US985958A - Steering device for vehicles, airships, aeroplanes, submarines, and the like. - Google Patents
Steering device for vehicles, airships, aeroplanes, submarines, and the like. Download PDFInfo
- Publication number
- US985958A US985958A US57875510A US1910578755A US985958A US 985958 A US985958 A US 985958A US 57875510 A US57875510 A US 57875510A US 1910578755 A US1910578755 A US 1910578755A US 985958 A US985958 A US 985958A
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- US
- United States
- Prior art keywords
- submarines
- aeroplanes
- vehicles
- steering
- airships
- 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
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Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
- G05G9/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
- G05G9/02—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only
- G05G9/04—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously
- G05G9/047—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks
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- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/20—Control lever and linkage systems
- Y10T74/20012—Multiple controlled elements
Definitions
- Figure 1 shows a part-sectional elevationof the device
- Fig. 2 shows a plan of same
- Fig. 3 shows a section through the bottom part of the device in the direction of the arrow 1, Fig. 1
- Fig.4 shows a vertical section through the steering lever in the direction of the arrow '2, 1, the whole being illustrated on a larger scale for the sake of clearness.
- a frame or base 10 of preferably square-shaped form with a square hole in the center serving to carry a shaft or axle 13, and having lugs 11, by means of which the base can be screwed onto a horizontal part of the aerial or other conveyance.
- the projecting ends of the shaft 13 carry bars 16 to which are fastened at 6, the wires 8 connecting one of the planes or steering wheels respectively.
- At a right angle to the axle 13, and also carried by the base 10 are bolts 19 upon which bars 20 are mounted, the latter being again connected with another plane or theother steering wheel respectively by means of wires 7, Fig. 2.
- the bars 16 at their upper end carry a toothed segment 17 the teeth being at the lower side of same, while a similar toothed segment 21 is carried by the bars 20.
- the last named segment is at right angles with the segment 17 and on the underside of same. Both segments are slotted in longitudinal directions and serve to guide the steering lever 15, which pivotally hinged to axle 13, terminates in a drilled handle 26 above the segment 17.
- the said handle is provided with a button 27 forming the top end of a spindle 28,-the whole being influenced by a spring 31, Fig. 4, the latter thus effecting an automatic return of the button when the latter has been pressed downward and released again.
- Button and spindle are in connection with pawls 22 and 24 which are adapted to engage with the teeth of the segments 17 and 21.
- the upper end of the steering lever 15 to which the handle is secured. is suitably drilled, Fig. 4, or may consist of a tube, the said tube containing a second tube 29 with head piece 30 the latter serving as securing and 24 are firmly wedged into the inner tube 29 and extend through the outer tube of the steering lever 15 by means of slots 23 and 25, in which they are adapted to slide. If the operator presses upon the button 27 the pawls slide downward in their respective slots thus disengaging from the teeth of the segments and vice versa, if the pressure on the button is released, the pawlsslide automatically, that is to say under influence of the spring 31 upward so that they again engage with the teeth of the segments.
- steering lever which is pivotally mounted upon the axle 13 by means of its forked end 14, may be moved in any desired direction, while immediately after the release of the button the pawls become engaged with the teeth of their respective segments, so that the lever and with it all the movable parts inclusive of the planes or steering wheels are secured and rigidly kept in any desired position.
- the wires 7 and 8 may be attached to the bars 16 and 20 in any con-. venient manner.
- the conveyance thus moving horizontally and in a straight line, the simultaneous-rear movement of the steering lever 15, in the direction of the arrows 4 and 5 has the contrary effect, that is'to say, the conveyance may be made to move downward and-upward or to the left and right by means of i a single lever.
- a tubular hand lever having a forked lower end bein pivotally arran ed upon the aforesaid shalt, the upper end being adapted to slide in the slots of the segments, and of means for securing and releasing the said leverin and from the teeth of the segments, substantially as described and shown and for the purpose specified.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Steering Controls (AREA)
Description
J. WETTERWALD.
STEERING DEVICE FOR VEHICLES, AIRSHIPS, AEROPLANES, SUBMARINES, AND THE LIKE.
APPLIOATIOH FILED AUG. 24, 1910.
Patented Mar. 7, 1911.
[UNITED STATES PATENT OFFICE. I
' J'dSEPH WETTER'WALD, OF LUCEBNE, SWITZERLAND.
STEERING DEVICE FOR VEHICLES,'AIBSHIPS, LEROPLANES, SUBMARINES, AND THE LIKE.
- Specification of Letters Patent.
Patented Mar. '7, 1911.
Application filed August 24, 1910. Serial No. 578,755.
To all whom it may concern:
Be it known that I, J osErH' Wn'r'rnRwALo, a citizen of Switzerland, and resident of Lucerne, Switzerland, have invented :1 Steering Device for Vehicles, Airships,
'Aeroplanes, Submarines, and the Like, of
or' the steering wheels respectively is obtained.
In order that this invention may be more clearly understood, I refer to the accompanying drawlng, inwhlch:
Figure 1 shows a part-sectional elevationof the device; Fig. 2 shows a plan of same; Fig. 3 shows a section through the bottom part of the device in the direction of the arrow 1, Fig. 1; and Fig.4 shows a vertical section through the steering lever in the direction of the arrow '2, 1, the whole being illustrated on a larger scale for the sake of clearness.
In practice I provide a frame or base 10 of preferably square-shaped form with a square hole in the center, the said base serving to carry a shaft or axle 13, and having lugs 11, by means of which the base can be screwed onto a horizontal part of the aerial or other conveyance. The projecting ends of the shaft 13 carry bars 16 to which are fastened at 6, the wires 8 connecting one of the planes or steering wheels respectively. At a right angle to the axle 13, and also carried by the base 10 are bolts 19 upon which bars 20 are mounted, the latter being again connected with another plane or theother steering wheel respectively by means of wires 7, Fig. 2. The bars 16 at their upper end carry a toothed segment 17 the teeth being at the lower side of same, while a similar toothed segment 21 is carried by the bars 20. The last named segment is at right angles with the segment 17 and on the underside of same. Both segments are slotted in longitudinal directions and serve to guide the steering lever 15, which pivotally hinged to axle 13, terminates in a drilled handle 26 above the segment 17. The said handle is provided with a button 27 forming the top end of a spindle 28,-the whole being influenced by a spring 31, Fig. 4, the latter thus effecting an automatic return of the button when the latter has been pressed downward and released again. Button and spindle are in connection with pawls 22 and 24 which are adapted to engage with the teeth of the segments 17 and 21. The upper end of the steering lever 15 to which the handle is secured. is suitably drilled, Fig. 4, or may consist of a tube, the said tube containing a second tube 29 with head piece 30 the latter serving as securing and 24 are firmly wedged into the inner tube 29 and extend through the outer tube of the steering lever 15 by means of slots 23 and 25, in which they are adapted to slide. If the operator presses upon the button 27 the pawls slide downward in their respective slots thus disengaging from the teeth of the segments and vice versa, if the pressure on the button is released, the pawlsslide automatically, that is to say under influence of the spring 31 upward so that they again engage with the teeth of the segments.
In action the device operates as follows:
means for the spindle 28. Both pawls 22 If the button 27 is pressed downward, the
steering lever which is pivotally mounted upon the axle 13 by means of its forked end 14, may be moved in any desired direction, while immediately after the release of the button the pawls become engaged with the teeth of their respective segments, so that the lever and with it all the movable parts inclusive of the planes or steering wheels are secured and rigidly kept in any desired position. The wires 7 and 8 may be attached to the bars 16 and 20 in any con-. venient manner. If now by way of example, the steering lever 15 in the afore described mannerjs moved forward, in the direction of the arrow, only the vertically disposed segment 17 guiding the said lever, is coming into operation, and with it the plane or the steering wheel which is connected by means this being an 1m ortant feature of the presoperating both elevating and directing plane,
ent invention. roviding one of the p anes has already been put into a certain position or to be more explicit, if the steering lever 15 has been'moved to the left, the operator is still enabled to proceed forward as well as backward without altering the position of the-already adjusted plane or rudder, since the corresponding toothed segment is kept rigid, only the segment of the second plane being put in action. In conse uence of the fact, that the middle position 0 the steering lever 15 is the means of placin the planes or the steering wheels or rud ers in their middle position, the conveyance thus moving horizontally and in a straight line, the simultaneous-rear movement of the steering lever 15, in the direction of the arrows 4 and 5 has the contrary effect, that is'to say, the conveyance may be made to move downward and-upward or to the left and right by means of i a single lever.
In constructing my device I make all the parts preferably of aluminium at the same time making due allowance as regards the strength of the said arts; The wlres 7 and 8 are in reality muc longer and should be guided by means of rollers to assist in the smooth working of the device. The teeth are furthermore made so that any breakage or disengagement of the pawls is obviated.
ends of the shaft and Having now fully described my said invention what I claim and desire to secure by Letters Patent is t 1. In a steeringdevice for vehicles, airships, aeroplanes, submarines and the like the combination with a frame (10) which is attached to the said conveyances, of a shaft carried by the frame, bolts mounted in the frame and at right angles to the said shaft, bars pivotally mounted u on the projecting olts respectively,
witnesses.
toothed segments carried by the said bars and being provided with longitudinal slots, a tubular hand lever having a forked lower end bein pivotally arran ed upon the aforesaid shalt, the upper end being adapted to slide in the slots of the segments, and of means for securing and releasing the said leverin and from the teeth of the segments, substantially as described and shown and for the purpose specified. v
2. In a steering device for air-ships, aeroplanes and submarines, the combination with a frame (10) which is attached to the said conveyances, of a shaft carried by the frame,
bolts mounted in the frame and at right 1 angles to the said mounted upon the projecting ends of the shaft, and bolts respectively, toothed-segments carried by the said bars and being providedwith longitudinal slots, a tubular hand leverhaving a forked lower end being pivotally arranged upon the aforesaid shaft, the upper end being ada ted to slide in the slots of thesegments, an of means for securing and releasing the said lever in and from the teeth of the segments, the said means consisting of a spring influenced spindle with button at its top end, both spindle and button being guided in the drilled handle of the tubular lever, a second tube arranged inside the tubular lever and being connected to the aforesaid spindle, two pawls at right angles to each other secured in the inner tube and adapted to slide up and down in the slots of the outer tube, substantially as described and shown and for the purpose specified.
In testimony whereof I have hereunto set my hand in the presence of twosubscribing N J. WETTERWALD. Witnesses: n
T. SENNRIGH, J. C. GEDEAN;
shaft, bars pivotally
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US57875510A US985958A (en) | 1910-08-24 | 1910-08-24 | Steering device for vehicles, airships, aeroplanes, submarines, and the like. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US57875510A US985958A (en) | 1910-08-24 | 1910-08-24 | Steering device for vehicles, airships, aeroplanes, submarines, and the like. |
Publications (1)
Publication Number | Publication Date |
---|---|
US985958A true US985958A (en) | 1911-03-07 |
Family
ID=3054302
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US57875510A Expired - Lifetime US985958A (en) | 1910-08-24 | 1910-08-24 | Steering device for vehicles, airships, aeroplanes, submarines, and the like. |
Country Status (1)
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US (1) | US985958A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2502969A (en) * | 1945-01-30 | 1950-04-04 | Oil Well Supply Co | Power input control for welldrilling hoists |
US2505260A (en) * | 1945-04-07 | 1950-04-25 | Westinghouse Air Brake Co | Control apparatus |
US2608105A (en) * | 1948-03-22 | 1952-08-26 | Mcgill Mfg Company Inc | Adapter for universal lever switches |
US2616305A (en) * | 1948-03-17 | 1952-11-04 | Bendix Aviat Corp | Flight controller for automatic pilots |
US20090230252A1 (en) * | 2008-03-13 | 2009-09-17 | Eurocopter | Aircraft flight control |
-
1910
- 1910-08-24 US US57875510A patent/US985958A/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2502969A (en) * | 1945-01-30 | 1950-04-04 | Oil Well Supply Co | Power input control for welldrilling hoists |
US2505260A (en) * | 1945-04-07 | 1950-04-25 | Westinghouse Air Brake Co | Control apparatus |
US2616305A (en) * | 1948-03-17 | 1952-11-04 | Bendix Aviat Corp | Flight controller for automatic pilots |
US2608105A (en) * | 1948-03-22 | 1952-08-26 | Mcgill Mfg Company Inc | Adapter for universal lever switches |
US20090230252A1 (en) * | 2008-03-13 | 2009-09-17 | Eurocopter | Aircraft flight control |
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