US263505A - A lex andes - Google Patents

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US263505A
US263505A US263505DA US263505A US 263505 A US263505 A US 263505A US 263505D A US263505D A US 263505DA US 263505 A US263505 A US 263505A
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piston
head
wings
steam
port
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/34Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
    • F01C1/344Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F01C1/352Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the vanes being pivoted on the axis of the outer member

Definitions

  • the object of the invention is to provide a cheaply-constructed, simple, and effective rotary engine capable of being propelled by either steam, water, or compressed air, and equally eil'ective when used as a rotary pump; and it consists of a peculiarly-formed hollow cylindriical piston pivoted within a cylinder so bored outthatasegmeutot'itsinterior periphery shall correspond with the circle of the cylindrical piston within it, while the balance of the inteiior periphery of the cylinder is enlarged to correspond with the circle described by the extended wings passing through the cylindrical piston, as hereinafter described.
  • Figure l is a sectional end view through X Y.
  • Fig. 2 is a crosssection through Z W.-
  • Fig. 3 is a perspective view of my cylindrical piston-head.
  • Fig. 4 is a perspective view of one of the wings.
  • Figs. 5 and 5 are details showing a plan for packing the connection between wings and cylindrical piston-head.
  • A is my cylindrical piston-head, having slotted passage-ways a (see Fig. 3) cut in its body, as shown.
  • O is an open-ended cylinder provided with covers D.
  • the cylindrical piston-head A fits within the cylinder 0, and the spindle B passes through and is journaled within holes made in the covers D, suspending the cylindrical piston-head A immediately over and in proximity to the segment 6 of the interior periphery of the cylinder 0, made to correspond with the circle of the piston-head.
  • the wings E are the wings, made to fit in the passage ways a and extending clear through the piston-head A.
  • Theloopsconnectingthetwoends of the wings E permit their adjustment, not withstanding the spindle B, which passes through the center of the cylinder.
  • each end of the wings E comes in contact with the segment 0 of the interior periphery of the cylinder corresponding with the circle of the piston-head A it is pushed in flush, or nearly so, with the circle of the piston-head, the opposite end of the wing being thereby caused to protrude on the opposite side of the piston-head, the interior periphery of the cylinder being bored out to correspond to the circle described by the end of the wings when protruding in the manner mentioned.
  • At one end of the segment 6 is formed the inlet-port F, and at, or rather near, the other end of the segment is formed the outlet-port G.
  • I provide an adjustable ring, H fitting into a groove cut in the inside surface of the covers D. These rings are provided with adjustingscrews H screwed into the covers D, so that the pressure of the rings against the ends of the piston-head may be adjusted so as to form the required joint.
  • each recess f Through the wall forming each recess f, I pierce a-hole, h, connecting the interior of the piston-head A with the recess behind each gib g. These holes are intended to admit the steam-pressure behind each gib, so as to force the surface of each against the side of each wing it is fitted to.
  • the cylinder 0, having segment 6, inlet F, and outlet G, and channels d n, adjacent to the inlet and outlet, in combination with a pistonhead, A, provided with adjustable wings E, recessesf, gibs 9, holes L, leading into the recesses f, and the ports 70, substantially as and for the purpose specified.

Description

(No Model.)
A. 0. GIBSON.
' ROTARY ENGINE. No. 263,505. Patented Aug. 29, 1882.
NIIE STATES ATENT FFIQE.
ONE-HALF TO EDMOND ARMANT, OF SAME PLACE.
ROTARY ENGINE.
SPECIFICATION forming part of Letters Patent No. 263,505, dated August 29, 1882.
Application filed April 10, 1882. (No model.)
I 0 all whom it may concern:
Be it known that I, ALEXANDER CALDER GIBsON, a subject of the'Queen of Great Britain, residing at the city of Toronto, in the county of York, in the Province of Ontario, Dominion of Canada, have invented certain new and useful Improvements in Rotary Engines, of which the following is a specification.
The object of the invention is to provide a cheaply-constructed, simple, and effective rotary engine capable of being propelled by either steam, water, or compressed air, and equally eil'ective when used as a rotary pump; and it consists of a peculiarly-formed hollow cylindriical piston pivoted within a cylinder so bored outthatasegmeutot'itsinterior periphery shall correspond with the circle of the cylindrical piston within it, while the balance of the inteiior periphery of the cylinder is enlarged to correspond with the circle described by the extended wings passing through the cylindrical piston, as hereinafter described.
Figure l is a sectional end view through X Y. Fig. 2 is a crosssection through Z W.-
Fig. 3 is a perspective view of my cylindrical piston-head. Fig. 4 is a perspective view of one of the wings. Figs. 5 and 5 are details showing a plan for packing the connection between wings and cylindrical piston-head.
A is my cylindrical piston-head, having slotted passage-ways a (see Fig. 3) cut in its body, as shown.
B is a spindle attached to or forming part of the piston-head A. I
O is an open-ended cylinder provided with covers D. The cylindrical piston-head A fits within the cylinder 0, and the spindle B passes through and is journaled within holes made in the covers D, suspending the cylindrical piston-head A immediately over and in proximity to the segment 6 of the interior periphery of the cylinder 0, made to correspond with the circle of the piston-head.
E are the wings, made to fit in the passage ways a and extending clear through the piston-head A. Theloopsconnectingthetwoends of the wings E permit their adjustment, not withstanding the spindle B, which passes through the center of the cylinder. As shown in the drawings, there are two wings, forming four projecting points beyond the peripheryot' the piston-head, the form of the loops connecting the two ends of the piston-head being such that they pass the spindle B at right angles to each other and may be adjusted independently. As each end of the wings E comes in contact with the segment 0 of the interior periphery of the cylinder corresponding with the circle of the piston-head A it is pushed in flush, or nearly so, with the circle of the piston-head, the opposite end of the wing being thereby caused to protrude on the opposite side of the piston-head, the interior periphery of the cylinder being bored out to correspond to the circle described by the end of the wings when protruding in the manner mentioned. At one end of the segment 6 is formed the inlet-port F, and at, or rather near, the other end of the segment is formed the outlet-port G. As the steam enters the inletport F it comes in contact with a protruding end of one of the wings E, thereby causing the piston-head A to revolve, each wing being acted upon in its turn by the incoming steam, which escapes when the wing reaches the outlet-port G, the projecting end of the wing coming in contact with the inclined guide I), leading from the enlarged portion of the cylinders interior to the smaller circle formed by the segment a. The wings being thus adjusted so that the end which formerly protruded is forced into the piston-head, while the other end is caused to protrude on the opposite side, the steam coming in contact with it thereby maintainingthe rotary movementofthe piston-head.
In order to form a steam-tight joint between the covers D and the ends of the piston-head A, I provide an adjustable ring, H fitting into a groove cut in the inside surface of the covers D. These rings are provided with adjustingscrews H screwed into the covers D, so that the pressure of the rings against the ends of the piston-head may be adjusted so as to form the required joint.
With the view of forming ajointon the edges of the projecting ends of the wings E, I place on each cover D an adjustable ring, H, pro vided with adjusting-screws H. These rings do not extend round the entire circle of the cover, merely extending round that portion of the cover where the wings project beyond the circle of the cylindrical piston.
In order that the full pressure of the steam may be exerted on each projecting end of the wings E as long as possible, I cut a groove or channel, (1, leading from one side of the inletport F, so that the steam will find its way into the space between the end of the wing approaching the outlet-port and the end of the wing passing through the inlet-port. In this manner the full effect of the steam is secured for as long a time as possible,live steam being directed against each projecting end during nearly the whole of its travel between the inlet and outlet ports.
In order that any water or steam which might be carried beyond the outlet-port G shall have an opportunity ofescaping, I out a groove or channel, n, corresponding with the groove or channel d, but extending from the side of the outlet-port G to the interior surface of the segmente,as is clearly shown in Fig. 1.
With the view of forming a steam-tightjoint on either side of the wings where they pass through the slotted passage-ways win the piston head A, I form on either side of each wing a recess, f, into which I fit a gib or pressureplate, g. (See Fig. 5.)
Through the wall forming each recess f, I pierce a-hole, h, connecting the interior of the piston-head A with the recess behind each gib g. These holes are intended to admit the steam-pressure behind each gib, so as to force the surface of each against the side of each wing it is fitted to.
With theview of admitting the steam-pressure into the interior of the piston-head, and at the same time preventing the steam so admitted escaping when passing the port G, I pierce the body of the piston-head A with a number of holes, k, each hole being provided with a stopvalve, I, which is held in position by the cage or guide-piece. So long as the pressure outside the piston-head A exceeds the pressure within it the valves 5 remain open, permitting the free passage of the steam through the holes k. When the pressure within the piston-head A becomes greater than the pressure withoutfor instance, when passing the outlet-port G- the valves close, thereby preventing the escape ofthe steam within the piston-head. Consequently, the pressure within the piston-head being always maintained, the gibs g are constantly held against the surface of the wings.
The foregoing description refers to myimproved rotary engine when propelled by steam, water, or compressed air. When it is to be used as a pump the spindle B will be driven by some suitable motor, in which case the action of the wings will draw the water into the port F and discharge it from the port G, forming a powerful and effective rotary pump.
Of course when the engine is to be used as a rotary pump it will not be necessary to make any provision, such as described, for packing the side of the wings.
What I claim as my invention is- 1. The cylinder 0, having segment 6, inlet F, and outlet G, and channels d n, adjacent to the inlet and outlet, in combination with a pistonhead, A, provided with adjustable wings E, recessesf, gibs 9, holes L, leading into the recesses f, and the ports 70, substantially as and for the purpose specified.
2. In a rotary engine having a hollow cylin drical piston-head provided with adjustable wings and revolving within the cylinder or case 0 D, as described, the gib g and spring, and the apertures h, connecting the interior of the piston-head with the recesses f and adapted to admit steam-pressure therein to force said gih against the side of the wing E, all combined and operating as set forth.
3. In a rotary engine havinga hollow cylindrical piston-head provided with adjustable wings and revolving within a cylinder, as described, the hole h, connecting the interior of the piston-head with the recess f behind each gib g, in combination with the holes k, each hole being provided with a stop or check valve, l, substantially as and for thepurpose specified.
ALEX. C. GIBSON.
Witnesses:
Lnwrs ToMLINsoN, O. (J. BALDWIN.
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5386912A (en) * 1990-12-17 1995-02-07 United States Surgical Corporation Package for multiple sutures
US20040084331A1 (en) * 2002-07-17 2004-05-06 Mark Roby Suture pledget package
US20170373164A1 (en) * 2011-11-23 2017-12-28 Acorn Technologies, Inc. Metal contacts to group iv semiconductors by inserting interfacial atomic monolayers

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5386912A (en) * 1990-12-17 1995-02-07 United States Surgical Corporation Package for multiple sutures
US20040084331A1 (en) * 2002-07-17 2004-05-06 Mark Roby Suture pledget package
US20170373164A1 (en) * 2011-11-23 2017-12-28 Acorn Technologies, Inc. Metal contacts to group iv semiconductors by inserting interfacial atomic monolayers

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