US1317056A - Planooraph co - Google Patents

Planooraph co Download PDF

Info

Publication number
US1317056A
US1317056A US1317056DA US1317056A US 1317056 A US1317056 A US 1317056A US 1317056D A US1317056D A US 1317056DA US 1317056 A US1317056 A US 1317056A
Authority
US
United States
Prior art keywords
cylinder
engine
steam
casing
rotary
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
Publication date
Application granted granted Critical
Publication of US1317056A publication Critical patent/US1317056A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/30Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C18/34Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, 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 F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
    • F04C18/344Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, 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 F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F04C18/352Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, 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 F04C18/08 or F04C18/22 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

  • Figure 1 is a side elevation of the rotary engine constituting ⁇ the best practical embodiment of my invention that I have as yet devised.
  • Fig. 2 is a longitudinal vertical section illustrative of the interior construction of the engine.
  • Fig. -3 isa vertical central section taken ,at right angles to Figs. 1 and 2.
  • Figs. 4 and ⁇ 5 are enlarged detail sections illustrative of the blade mounting.
  • Fig. 6 is an enlarged perspective ⁇ of the double ported valve ⁇ of the engine.
  • I employ a support 1 for the exterior casing ofthe engine, and standards 2 or'maintaining in proper position the rotary member of the engine. I also prefer to have the exterior casing of the ening the invention.
  • Located as best shown in Fig. 2 are groups of cylinders :6.
  • y At 7 are conduits connected with the cylinders 6.
  • the ends or heads of the inner cylinder are designated ⁇ by 8, Fig. 8, and at 9 are rings secured to the inner cylinder and forming walls against which annular metal packing members 10 bear as illustrated.
  • At 11, Fig. 3, is a tubular journal for one side oi the inner cylinder, and at 12 is the nonrotating shaft complementary Ito the stal.tionary arms 13 disposed inside of the inner cylinder.
  • the ports of lthe valve20 are numbered G0, 61, 62 and 63, Figs. 2 and 6.
  • steam entering the port 64 from the supply ,conduit passes through port 61 to ⁇ the righthand conduit 22, Fig. 2, and at ⁇ the same time lexhaust steam from ⁇ the left-hand con- ,duit 22 passes through the port 62, which ,extends partly around the valve to the pipe 23.
  • FIG. i3 it will be noted ⁇ that 24 is a shaft fixed to one of the heads 8 of the inner cylinder. Also that 26 are stationary shaft portions, and 27 are the inwardly-reachingarms on the blades 28.- The Vblades 2 8 form walls of the steam chambers in conjunction with the circular wall 8a of the inner'cylinder.
  • Y In conjunction with the blades 28 I provide metallic packing glands 31, of rocking type, best shown in Figs. t and 5,'which rocking glands are adapted to slide upon the "blades 28l in the direction ofthe length of tenanc'es' the' piston may be rotated, in eitherV direction and'may be 'quickly and'easily reversed when necessityfdemandsl
  • the operation'oftheY engine will be attended the rotation of the inner' ⁇ cylinder including the ⁇ VVwall' 8a aboutthe stationary-shaft' portions 12, and incidental to :such rotation of the. cylinder, the blades 28 ⁇ will be yrotated or moved about the center allorded by lthe shaft y portions 26.
  • valves complementary'to. said 'ports and f connected with saidpistons, a conduit' con- ⁇ nected withf the vcurvilinear chambers, a
  • valve casing connected vwith said conduit and also with the interior of the circularl control valve in said casing, a rotary cylin# der mounted keccentri'cally inthe'- circular casing and havingfrocking bearings at intervalsj in itszf circular wall,- a stationary' casing andl havingl a conduitof its own, a Y

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

w. wAAGBo. ROTARY ENGINE.
APPLICATION FILED APILZI. I9I9.
1,317,056. Patentedsept. 23,1919.
4 SHEETS-SHEET I.
gvwemtoz Wmme@ a@ W7/4J wow n THB COLUMBIA PLANoanAPM co.. WASHINGTON. D. C.
W. WAAGB.
ROTARY ENGINE.
APPLICATION FILED APR. 2|. 1919.
Patented Sept. 23, 1919.
4 SHEETS-SHEET 2.
W. WAAGBO.
ROTARY ENGINE.
APPLICATION FILED APH. 2|. I9I9.
1,317,056. l y Pamedsept. 23, 1919.
4 SHEETS-SHEET 3.
J1/wanton I MQQNLWQ@ o u mmyW-M dmoz/wu,
THB COLUMBIA MPH C0.. WASHINGTON, D. C.
W. WAAGBO.
ROTARY ENGINE.
v 1,1919. 1 ,317,056, PatentedSept. 23, 1919.
4 SHEETS-SHEET 4.
UNITED STATES `PATENT OFFICE.
WILLIAM WAAGBO, OSF NORTHPQBT, MICHIGAN.
ROTARY ENGINE.
Specification of Letters Patent. Patented Sept. 23, 1919,
Application led April 21. 1919. Serial No. 291.441.
.provision of an organized lmechanism adapted to be usedto advantage not only in a rotary steam engine but also ina water force pump, an air pump and an internal combustion engine of the rotary type.
Other objects and practical advantages peculiar to my invention will be fully understood from the follow-ing description and claims when the same are read in connection with the drawings, accompanying and forming part of this specification, in which: v 4
Figure 1 is a side elevation of the rotary engine constituting `the best practical embodiment of my invention that I have as yet devised.
Fig. 2 is a longitudinal vertical section illustrative of the interior construction of the engine.
Fig. -3 isa vertical central section taken ,at right angles to Figs. 1 and 2.
Figs. 4 and `5 are enlarged detail sections illustrative of the blade mounting.
Fig. 6 is an enlarged perspective `of the double ported valve `of the engine.
Similar numerals of reference designate lcorrespondiiilg parts in all the views of the drawings.
In `the present and preferred embodiment of my invention, I employ a support 1 for the exterior casing ofthe engine, and standards 2 or'maintaining in proper position the rotary member of the engine. I also prefer to have the exterior casing of the ening the invention. Located as best shown in Fig. 2 are groups of cylinders :6. y At 7 are conduits connected with the cylinders 6. The ends or heads of the inner cylinder are designated `by 8, Fig. 8, and at 9 are rings secured to the inner cylinder and forming walls against which annular metal packing members 10 bear as illustrated. At 11, Fig. 3, is a tubular journal for one side oi the inner cylinder, and at 12 is the nonrotating shaft complementary Ito the stal.tionary arms 13 disposed inside of the inner cylinder.
In each of the cylinders 6 is disposed the piston 18 of an exhaust valve 14. It is essential that these valves 14 bear Hush in apertures 14 in the wall 3. Each valve 14 is 4provided with a stem 15, of angular form yin cross-section, disposed in an angular conduits which are provided for the supply of steam. An exhaust pipe or :drain 23 is provided as an adjunct to the said conduits 22.
When steam is let into one of the` conduits duit 7 and entering the cylinders .6 at one side of the engine, closes and retains in closed position the valves 14 of the pistons 16 in said cylinder. At the same time the steam exhausting through the other conduit 22 will create a suction in `the other yconduit and therebycontribute to the opening of the valves 14 at the other side of the engine, so as to permit the exhaust ,steam `to enter the adjacent exhaust chamber 5.
The ports of lthe valve20 are numbered G0, 61, 62 and 63, Figs. 2 and 6. When said valve is in the position shown in Fig. 2, steam entering the port 64 from the supply ,conduit passes through port 61 to `the righthand conduit 22, Fig. 2, and at `the same time lexhaust steam from` the left-hand con- ,duit 22 passes through the port 62, which ,extends partly around the valve to the pipe 23. When the valve 20 is turned through half of a revolution to reverse the en ine, live steam from conduit 19 will pass rom the longitudinal bore 64 in valve 20 through the port 60 to the left-hand conduit 22, and at the same time exhaust steam from the right-hand conduit 22 will pass through the port 63 to the pipe 23. Y Y
By reference to Fig. i3 it will be noted `that 24 is a shaft fixed to one of the heads 8 of the inner cylinder. Also that 26 are stationary shaft portions, and 27 are the inwardly-reachingarms on the blades 28.- The Vblades 2 8 form walls of the steam chambers in conjunction with the circular wall 8a of the inner'cylinder.
The inner and rotary cylinder-comprises spokes 30 liXed to the circular wall 8a.
f There are preferably six of the stationary arms 13, and the spokes 30 are adapted to swing about pins V30a carried between the Y arms 13 of lthe two pairs,- Fig.'3.
On their outer and side'edges theblades 28-are provided with suitable packing, as in-V dicated by the dottedlines in Fig. 3.l
Y In conjunction with the blades 28 I provide metallic packing glands 31, of rocking type, best shown in Figs. t and 5,'which rocking glands are adapted to slide upon the "blades 28l in the direction ofthe length of tenanc'es' the' piston may be rotated, in eitherV direction and'may be 'quickly and'easily reversed when necessityfdemandsl The operation'oftheY engine will be attended the rotation of the inner'` cylinder including the `VVwall' 8a aboutthe stationary-shaft' portions 12, and incidental to :such rotation of the. cylinder, the blades 28` will be yrotated or moved about the center allorded by lthe shaft y portions 26. Y Y .y Y It will be readilyinotedthat the inner cylinder, the blades, andthe parts complementary thereto may-'be employed in combination and to:adi'fa'ntage1in` a force pump v for water or otherliquid, 'an*air'p'ump, an internal VVcombustion* engine, and analogous apparatus.
I-have enteredinto detailed: description of the construction andrelative arrangement ofthe elements embracedA in the present em-` j bodiment of my invention,` injorder to`im-l V parta` full, clear and exact understanding .fofthe said specific embodiment. Ido `not Gopies or this patent may be rottaiinedror desire,f however',},to be V'understood as con-y fining myselftothe said specific construction u v and relative 'arrangement'of parts, since `in the future practice of the invention various changes in the form; and arrangement may be made as clearly fall within ythe scope of `my appended claims.
Having described my invention, what I claimrand desire to secure byLetters-Patent, is: v Y
1.- The combination of a casing, an inner rotary cylinder having a Xed center Y of movement, a plurality of blades'extending through the cylinder` wall and having a center of movementolf the first-namedcenter,
and rocking glands'slidableon thebl-ades and carried in and heldlagainst 4lateral movement by the cylinder; the portions of the cylinder wall "at" opposite sides of theY rocking glands being held under yielding pressure against saidglandsQ Y 2.1 The combination'fof a casing, a revoluble cylinder mounted therein Iandhaving a circular wall providedgat intervals with gland seats and bifurcated portions atopposite sides of said seats andA also provided with means for yieldinglyV crowding 'the' bifurcated portions inwardly'to'take up wear, bladeshaving a center of movement 01T the center of movement of the cylinder Vand eXtending throughthe-gland seats, and Y rocking glands'disposed in said seats and yslidably receivingthew blades. "al1 v Y 3.*'The comb'nation of a cylinder wall havinga gland seat and bifurcated portions at opposite sidesthereo and also having means `connectedwith said rbifurcated por-- tions Vto take up wear, a blade extendingthrough' the seat, and 'aroclring gland disthe seatandslidably v'receivingthe Y `blade. f v A posedv in The combination of a circularV casing having portsat intervalsin its circular wall,
-curvilinear chambers at* opposite sides 'of the casing and communicatingf'wi'th: said: ports, piston cylinders'onjtheouter wall of said chambers, pistons )inA saidcylinders,
fioo
valves complementary'to. said 'ports and f connected with saidpistons, a conduit' con-` nected withf the vcurvilinear chambers, a
valve casing connected vwith said conduit and also with the interior of the circularl control valve in said casing, a rotary cylin# der mounted keccentri'cally inthe'- circular casing and havingfrocking bearings at intervalsj in itszf circular wall,- a stationary' casing andl havingl a conduitof its own, a Y
shaft Vmounted within `the?'c y'f'linder and 'olf thecenter thereof andv blades'fmounted to swing about'sa'idishaft and`fslidably arranged in'said*bearings. ,V
five cents each, by'addressing 'the 2Cammissiim'elf.ofrlfatentsV Y Washington, 03" f *y i l f
US1317056D Planooraph co Expired - Lifetime US1317056A (en)

Publications (1)

Publication Number Publication Date
US1317056A true US1317056A (en) 1919-09-23

Family

ID=3384537

Family Applications (1)

Application Number Title Priority Date Filing Date
US1317056D Expired - Lifetime US1317056A (en) Planooraph co

Country Status (1)

Country Link
US (1) US1317056A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3185102A (en) * 1964-01-13 1965-05-25 Thompson Ramo Wooldridge Inc Vane pump sealing glands
US3743451A (en) * 1971-05-24 1973-07-03 H Chapman Rotary engine
US3976403A (en) * 1974-06-24 1976-08-24 Jensen Robert L Rotary vane fluid pressure machine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3185102A (en) * 1964-01-13 1965-05-25 Thompson Ramo Wooldridge Inc Vane pump sealing glands
US3743451A (en) * 1971-05-24 1973-07-03 H Chapman Rotary engine
US3976403A (en) * 1974-06-24 1976-08-24 Jensen Robert L Rotary vane fluid pressure machine

Similar Documents

Publication Publication Date Title
US938911A (en) Propelling means for vessels.
US1317056A (en) Planooraph co
US1019856A (en) Rotary internal-combustion engine.
US1151568A (en) Internal-combustion engine.
US1232850A (en) Rotary engine.
US1138481A (en) Rotary engine.
US892443A (en) Rotary engine.
US1053767A (en) Rotary engine.
US1574976A (en) Rotary engine
US2466759A (en) Rotary power unit
US1422458A (en) Reversible fluid-pressure turbine
US610084A (en) Of same place
US1341328A (en) Plotigh
US606606A (en) Rotary engine
US1343331A (en) Rotary engine
US1176402A (en) Valve for engines.
US797869A (en) Rotary engine.
US821707A (en) Rotary engine.
US697075A (en) Rotating-piston engine.
US751694A (en) sheaeee
US1420009A (en) Rotary engine
US1515378A (en) Steam engine
US1514299A (en) Fluid-pressure engine
US454192A (en) white
US755161A (en) Rotary engine.