 view showing the astern running position.
  • Fig. 8 is a similar view showing the ahead starting position.
  • Fig. 9 is a similar view showing the ahead running position.
  • Fig. 10 is a diagrammatic view showing the positions taken by the motor parts in astern running sition.
  • Fig. 11 is a similar view showing astern startlng position.
  • Fig. 12 is a similar view showing stop position.
  • Fig. 13 is a similar view showing ahead starting position.
  • Fig. 14 is a similar view showing ahead runnmg position.
  • Figs. 1 to 9 inclusive is diagrammatic to the extent that the ports are drawn as if they all lay in a single plane of section, according to a convention familiar in the pneumatic control art and adopted to permit the tracing of the flow paths throughout the drawings.
  • the exact layout of the ports is immaterial to the invention,
  • 16 represents a shaft formmg part of the engine starting gear.
  • the two extreme rotary ositions of the shaft 16 are those correspon ing to the starting functions of the engine (in reverse directions).
  • the shaft turns about 190 in passing from one to the other.
  • the stop position is intermediate the two starting positions and thus approximately at 95 to each.
  • the two running positions are displaced on opposite sides of the stop position 30 or less. These angular displacements are mentioned merely as characteristic of one typical gear with which the controlling mechanism may be used.
  • a gear 17 Swiveled on the shaft 16 is a gear 17 which might be fast on the shaft, but which in the example illustrated, is releasably clutched thereto by a dental clutch, part of which appears at 18.
  • This clutch is asymmetric as to its engaging jaws so that the gear ma be clutched to the shaft 16 only in one de nite angular relation to the shaft.
  • the gear 17 meshes with a rack 19 formed on a longitudinally sliding piston rod 21.
  • the piston rod 21 is guided in a sleeve hushing 22 fixedly locked in the main casting 23 by nuts 24 and held against rotation therein by a stud 25.
  • the stud 25 has also a tongue which enters a keyway 20 in the piston rod 21 and holds this rod against rotation.
  • Formed on the casting 23 are two oppositely directed tubular extensions 26, each of which carries at its end an annular stop nut 27. This stop nut 27 limits the outward motion of respective plunger thimbles 28 which are urged to their outward position by coil springs 29.
  • the piston rod 21 passes through the ends of the thimbles 28 and is provided at opposite ends with identical pistons 31R and 31A.
  • Each piston 31A, 31R is provided with a peripheral cup leather 32 and is slidable in a corresponding movable cylinder 33 which is formed as an extension on an inner piston 34A or 34R respectively.
  • the pistons 31A, 31R are each single acting, the space between the two pistons bein vented to atmosphere.
  • the pistons 34A, 34 have each a peripheral packing cup leather 35 and each works in a corresponding fixed cylinder 36 whlch is supported by the main casting 23.
  • the outer ends of the cylinders 36 are closed by heads 37.
  • Each cylinder 33 is really a tubular extension on the piston 34A or 34R and has an outside diameter less than the diameter of such piston.
  • the pistons 34A and 34R are really each a single acting piston, the annular space 39 not entering as a material factor in the force exerted on the piston. Instead, each annular space serves merely as a part of the connection to the working space of the corresponding cylinder 33. This is a convenient way of maintaining this connection regardless of the position 0 piston 34.
  • each of the pistons 34A, 34R there is a check valve 30 opening to permit flow from the space in cylinder 33 to the space in cylinder 36.
  • Fig. 1 shows two remote control valves and one engineers control valve ad jacent the starter shiftin mechanism. These are desi nated on Fig. 1 by the letters RC#1, R #2 for the two remote control valves and EC for the engineers control valve. RC#1 and RC#2 are shown in lap osition, the handle being removed from C#1 and applied to RC#2. Most of the handle of EC is invisible in Fig. 1, being forward of the plane of section, but it will be understood that the use of a handle on EC at all times is contemplated on the theory that it is advisable to permit control by the engineer at any time.
  • valves EC, RC#1 and RC#2 are essentially identical'except that EC is provided with a double check valve which serves all three valves and hence is not duplicated. It might'be located in any of the three.
  • ach includes as a base member a pipe bracket 44 to which all pipe connections are made, a superposed ported valve seat member 45, a removable cap 46 to which the pressure supply is admitted, and a rotary valve 47 which controls the ports in the said seat.
  • the rotary valve 47 may be rotated to its various positions by a removable handle 49 which has a spring plunger latch 51 coacting with a notched sector 52 fixedly supported on the cap 46.
  • An arcuate guard 57 is provided and prevents the removal of the member 49 except when the valve 47 is in lap position, lap position being that in which all the ports in the seat are closed by the rotary valve (see Fig. 5).
  • the member 49 is not strictly the handle member but instead a hand grip 58 is pivoted at 59 on the member 49 so as to swing in a vertical plane.
  • This carries a downward extending arm 61 which in lap position may engage the protruding stem of a valve 62 and force the same open against the resistance of its spring 63 and the pressure sustained by the valve.
  • the yalve 62 is the stop valve and is a novel feaare.
  • This arrangement is to allow the control valves to be moved to lap position without stopping the engine and et to provide for the stopping of the engine wh le the valves are in lap position and only while they are in lap position.
  • valve EC in Fig. 1, the analogue of the pipe head member used on RC#1 and RC#2 is formed directly in the castlng 23. It has already been stated that the ports in the member 45 are continuations of ports in the member 44. It will also be apparent from an inspection of Fig. 1 that as to the valve EC the ports are extensions of ports formed in the casting 23. Connections between the pipe brackets 44 and the casting 23 are made by pipes, but to avoid confusion by the use of an excessive number of references, a single continuous passage will be indicated by a single reference numeral.
  • Alr 1s supplied to the space within the caps 46 by a supply passage 65 This is fed from a reservoir 66 maintained charged at a uniform pressure by any suitable means, not shown.
  • the reservoir may be provided with a pressure gage 67, a drain cock 68 and a stop cock 69 may be inserted in the pipe connecting the reservoir with the line 65.
  • passages 71, 72, 73 and 74 all lead from the seats of all three rotary valves 47 to the four working cylinder spaces, as follows: 71 leads to the space to the left of the piston 34A. 72 leads to the space to the left of the piston 31A. 73 leads to the space to the right of the piston 34R and 74 leads to the space to the valves. There are also extensions of passages- 71 and 73 leading to these faces. These extensions are blanked off in the case of RC#1 and RC#2 by cover plates 78 and gaskets 79, but in the case of the valve EC there is a double check valve whose body is indicated generally by the numeral 81. This valve is illustrated in Fig. 1 and is shown on an enlarged scale in Fig. 2.
  • the body 81 has a cap 82 and the two together house a cylindrical valve bushing 83 in which is longitudinally slidable a check valve element 84.
  • This has sealing gaskets 85 on its ends which coact alternately with annular valve seats 86 and 87.
  • the valve functions, as will be apparent, to connect either passage 71 or 73 with the passage 76 controlled by the valves 62.
  • the passages 71 and 73 are connected respectively to the working space to the left of piston 34A and the working space to the right of piston 34R.
  • the valve 84 shifts to connect the passage 76 to whichever one of these working spaces is at the time charged. Since only one is charged at a time, the valve 84 operates to place which ever one is charged under control of the valves 62.
  • valves 62 When opened will operate to vent the charged workmg space and allow the mechanism to move to engine stopping position. If working spaces of cylinders 33 and 36 are both charged, as occurs in starting position, the exhaust of 36 will also exhaust 33 through a check valve 30.
  • each rotary valve 47 is provided with recesses 91, 92 and through ports 93, 94 and 95, which serve to subject pistons 31R and 34R to pressure and vent pressure acting against pistons 31A and 34A (Fig. 6) subject piston 34R to pressure and vent pressure acting against p stons 31R, 31A and 34A (Fig. 7) sub ect pistons 31A and 34A to pressure and vent pressure acting against pistons 31R and 34R (Fig. 8) or subject piston 34A to pressure and vent pressure acting against pistons 31A, 31R and 34R (Fig. 9).
  • Pressure acting against plstons 34A and 34R is manually vented by the valves 62, and if either piston 31A or 31R is subject to pressure, this will be vented by check valve 30 in piston 34A or 34R.
  • each of the passages 71, 72, 73 and 74 serves as a combined supply and exhaust port for pressure fluid flowing to and from the working spaces of the respective cylinders.
  • a quick release valve is interposed in each of the passages adjacent the working space served by the passage, the quick release valve being so arranged that it closes a local exhaust when flow toward the working space occurs and opens it immediately that flow from the working space starts. This greatly accelerates the response of the mechanism.
  • Valve 96 is illustrated in detail in Fig. 3 and is typical of all the valves.
  • 96 is applied to the body of the valve and 101 represents a removable cap.
  • This has a guideway for the stem 102 of a check valve 103 which opens, inward and is guided by its pilot 104 into and out of seating engagement with the seat 105.
  • Seat 105 surrounds a. port 106 leading to atmosphere.
  • the disk 108 is held upward by a spring 111 against the stop 107 and the parts are so arranged that when the valve 103 is seated and the disk 108 is against the stop 107, this disk is at about mid-length of the restricted cylindrical portion 109.
  • Valve 96 is interposed in the passage 71 and the connections are such that fiow from any control valve RC#1, RC#2 or EC toward the working space to the left of piston 34A will urge the valve 103 closed by .forcing the piston member 108 downward against spring 111.
  • reverse flow that is from the cylinder to a control valve and thence to exhaust, will act upward on the disk 108, unseat the valve 103 and open a large local exhaust from the working space.
  • Fig. 4 indicates the five positions of the control valves corresponding to Figs. 5 to 9 inclusive.
  • the device operates as follows:
  • the handle 58 is swung clockwise (i elatively to Fig. 4) to its limiting position, which is astern starting position. This puts the rotary valve in the position of Fig. 6. In this position ports 71 and 72 are both connected to exhaust port and ports 73 and 74 receive air which is supplied to the space within cap 46 by passage 65. This action occurs no matter which one of the three control valves is manipulated. The effect is to charge the working spaces of pistons 31R and 34R, thus moving the piston rod to the extreme leftward position indicated in Figs. 1 and 11. This establishes the starting action of the engine starter and as soon as the engine is in proper motion the operator moves the handle 58 to astern running position. The effect of this as illustrated in Fig. 7 is to connect the port 74 also to atmoshere while maintaining the supply to port 3/ It follows that the space to the right of piston 31R is exhausted and the parts move to the position indicated diagrammaticall in Fig. 10.
  • Fbrward starting is effected in a similar manner by shifting first to ahead starting osition to establish the connections shown In Fig. 8 which admits pressure against pistons 31A and 34A, as indicated in Fig. 13,
  • valves RC# 1, RC#2 or EC may be manipulated to produce the above result. If the control is to be maintained at the station at which starting was effected the valve will be left in running position, but if control is to be transferred to another valve the handle is swung to lap position, removed, transferred to the selected other control valve, which is then shifted to running position to preclude loss of pressure through gradual leakage. Whenever it is desired to stop the engine, the control valve is swung to lapposition and the handle 58 is depressed to open the valve 62. The effect is to vent the passage 76 and consequently whichever one of the passages 71 or 73 may then be connected to the passage 76 by the check valve 84:.
  • each of the two motors shall act cumulatively, each adding its increment of motion to that of the other, so that by charging one or both the necessary plurality of positions may be secured.
  • each engine might have its individual starter actuating mechanism. This might be subjected to common control by a single control valve or a single set of control valves. Ordinarily, however, on multiple screw vessels it is desired to start and stop individual engines inde endently for maneuvering purposes.
  • Means for actuating astarting gear having a starting position, a running position and a stop position comprising in combination two expansible chamber motors; means for connecting said motors with said gear whereby each motor may impart independently an increment of motion thereto; valve means operable selectively to admit pressure fluid to othmotors, to admit it to one and exhaust the other and to exhaust both; and
  • an exhaust valve associated with each motor and having actuating means in the path of flow of pressure fluid to and from the motor, and arranged to be shifted in a valve closing direction by flow toward the motor and in a valve opening direction'by flow from the motor.
  • Means for actuating a starting gearhaving forward and reverse starting position, forward and reverse running positions and a sto position comprising in combination a member adapted for connection with said gear; yielding means urging said member to stop position; a forward shifting unit and a reverse shifting unit, each of said units including two expansible chamber motors each connected to said member to impart independently an increment of motion thereto; and means controllable selectively to admit pressure fluid to both motors of one unit while exhausting the motors of the other unit, to admit it to one motor of one unit while exhausting the other motor of that unit and those of the other unit, and to exhaust all the motors.
  • Means for actuating a starting gear having forward and reverse starting position, forward and reverse running positions and a stop position comprising in combination a member adapted for connection with said gear; yielding means urging said member to stop position; a forward shift-ing unit and a reverse shifting unit, each of said units includingtwo expansible chamber motors, the

Description

May 26, 1931. c. A. CAMPBELL REMOTE CONTROL MECHANISM Filed Jan. 29, 1929 2 Sheets-Sheet l 29. 1929 2 Sheets-Sheet 2 AJTEEN JTAET AHEAD JTAET C. A. CAMPBELL REMOTE CONTROL MECHANISM Filed Jan.
May 26, 1931.
Patented .May 26, 1931 UNITED STATES PATENT OFFICE- CHARLI'B A. CAIDBELL, OF WATERTOWN, NEW YORK, ASSIGNOR TO THE NEW YORK AIR BRAKE COMPANY, A CORPORATION OF NEW JERSEY REMOTE CONTROL MECHANISM Applicatloi1 flled January 29, 1929. Serial No. 335,956.
This invention relates to remote control devices and embodies features of general applicability in remote control installations, but will be described as applied to a remote (5 control for marine Diesel engines. The control is of the pneumatic type which is peculiarly suitable for use with Diesel engines because compressed air is customarily used to start such engines, and consequently is usually available.
The present remote control mechanism is so contrived as to permit alternative control from a plurality'of stations, three being i1- lustrated in the drawings, one, for example,
to be located on the bridge or in the pilot house, another on the after-deck, and the third adjacent the engine. Obviously other locations are possible and there is nolimit to the number of control stations which may be provided. Furthermore, one set of stations may be used if desired for the simultaneous controlof the starting mechanisms of a plurality of engines.
Generally stated, the device is applicable in the form shown to any engine or engines having a five-position maneuvering gear. In such gears there is a neutral or mid-position in which the engine stops, a forward starting position and a rearward starting position in which the engine is put into motion in respectively opposite directions by compressed air admitted directly to one or more of the cylinders, and a forward running position and a reverse running position in which fuel is admitted to all the cylinders in relatively reverse sequences according to the firing order of the cylinders.
Starting gears for internal combustion engines, and particularly Diesel en ines, differ among themselves in the num r of engine cylinders which receive starting air and in the manner in which the valve action is modified to distribute the starting air, and in other details; but these features are not elements of the resent invention, the present control gear eing available, in the specific form illustrated, for use with any fiveposition starter regardless of how this starter may function, or for use to control any five position device.
of the five-position type and the invention can best be illustrated as so applied."
Generally stated the invention contem- I plates a movable elementwhich is shifted to five different positions by the concurrent action of two opposed sets each comprising two fluid pressure ex ansible chamber motors (for example cy inders with pistons). Preferably one cylinder of each set is fixed and the other cylinder is mounted on the piston of the first cylinder. The device chosen for illustration functions as follows:
When all four cylinders are exhausted a spring mechanism shifts the starting mechanism to stop position. When both cylinders of either pair are subject to pressure the starting mechanism is shifted to one or the other starting position, and when thereafter one of the cylinders of the energized pair is exhausted the starting mechanism is shifted to the corresponding running position.
The above mechanism is controlled by any one of a plurality of control valves. Each of the control valves has four positions in which the four cylinders are charged or exhausted in different relations as'just outlined and a lap position in which all portsin the valve are blanked so that the pressure condition last established is permanently maintained. It is contemplated that each.
control valve will be equipped to receive a removable handle or actuator, and'that a guard will be provided so that this handle can be removed and applied only when the valve 18 in lap position. From this it follows that any control valve which is put out of action by the removal of its handle must be left in lap position, so. as not to interfere with the controlling action of other control valves. By limiting the number of handles to one or two the chance of conflicting manipulation of control valves may be eliminated or reduced as occasion may reuire.
It will be observed that the motion of the valve to lap position does not stop the engme, but the controlling handle is so arranged that in lap position, and in lap positiononly, it ma be manipulated to open a vent valve associated with the control valve wh ch exhausts any 0 linder or cylinders which may be charged and thus stops the engme.
As there are two cylinders either of which may be charged in running position, and as it is desired to effect stopping by the operation of a single valve, use is made of a double check valve which connects the two cylinders selectively with the stop line according to which one is charged. This double check valve is an important feature of the invention.
It is necessary to provide only six control pipe lines, one for each of the four cylinders, one for the supply of motive fluid andthe sixth for the stop or cylinder venting function.
Since some of the control stations are remote from the engine, the volume of the various control lines is considerable, and the friction of flow through the long pipe lines is commonly such as to render the action of the device sluggish if the entire exhaust flows through the l1ne. Accordingly there is pro vided for each cylinder 9. quick release valve which upon the venting of the connected pipe volume functions to open a direct exhaust from the corresponding cylinder. In this way immediate complete response of the control mechanism is secured.
The preferred embodiment of the invention is illustrated in the accompanying drawings, in which,-
Fig. l is a vertical axial section of a starter shifting mechanism equipped with one control valve adjacent the mechanism and two remote control valves, the parts hein shown in astern starting position.
Fig. 2 is a vertical axial section of the double check valve controlling the exhaust.
Fig. 3 is a vertical axial section of a quick exhaust valve used, on the motor cylinders of the device.
Fig. 4 is a plan view partly in section showing one of the remote control valves.
Fig. 5 is a vertical axial section of one of the remote control valves showing it in lap position.
Fig. 6 is a fragmentary view of the rotary valve and valve seat forming parts of the valve of Fig. 5 but showing them in the astern starting position.
Fig. 7 is a similar 1 view showing the astern running position.
Fig. 8 is a similar view showing the ahead starting position. t
Fig. 9 is a similar view showing the ahead running position.
Fig. 10 is a diagrammatic view showing the positions taken by the motor parts in astern running sition.
Fig. 11 is a similar view showing astern startlng position.
Fig. 12 is a similar view showing stop position.
Fig. 13 is a similar view showing ahead starting position.
Fig. 14 is a similar view showing ahead runnmg position.
The showing in Figs. 1 to 9 inclusive is diagrammatic to the extent that the ports are drawn as if they all lay in a single plane of section, according to a convention familiar in the pneumatic control art and adopted to permit the tracing of the flow paths throughout the drawings. The exact layout of the ports is immaterial to the invention,
but obviously more compact arrangements can be adopted, based on principles which will be familiar to those skilled in the art.
Referrin first to Fig. 1, 16 represents a shaft formmg part of the engine starting gear. In the example illustrated the two extreme rotary ositions of the shaft 16 are those correspon ing to the starting functions of the engine (in reverse directions). The shaft turns about 190 in passing from one to the other. The stop position is intermediate the two starting positions and thus approximately at 95 to each. The two running positions are displaced on opposite sides of the stop position 30 or less. These angular displacements are mentioned merely as characteristic of one typical gear with which the controlling mechanism may be used.
Swiveled on the shaft 16 is a gear 17 which might be fast on the shaft, but which in the example illustrated, is releasably clutched thereto by a dental clutch, part of which appears at 18. This clutch is asymmetric as to its engaging jaws so that the gear ma be clutched to the shaft 16 only in one de nite angular relation to the shaft.
The gear 17 meshes with a rack 19 formed on a longitudinally sliding piston rod 21. The piston rod 21 is guided in a sleeve hushing 22 fixedly locked in the main casting 23 by nuts 24 and held against rotation therein by a stud 25. The stud 25 has also a tongue which enters a keyway 20 in the piston rod 21 and holds this rod against rotation. Formed on the casting 23 are two oppositely directed tubular extensions 26, each of which carries at its end an annular stop nut 27. This stop nut 27 limits the outward motion of respective plunger thimbles 28 which are urged to their outward position by coil springs 29. The piston rod 21 passes through the ends of the thimbles 28 and is provided at opposite ends with identical pistons 31R and 31A. (The letters indicate ahead and reverse functions of the respective pistons.) The parts are so dimensioned that when the springs 29 are extended to a point at which the thimbles 28 are arrested by the stop nuts 27 the two thimbles 28 are in engagement with the two pistons 31A, 31R and thus hold the piston rod 21 and consequently the rack 19 in mid-position. In this position the gear 17 and shaft 16 are held in engine stopping position. This is the normal position assumed by the device when freed of pressure.
Each piston 31A, 31R is provided with a peripheral cup leather 32 and is slidable in a corresponding movable cylinder 33 which is formed as an extension on an inner piston 34A or 34R respectively. The pistons 31A, 31R are each single acting, the space between the two pistons bein vented to atmosphere. The pistons 34A, 34 have each a peripheral packing cup leather 35 and each works in a corresponding fixed cylinder 36 whlch is supported by the main casting 23. The outer ends of the cylinders 36 are closed by heads 37. Each cylinder 33 is really a tubular extension on the piston 34A or 34R and has an outside diameter less than the diameter of such piston. At its inner end .the extension is uided in a portion of the casting 23 and ma es a close fit therewith as indicated at 38. There are thus provided annular spaces 39 each of which communicates with the working space of the corresponding cylinder 33 by means of ports 41. The pistons 34A and 34R are really each a single acting piston, the annular space 39 not entering as a material factor in the force exerted on the piston. Instead, each annular space serves merely as a part of the connection to the working space of the corresponding cylinder 33. This is a convenient way of maintaining this connection regardless of the position 0 piston 34.
In each of the pistons 34A, 34R there is a check valve 30 opening to permit flow from the space in cylinder 33 to the space in cylinder 36.
As stated, Fig. 1 shows two remote control valves and one engineers control valve ad jacent the starter shiftin mechanism. These are desi nated on Fig. 1 by the letters RC#1, R #2 for the two remote control valves and EC for the engineers control valve. RC#1 and RC#2 are shown in lap osition, the handle being removed from C#1 and applied to RC#2. Most of the handle of EC is invisible in Fig. 1, being forward of the plane of section, but it will be understood that the use of a handle on EC at all times is contemplated on the theory that it is advisable to permit control by the engineer at any time. The provision of a single handle for use on RC#1 and RC#2 selectively will preclude interference in control by either of these stations with control by the other. Where interference can beotherwise guarded against this precaution is unnecessary. The valves EC, RC#1 and RC#2 are essentially identical'except that EC is provided with a double check valve which serves all three valves and hence is not duplicated. It might'be located in any of the three.
In their general makeu J these valves follow standard practice. ach includes as a base member a pipe bracket 44 to which all pipe connections are made, a superposed ported valve seat member 45, a removable cap 46 to which the pressure supply is admitted, and a rotary valve 47 which controls the ports in the said seat. The rotary valve 47 may be rotated to its various positions by a removable handle 49 which has a spring plunger latch 51 coacting with a notched sector 52 fixedly supported on the cap 46. An arcuate guard 57 is provided and prevents the removal of the member 49 except when the valve 47 is in lap position, lap position being that in which all the ports in the seat are closed by the rotary valve (see Fig. 5). In the valve as constructed the member 49 is not strictly the handle member but instead a hand grip 58 is pivoted at 59 on the member 49 so as to swing in a vertical plane. This carries a downward extending arm 61 which in lap position may engage the protruding stem of a valve 62 and force the same open against the resistance of its spring 63 and the pressure sustained by the valve. The yalve 62 is the stop valve and is a novel feaare.
The purpose of this arrangement is to allow the control valves to be moved to lap position without stopping the engine and et to provide for the stopping of the engine wh le the valves are in lap position and only while they are in lap position.
In the case of the valve EC in Fig. 1, the analogue of the pipe head member used on RC#1 and RC#2 is formed directly in the castlng 23. It has already been stated that the ports in the member 45 are continuations of ports in the member 44. It will also be apparent from an inspection of Fig. 1 that as to the valve EC the ports are extensions of ports formed in the casting 23. Connections between the pipe brackets 44 and the casting 23 are made by pipes, but to avoid confusion by the use of an excessive number of references, a single continuous passage will be indicated by a single reference numeral.
Alr 1s supplied to the space within the caps 46 by a supply passage 65. This is fed from a reservoir 66 maintained charged at a uniform pressure by any suitable means, not shown. The reservoir may be provided with a pressure gage 67, a drain cock 68 and a stop cock 69 may be inserted in the pipe connecting the reservoir with the line 65.
The passages 71, 72, 73 and 74 all lead from the seats of all three rotary valves 47 to the four working cylinder spaces, as follows: 71 leads to the space to the left of the piston 34A. 72 leads to the space to the left of the piston 31A. 73 leads to the space to the right of the piston 34R and 74 leads to the space to the valves. There are also extensions of passages- 71 and 73 leading to these faces. These extensions are blanked off in the case of RC#1 and RC#2 by cover plates 78 and gaskets 79, but in the case of the valve EC there is a double check valve whose body is indicated generally by the numeral 81. This valve is illustrated in Fig. 1 and is shown on an enlarged scale in Fig. 2.
The body 81 has a cap 82 and the two together house a cylindrical valve bushing 83 in which is longitudinally slidable a check valve element 84. This has sealing gaskets 85 on its ends which coact alternately with annular valve seats 86 and 87. The valve functions, as will be apparent, to connect either passage 71 or 73 with the passage 76 controlled by the valves 62. The passages 71 and 73 are connected respectively to the working space to the left of piston 34A and the working space to the right of piston 34R. The valve 84 shifts to connect the passage 76 to whichever one of these working spaces is at the time charged. Since only one is charged at a time, the valve 84 operates to place which ever one is charged under control of the valves 62. Any one of the valves 62 when opened will operate to vent the charged workmg space and allow the mechanism to move to engine stopping position. If working spaces of cylinders 33 and 36 are both charged, as occurs in starting position, the exhaust of 36 will also exhaust 33 through a check valve 30.
As best indicated in Figs. 6, 7, 8 and 9, in which the porting is strictly diagrammatic, each rotary valve 47 is provided with recesses 91, 92 and through ports 93, 94 and 95, which serve to subject pistons 31R and 34R to pressure and vent pressure acting against pistons 31A and 34A (Fig. 6) subject piston 34R to pressure and vent pressure acting against p stons 31R, 31A and 34A (Fig. 7) sub ect pistons 31A and 34A to pressure and vent pressure acting against pistons 31R and 34R (Fig. 8) or subject piston 34A to pressure and vent pressure acting against pistons 31A, 31R and 34R (Fig. 9). Pressure acting against plstons 34A and 34R is manually vented by the valves 62, and if either piston 31A or 31R is subject to pressure, this will be vented by check valve 30 in piston 34A or 34R.
From this it follows that each of the passages 71, 72, 73 and 74 serves as a combined supply and exhaust port for pressure fluid flowing to and from the working spaces of the respective cylinders.
For the purpose of reducing the delay by friction of flow through long passages to the remote control valves, a quick release valve is interposed in each of the passages adjacent the working space served by the passage, the quick release valve being so arranged that it closes a local exhaust when flow toward the working space occurs and opens it immediately that flow from the working space starts. This greatly accelerates the response of the mechanism.
These local release valves are all identical in structure. The one interposed in the passage 71 is indicated on Fig. 1 at 96, the one in the passage 72 at 97, the one in the passage 73 at 98 and the one in the passage 74 at 99.
Valve 96 is illustrated in detail in Fig. 3 and is typical of all the valves. In this figure 96 is applied to the body of the valve and 101 represents a removable cap. This has a guideway for the stem 102 of a check valve 103 which opens, inward and is guided by its pilot 104 into and out of seating engagement with the seat 105. Seat 105 surrounds a. port 106 leading to atmosphere. Slidably mounted on the stem 101 and limited in its upward motion by a stop nut 107, is a pistonlike disk 108 which approximately but not quite fills the short cylindrical space 109. The disk 108 is held upward by a spring 111 against the stop 107 and the parts are so arranged that when the valve 103 is seated and the disk 108 is against the stop 107, this disk is at about mid-length of the restricted cylindrical portion 109.
Valve 96 is interposed in the passage 71 and the connections are such that fiow from any control valve RC#1, RC#2 or EC toward the working space to the left of piston 34A will urge the valve 103 closed by .forcing the piston member 108 downward against spring 111. On the other hand, reverse flow, that is from the cylinder to a control valve and thence to exhaust, will act upward on the disk 108, unseat the valve 103 and open a large local exhaust from the working space.
Fig. 4 indicates the five positions of the control valves corresponding to Figs. 5 to 9 inclusive.
The device operates as follows:
Assuming that the handle 58 is in lap position, the reservoir 66 is properly charged, valve 69 is open and shaft 16 is held in midposition by piston rod 21 which is then in mid-position, the operation of starting the engine in reverse running direction is as follows:
The handle 58 is swung clockwise (i elatively to Fig. 4) to its limiting position, which is astern starting position. This puts the rotary valve in the position of Fig. 6. In this position ports 71 and 72 are both connected to exhaust port and ports 73 and 74 receive air which is supplied to the space within cap 46 by passage 65. This action occurs no matter which one of the three control valves is manipulated. The effect is to charge the working spaces of pistons 31R and 34R, thus moving the piston rod to the extreme leftward position indicated in Figs. 1 and 11. This establishes the starting action of the engine starter and as soon as the engine is in proper motion the operator moves the handle 58 to astern running position. The effect of this as illustrated in Fig. 7 is to connect the port 74 also to atmoshere while maintaining the supply to port 3/ It follows that the space to the right of piston 31R is exhausted and the parts move to the position indicated diagrammaticall in Fig. 10.
Fbrward starting is effected in a similar manner by shifting first to ahead starting osition to establish the connections shown In Fig. 8 which admits pressure against pistons 31A and 34A, as indicated in Fig. 13,
and then moving the valve back to ahead run ning position to establish the connections illustrated in Fig. 9. This vents the pressure acting on piston 31A and causes the parts to move to the position shown in Fig. 14.
Obviously any of the valves RC# 1, RC#2 or EC may be manipulated to produce the above result. If the control is to be maintained at the station at which starting was effected the valve will be left in running position, but if control is to be transferred to another valve the handle is swung to lap position, removed, transferred to the selected other control valve, which is then shifted to running position to preclude loss of pressure through gradual leakage. Whenever it is desired to stop the engine, the control valve is swung to lapposition and the handle 58 is depressed to open the valve 62. The effect is to vent the passage 76 and consequently whichever one of the passages 71 or 73 may then be connected to the passage 76 by the check valve 84:.
While I prefer cylinders and pistons as the moving elements and prefer to mount the cylinder of one unit on the iston of the other, it is conceivable that ot er types of expansible chamber motor may be substituted for cylinders and pistons and that they mi ht be otherwise mechanically related.
be important thing is that each of the two motors shall act cumulatively, each adding its increment of motion to that of the other, so that by charging one or both the necessary plurality of positions may be secured. I
It is important also to observe that there is no limit on the number of control valves that might be used if necessary.
Where it is desired --to start, stop and reverse two engines simultaneously, each engine might have its individual starter actuating mechanism. This might be subjected to common control by a single control valve or a single set of control valves. Ordinarily, however, on multiple screw vessels it is desired to start and stop individual engines inde endently for maneuvering purposes.
he present disclosure does not go into the question of speed control which may be effected at the engine or otherwise, as may be preferred. The installation of the present apparatus imposes no limitation on speed control either by local or remote control means.
\(Vhat is claimed is,-
1. Means for actuating astarting gear having a starting position, a running position and a stop position, comprising in combination two expansible chamber motors; means for connecting said motors with said gear whereby each motor may impart independently an increment of motion thereto; valve means operable selectively to admit pressure fluid to othmotors, to admit it to one and exhaust the other and to exhaust both; and
an exhaust valve associated with each motor and having actuating means in the path of flow of pressure fluid to and from the motor, and arranged to be shifted in a valve closing direction by flow toward the motor and in a valve opening direction'by flow from the motor.
2. Means for actuating a starting gearhaving forward and reverse starting position, forward and reverse running positions and a sto position, comprising in combination a member adapted for connection with said gear; yielding means urging said member to stop position; a forward shifting unit and a reverse shifting unit, each of said units including two expansible chamber motors each connected to said member to impart independently an increment of motion thereto; and means controllable selectively to admit pressure fluid to both motors of one unit while exhausting the motors of the other unit, to admit it to one motor of one unit while exhausting the other motor of that unit and those of the other unit, and to exhaust all the motors.
3. Means for actuating a starting gear having forward and reverse starting position, forward and reverse running positions and a stop position, comprising in combination a member adapted for connection with said gear; yielding means urging said member to stop position; a forward shift-ing unit and a reverse shifting unit, each of said units includingtwo expansible chamber motors, the
' second mounted on the moving element of the first and having its moving element connected with said member; and means controllable selectively to admit pressure fluid to both motors of one unit while exhausting the motors of the other unit, to admit it to one motor of one unit while exhausting the other motor of that unit and those of the other unit, and to exhaust all the motors.
4. The combination with a starting memand a lap position in which all ports are closed; an actuator for said maneuverin valve; and a stopping valve independent 0 said maneuvering valve controlling the stop function of said motor means and operable by said actuator only when the maneuvering valve is in lap position.
5. The combination with a starting member having starting and running positions both forward and reverse and a stop position, of motor means for shifting said member selectively to said positions; a maneuvering valve controlling said motor means and having forward starting and running positions and reverse starting and running positions in which ports are opened selectively, and an intermediate lap position in which all ports are closed; an actuator for said maneuvering valve; and a stop valve independent of said maneuvering valve controlling the stop function of said motor means and operable by said actuator only when the maneuvering valve is in lap position.
6. The combination with a starting member having starting and running positions and a stop position, of motor means for shifting said member selectively to said positions; a plurality of maneuvering valves each capable of controlling said motor meansand having starting and running positions in which ports are opened selectively, and a lap position in which all ports are closed; a stopping valve associated with each maneuvering valve and operable to effect the stopping function; a removable actuator applicable selectively to said maneuvering valves to actuate the same, said actuator being capable of actuating said stopping valve but only when the maneuvering valve is in lap position; and a guard on each maneuvering valve permitting the application and removal of the actuator only when the valve is in lap position.
7. The combination with a starting member having starting and running positions both forward and reverse and a stop position, of motor means for shifting said member selectively to said positions; a'plurality of maneuvering valves each capable of controlling said motor means and having forward starting and running positions and reverse starting and running positions in which ports are opened selectively, and an intermediate lap position in which all ports are closed; a stopping valve associated with each maneuvering valve and operable to effect the stopping function; a removable actuator applicable selectively to said maneuvering valves to actuate the same, said actuator being capable of actuating said stopping valve but only when the maneuvering valve is in lap position; and a guard on each maneuvering valve permitting the application and removal of the actuator only when the valve is in lap position.
8. The combination with a starting member having starting and running positions and a stop position, of motor means for shifting said member selectively to said positions; a maneuvering valve controlling said motor means and having starting and running positions in which ports are opened selective ly, and a lap position in which all ports are closed; an actuator for said maneuvering valve; an independent stopping valve controlling the stop function of said motor means; and means for actuating said stopping valve, said means being operatively positioned relatively to the stopping valve by the motion of said maneuvering valve to lap position.
9. The combination with a starting member having starting and running positions both forward and reverse and a stop position, of motor means for shifting said member selectively to said positions; a maneuvering valve controlling said motor means and having forward starting and running positions and reverse starting and running positions in which ports are opened selectively, and an intermediate lap position in which all ports are closed; an actuator for said maneuvering valve; an independent stopping valve controlling the stop function of said motor means; and means for operating said stopping valve, said means being operatively positioned relatively to the stopping valve by the motion of said maneuvering valve to lap position.
10. The combination with a starting member having starting and running positions both forward and reverse and a stop position, of motor means for shifting said member selectively to said positions; a maneuvering valve controlling said motor means and having forward starting and running positions and reverse starting and running positions in which ports are opened selectively, and an intermediate lap position in which all ports are closed; an actuator for said maneuvering valve; a single stop valve for controlling the stop functions of said motor means; and a pressure actuated selector valve for connecting said stop valve selectively with whichever of said forward and reverse motor means is under pressure.
11. The combination with a starting member having starting and running positions both forward and reverse and a stop position, of motor means for shifting said member selectively to said positions; a maneuvering valve controlling said motor means and having forward starting and running positions and reverse starting and running positions in which ports are opened selectively, and an intermediate lap position in which all ports are closed; an actuator for said maneuvering valve; a stop valve independent of said maneuvering valve for controlling the stop function of said motor means and operable by said actuator only when the maneuvering valve is in lap position;and a pressure actuated selector valve for connecting said stop valve selectively with whichever of said forward and reverse m0- tor means is under pressure.
12. The combination with a starting member having starting and running ositions and a stop position, of motor means or shifting said member selectively to said positions; a maneuvering valve controlling said motor means and having starting and running positions in which ports are opened selectively, and a lap position in which all ports are closed; an actuator for said maneuvering valve; and a stopping valve distinct from said maneuvering valve'and controlling the stop function of said motor means.
13. The combination with a starting memher having starting and running positions both forward and reverse and a stop position, of motor means for shifting said member selectively to said positions; a maneuvering valve controlling said motor means and having forward starting and running positions and reverse starting and running positions in which ports are opened selectively, and an intermediate lap position in which all ports are closed; an actuator for said maneuvering valve; and a stop valve distinct from said maneuvering valve and controlling the stop function of said motor means.
In testimony whereof I have signed my name to this s cification.
C RLES A. CAMPBELL.
US335956A 1929-01-29 1929-01-29 Remote control mechanism Expired - Lifetime US1806669A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US335956A US1806669A (en) 1929-01-29 1929-01-29 Remote control mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US335956A US1806669A (en) 1929-01-29 1929-01-29 Remote control mechanism

Publications (1)

Publication Number Publication Date
US1806669A true US1806669A (en) 1931-05-26

Family

ID=23313955

Family Applications (1)

Application Number Title Priority Date Filing Date
US335956A Expired - Lifetime US1806669A (en) 1929-01-29 1929-01-29 Remote control mechanism

Country Status (1)

Country Link
US (1) US1806669A (en)

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2440478A (en) * 1942-11-24 1948-04-27 Adel Prec Products Corp Shuttle valve
US2473695A (en) * 1947-01-21 1949-06-21 Westinghouse Air Brake Co Multivalve control station for servomotors
US2485252A (en) * 1945-10-24 1949-10-18 Midland Steel Prod Co Door operating fluid motor system
US2491087A (en) * 1947-07-30 1949-12-13 Harland W Cardwell Air controlled shifting mechanism
US2510314A (en) * 1943-12-17 1950-06-06 Deere Mfg Co Fluid pressure motor
US2512013A (en) * 1946-01-17 1950-06-20 Westinghouse Air Brake Co Two station control of fluid motors
US2524488A (en) * 1948-03-13 1950-10-03 Westinghouse Air Brake Co Fluid pressure control apparatus
US2540710A (en) * 1947-08-21 1951-02-06 Westinghouse Air Brake Co Fluid pressure control apparatus
US2595486A (en) * 1948-03-06 1952-05-06 Skoda Works Nat Corp Servomotor and mechanism for limiting its piston movements at variably predetermined positions
US2630786A (en) * 1951-06-14 1953-03-10 Westinghouse Air Brake Co Multiple position fluid pressure motor
US2635584A (en) * 1950-09-15 1953-04-21 Askania Regulator Co Hydraulic relay control
US2669971A (en) * 1949-05-18 1954-02-23 John D Mooney Hydraulic reversing transmission
US2699756A (en) * 1950-09-15 1955-01-18 Leonidas C Miller Reciprocating pneumatic actuator for tools
US2707005A (en) * 1950-12-28 1955-04-26 Wolldeckenfabrik Zoeppritz Ag Means for the periodic and automatic rotation of a shaft through pre-determined angles which are controlled by a perforated card, more especially for the selective insertion of different yarn shuttles on looms
US2793632A (en) * 1946-06-11 1957-05-28 Bendix Aviat Corp Regulator and control device for an internal combustion aircraft engine
US3019771A (en) * 1960-06-09 1962-02-06 Gen Dynamics Corp Hydraulic rotary actuator
US3104589A (en) * 1960-11-14 1963-09-24 Flo Tork Inc Hydraulic control
US3172333A (en) * 1961-05-31 1965-03-09 Mercier Jean Adjustable torque hydraulic actuator system
US5207111A (en) * 1990-08-24 1993-05-04 Montech Ag Rotary unit

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2440478A (en) * 1942-11-24 1948-04-27 Adel Prec Products Corp Shuttle valve
US2510314A (en) * 1943-12-17 1950-06-06 Deere Mfg Co Fluid pressure motor
US2485252A (en) * 1945-10-24 1949-10-18 Midland Steel Prod Co Door operating fluid motor system
US2512013A (en) * 1946-01-17 1950-06-20 Westinghouse Air Brake Co Two station control of fluid motors
US2793632A (en) * 1946-06-11 1957-05-28 Bendix Aviat Corp Regulator and control device for an internal combustion aircraft engine
US2473695A (en) * 1947-01-21 1949-06-21 Westinghouse Air Brake Co Multivalve control station for servomotors
US2491087A (en) * 1947-07-30 1949-12-13 Harland W Cardwell Air controlled shifting mechanism
US2540710A (en) * 1947-08-21 1951-02-06 Westinghouse Air Brake Co Fluid pressure control apparatus
US2595486A (en) * 1948-03-06 1952-05-06 Skoda Works Nat Corp Servomotor and mechanism for limiting its piston movements at variably predetermined positions
US2524488A (en) * 1948-03-13 1950-10-03 Westinghouse Air Brake Co Fluid pressure control apparatus
US2669971A (en) * 1949-05-18 1954-02-23 John D Mooney Hydraulic reversing transmission
US2635584A (en) * 1950-09-15 1953-04-21 Askania Regulator Co Hydraulic relay control
US2699756A (en) * 1950-09-15 1955-01-18 Leonidas C Miller Reciprocating pneumatic actuator for tools
US2707005A (en) * 1950-12-28 1955-04-26 Wolldeckenfabrik Zoeppritz Ag Means for the periodic and automatic rotation of a shaft through pre-determined angles which are controlled by a perforated card, more especially for the selective insertion of different yarn shuttles on looms
US2630786A (en) * 1951-06-14 1953-03-10 Westinghouse Air Brake Co Multiple position fluid pressure motor
US3019771A (en) * 1960-06-09 1962-02-06 Gen Dynamics Corp Hydraulic rotary actuator
US3104589A (en) * 1960-11-14 1963-09-24 Flo Tork Inc Hydraulic control
US3172333A (en) * 1961-05-31 1965-03-09 Mercier Jean Adjustable torque hydraulic actuator system
US5207111A (en) * 1990-08-24 1993-05-04 Montech Ag Rotary unit

Similar Documents

Publication Publication Date Title
US1806669A (en) Remote control mechanism
US2142466A (en) Variable clearance volume engine
US1963444A (en) Remote control apparatus for power driven boats and the like
US2444273A (en) Engine conditioning control apparatus for starting, stopping, and reversing
SE421079B (en) DEVICE FOR REGULATING BRAKE POWER RECOVERY FROM A MULTI-CYLINDER-DIESEL ENGINE
US2395202A (en) Control system
US2142950A (en) Pneumatic diesel air chamber valve control mechanism
US2187465A (en) Gear shifting mechanism for motor vehicles
US2164522A (en) Internal combustion engine
US2270059A (en) Control mechanism for sawmill carriage steam feeds
US2394074A (en) Starting valve for reciprocating motors
US2444083A (en) Hydraulic motor means for actuating nested distributing valves
US1446109A (en) Assictnoe
US1772970A (en) Slide valve for the scavenging air pump and for the starting air in internal-combustion engines
US2243626A (en) Servo system
US1487347A (en) Engine
US2280588A (en) Fluid motor
US2584995A (en) Pressure actuated transmission control unit
US1233088A (en) Gear-shifting mechanism.
US1647561A (en) Rotary distributing valve and valve gearing for steam and other fluidpressure engines
US2457568A (en) Control apparatus for plural motor propulsion systems
US888007A (en) Starting mechanism for explosive-engines.
US991233A (en) Starting device for gas-engines.
US1603980A (en) Locomotive control
US2188279A (en) Gear shifting mechanism for motor vehicles