US948950A - Gas-engine. - Google Patents

Gas-engine. Download PDF

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US948950A
US948950A US34977306A US1906349773A US948950A US 948950 A US948950 A US 948950A US 34977306 A US34977306 A US 34977306A US 1906349773 A US1906349773 A US 1906349773A US 948950 A US948950 A US 948950A
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shaft
cylinder
series
vanes
chamber
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Dwight H Bennett
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/06Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H37/00Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00
    • F16H37/02Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00 comprising essentially only toothed or friction gearings
    • F16H37/06Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00 comprising essentially only toothed or friction gearings with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts
    • F16H37/08Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00 comprising essentially only toothed or friction gearings with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts with differential gearing
    • F16H37/0833Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00 comprising essentially only toothed or friction gearings with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts with differential gearing with arrangements for dividing torque between two or more intermediate shafts, i.e. with two or more internal power paths
    • F16H37/084Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00 comprising essentially only toothed or friction gearings with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts with differential gearing with arrangements for dividing torque between two or more intermediate shafts, i.e. with two or more internal power paths at least one power path being a continuously variable transmission, i.e. CVT
    • F16H37/086CVT using two coaxial friction members cooperating with at least one intermediate friction member

Definitions

  • nwmnr 3 sum, or nnooxmm, new roan.
  • FIG. 1 is a side elevation of such en invention.
  • Fig. 2 is sectional view of the lame. Big. is a vertical cross-sectional view onhnel 8 of Fig. 9.
  • Fig. 4 is a tiia a aectiodal view-oi one o the vanes I on Fig. 0 is a vertical longitudinal aectionaf view of the air inlet and compre-ion devices.
  • Fig. 7 is a detail view. of
  • Fig. is a detail view of the clutch nism inte betweenthe fan carrying 'ahaft of t e'compressing mechanism and the gear wheel which is connected with the actuating power.
  • the outer casing or cylinder of the en ne is indicated at 1. centric with the outer casing I construct an inner cylinder 8, 4, one part 3- extendmg from hea 2, or a considerable distanoe inward where it abuts a inst a rim of a set of hladee, and the otter Part, 4, j the rim of a succeeding set 0 blades to a )oint in line with the farther end of n 1, where the space between them is cloeetfhy an annular head, a.
  • the space between 1 on the outside and 8 and 4 outhe inside, is intended toconstitute a water jacket for the engine.
  • another cylinder 6 From the outer face of the annular head 5 another cylinder 6, extends longitudinally outward and is closed by a a central bore and. 7, having to acmmmodate the shaft, and its sleeve,
  • This c liuder 6 is pierced at a number of, places, tore sixteen, and the walls of each suci apcrturc are surrounded by flanges, 10, to the outer edges of which I secure an annular cylinder, 11, the interior face of which is aperture-d to register with the flanged apertures of cylinder 6.
  • stitute suflicient bearings for the slcm ed shaft. are rcfcrahly formed on the heads 2 and'7, buFit such bearings should be insnflicicnt, I could readily extend the shaft and mount it in willow blocks or other suitable supports.
  • lccrc 9 is fitted as closely to the s aft as possible without causing andue friction, and extends from a point some inches without the line of head 7 to a point slightlyv within the line of the head 5 of the main c linder. At the inner cud it carries a circu or disk 18 ri idl secured to it and of a diameter to titc ose y within the cylindcr 4.
  • Ncxtin succession to disk 13. surrounding; said sleeve 9 I place a wheel composed o a hub 15, rad an apertnred disk 17 covering its outer face and a partial rim in the form of a flange. 18 extending inward from the edge of disk 17 over the edges of arms 16, to a line just within that of the circle of apertures in cylinder 6. The inner outcr corners of the arms 16 are secured rigidly'to a ring 19,
  • Dial: 14 is provided with a number (here 16) of radially cut apertures, evenly spaced, eut,froni near the center outward for a distance usuallv (hut not nccesaaril ahont one-sixth of the diameter of said (hi; the width being about e ual to the space between the fll'HlH or partitions to.
  • Disk 17 is also provided with radially cut apertures 24, of a length and width corrw spending titres
  • Disk 20 has four radial aperturea, 25, evenly spaced and in length equaling apertures 22 and 24, with which they register but in width equal to the space lXftween alternate arms 16, that is to t ie space occu ied by two compartments 50, minus lllt' widti of the walls, and its thin 'a, -t, is provided with our apertures evenly spaced which .will at appropriate times I't iatcr with the apertures in lit! e 18 and er indcr 11.
  • Disk 13 has four ra ial a wrturea, 213, corresponding in width with the space hetwcen partitions l6 lus the thickness of the partitioia and in engtli extending from quite ii iii the sleeve 1) to a line jurt within the line ot the iii-are t edge of vanes 1".
  • film-ii- 1.2 t-Xtuiiils inward on - ⁇ hat't is to ll -ai -l -lm-viadjacent to wiiil ⁇ '2t ll("-- '31.
  • l Hi llllll a third *-"I "-t UrXttl'ith. L3.
  • Gear 45 meshes with a gen r 47 mounted on sleeve 12 and pulley l t'ttt'l'lt a belt 48 ruunin to shaft it and thereby any power developed by the movement of vanes 35 will be transmitted to shaft ti.
  • Sparking plugs'lt are located in each explosion chamber 50, (formed by hub 15. partitions 10, cover 17, disks 13 and 20, langea t8 and 2t and ring 10), and from thcni. wires, preferably buried in said pai'ti llulw, run to contacts 51 at.
  • l iui'eter is the car l iui'eter. It consists of a long tube open at. one end and at the other end communicating with tho equalizing chamber 33 lyin r within cylinder i lit-tween head 'i' and'dis 14.
  • l mount a slut ft 56 and on that shaft a balance wheel 57 whose spokes SS-arc vanes,- and a siu'itrfi of fan blades 59 all pitched in the hill? direction.
  • the bra cket77 a is bifurcated or forked and through readed acrew 86 provided
  • the thread of screw'86 carries an arm 88, from the end of which-a rod cord or line extends down to the hub wheel 79, to which it is-securely attached "means of a ring or collar thereon.
  • channels 91 through the thickeat parts of vanes 29 lead to the ope pace m and cylinder 1. Similar throufh the thickest 40 5:. o! vanes 85 and open in o the same at 'r i ends. These channels 92 extend cut I space to e sur ace shaft that the passage turning of t c .8 in llelve 12, the face of the shaft is from a see of the a aft.
  • disk-'13 will begilrtoiopcn ports 23 0f said four. chambers 50, thc'positionsof disk 13 and disk'2O 'ltcing co ad pasted on sleeve 9 as to produce such ctlect: 'hcn apertures 23 are about one-third .open (any'othcr distance may be selected if desired) the circuit closer! 52 reach and make contact between the contacts 51 of the tour chambers 50 already .90 named, s iarks are created at the spark plugs 49 and t 1e charges in those four chambers are tired.
  • disk 13 again closes ports 23 and in due course the movement of disk 20 brings the apertures in its llange 21 to register with the said four discharged chambers 50 and any remninin gas therein'may escape through the flan ports in cylinder 0 and into and through the annular chamber 11 and out of its exhaust 98, being hastened in that movement by the fresh incomin r explosive mixture which will by that time ie againcnteringthose chambore 50 under pressure.
  • the rcepectivcly Succeeding i'our (:hambcls .lllvarc likewise charged.
  • chamber 99 The purpose of chamber 99 is to cll'cct amore evenly continuous movement of the van and therefore the shaft than if the dirt-harm's were directly against the vanes.
  • the gases fill a chamber and in it become a species of butler. From thence they flow agatnat each set of vanes. and not merely the ones opposite the diacharginp chambers. Again the incomin gases ldt to the general pressure in chain r99 which acts as a reservoir from which the power is continually roceeding with a less pulsatory character than would otherwise be the ease. Meanwhile the shaft.
  • a gas en ine the combination of a cylinder, at sha t extending through said cylinder, a series of radial explosion chambers secured to the c 'liuder arranged about said shaft and provided with a series of gas inlets and outlets.
  • a rotary sleeve surrounding said shaft and carrying two disks, each provided with a series of apertures, those in one disk'being arran ed to suceemively register with the gas ililets, and those in the other to successively register with the gas outlets. and mechanism interposed between the said sleeve, and the shaft, wherebv one will partake of motion of the other, all substantially as set forth.
  • a cylinder extendin through saidocylinder an explosion eluun r, an equalizing chamber, a port in the exiplooion chamber, a port in the equalizing ciamber, registering with that in the explosion chamber, and a movable a iertured disk interposed between ut so connected with the shaft as to move in unison therewith, whereby passage from one to the other of said )orts will )0 alternately opened and close all substantially as set forth.
  • valves interposed tween the equalizing and the explosion chambers and between the explosion chambers and the said third chamber, substantially as set forth, whereby the gas may pass from the equalizing to the respective explosion chum iera in succession and the motive fluid may pass frour the reapcctive explosion chambers to the and third 0 mmber. for thc purposes set forth.
  • a gas engine the combination of a cylinder, a shaft extending through said cylinder, a series of radial explosion chambers secured to the cylinder arranged about said shaft and lets, a don the side and one at the ends of said chambers, an annular chamber surroundin the explosion chambers and provided wi an outlet and a series of apertures, registering ies ieetively with but at a distance om the out ets in the ends of the explosion chambers, a rotary sleeve surrounding said shaft and carrying two disks, one be.
  • a gas engine the combination of a cylinder, a shaft extending through said cylinder, a series of radial explosion chambers aecnred to the cylinder, arran about the -ahaft and provided with apnea of gas mlets and outlets, an equalizing chamber adjacent to the explosion chambers, means for forcing an explosive mixture into said cquah'i 15 izing chamber, outlets therefrom'regialering with the inlets of the explosion chambers, a,

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

' D. H. BENNETT.
Slave u for.
w; hwaacb tam/(W 14:41.. e 8e...
D. H. BENNETT.
- 0A8 SIGIIB.
uruonml nun no. n. ma, 948,950.
BUM Fob. 8,1910.
4 IIBII'l-llllf 0.
E .& i
UNITED STATES PATENT ormcn.
nwmnr 3; sum, or nnooxmm, new roan.
OABSNGINE.
948,950. W 1mm l'ltent Patented Feb. 8, 1910.
. Application lied December 38, 1006. lertal 110. 349,773.
' Toallwhomitmay other a sleeve 12, entirely independent of Be it known that I, Dwtom' H. BP-KNII'I', sleeve 9. Bosses or other devices to conm xiiii'iii'd a citiaen of the United States of America, reaidi at Brookggn, Kings county, New Yer ve invent certain new an useful Improvements in Gas-Engines, of which the f owing ia a specification.
My invention relates to gas engines of the class called turbines, and 1t devicea and combinations of devices hereinaftuand claimed. Figure 1 is a side elevation of such en invention. Fig. 2 is sectional view of the lame. Big. is a vertical cross-sectional view onhnel 8 of Fig. 9. Fig. 4 is a tiia a aectiodal view-oi one o the vanes I on Fig. 0 is a vertical longitudinal aectionaf view of the air inlet and compre-ion devices. Fig. 7 is a detail view. of
one of the orated tubes of the carbureter. Fig. is a detail view of the clutch nism inte betweenthe fan carrying 'ahaft of t e'compressing mechanism and the gear wheel which is connected with the actuating power.
The outer casing or cylinder of the en ne is indicated at 1. centric with the outer casing I construct an inner cylinder 8, 4, one part 3- extendmg from hea 2, or a considerable distanoe inward where it abuts a inst a rim of a set of hladee, and the otter Part, 4, j the rim of a succeeding set 0 blades to a )oint in line with the farther end of n 1, where the space between them is cloeetfhy an annular head, a. The space between 1 on the outside and 8 and 4 outhe inside, is intended toconstitute a water jacket for the engine. From the outer face of the annular head 5 another cylinder 6, extends longitudinally outward and is closed by a a central bore and. 7, having to acmmmodate the shaft, and its sleeve,
9. This c liuder 6 is pierced at a number of, places, tore sixteen, and the walls of each suci apcrturc are surrounded by flanges, 10, to the outer edges of which I secure an annular cylinder, 11, the interior face of which is aperture-d to register with the flanged apertures of cylinder 6.
In the heads 2 andt', which are centrally hored for the )urposc, I mount the main shaft, 8, one end carrying a sleeve 9 and the consists in the .7
It haaa head, 2. n-'
stitute suflicient bearings for the slcm ed shaft. are rcfcrahly formed on the heads 2 and'7, buFit such bearings should be insnflicicnt, I could readily extend the shaft and mount it in willow blocks or other suitable supports. lccrc 9 is fitted as closely to the s aft as possible without causing andue friction, and extends from a point some inches without the line of head 7 to a point slightlyv within the line of the head 5 of the main c linder. At the inner cud it carries a circu or disk 18 ri idl secured to it and of a diameter to titc ose y within the cylindcr 4. Ncxtin succession ,to disk 13. surrounding; said sleeve 9 I place a wheel composed o a hub 15, rad an apertnred disk 17 covering its outer face and a partial rim in the form of a flange. 18 extending inward from the edge of disk 17 over the edges of arms 16, to a line just within that of the circle of apertures in cylinder 6. The inner outcr corners of the arms 16 are secured rigidly'to a ring 19,
ial partition arms 16,
trian alarm cross section (as shown in Fig.
rial in that regard, its main purpose being to attach the-partitions disk 17 and rim 18, firnily'to the stationary cylinder and thus hold them also stationary, and, in conjunction with said huh. pal-ti tions and disk, to constitute a Stl'its of chain:- hers to be more particularly described hereafter. Beyond (ink 17 a partition 1t ex.- tcnds from the wall of cylinder 6, inward to a close fit with sleeve 1). It has a series of apertures .22 corresponding in number, size and relative location with the apertures 24 formed in disk 1?. 'Bct-wecn dish 1! and partition 14, I locate a third disk 20, rigidly secured to sleeve 9, so that its movement may he synchronous with that of disk 13, and
so nearly filling the space between 17 and 14' v as to just permit its turning without friction between it and them, and extending ltl, the hub, li i, thc
outward to the innerfate of cylinder 6 and there flanged or connected to a tliingi- 21. which extends inwardly, parallel with thiahaft, lwtween flanged! and the outer fanof ring 10 on the one side and cylinder 3 on the other./to a line beyond the circle of apertures in cylinder 6, and utilistnntiully to head 5. Dial: 14 is provided with a number (here 16) of radially cut apertures, evenly spaced, eut,froni near the center outward for a distance usuallv (hut not nccesaaril ahont one-sixth of the diameter of said (hi; the width being about e ual to the space between the fll'HlH or partitions to. Disk 17 is also provided with radially cut apertures 24, of a length and width corrw spending titres Disk 20 has four radial aperturea, 25, evenly spaced and in length equaling apertures 22 and 24, with which they register but in width equal to the space lXftween alternate arms 16, that is to t ie space occu ied by two compartments 50, minus lllt' widti of the walls, and its thin 'a, -t, is provided with our apertures evenly spaced which .will at appropriate times I't iatcr with the apertures in lit!" e 18 and er indcr 11. Disk 13 has four ra ial a wrturea, 213, corresponding in width with the space hetwcen partitions l6 lus the thickness of the partitioia and in engtli extending from quite ii iii the sleeve 1) to a line jurt within the line ot the iii-are t edge of vanes 1". an
til
that of ring 19. For a short tllhlllll ft! within disk 18, the cylinder 4 is left meant to form a rv ervoir of power, 09. Succe ding space 09, I place a circular series of vanes 24; secured to a sleeve or hub .2? surrounding aliiift 8 and provided with a rim 133, which as here shown constitutes the \'linder itself. Clorely following vanes 'J t is a second series of vanes 2t, lnit these are.
' l lt' too great rotarymotion the air wou tilllt't'\\'i. 'tt acquire. ltlt.-'llt"-' with gear tr. on shaft G3, which in Similar l)l'llt.'t" 2H and 4t, str ngth n and tn the length and width of apcr-,
support in place rwpectivcly the lllllt'l' coih Z llt\'t'l' lltlt-'h. uiidcr ll- :ii-ipiirvd momentum of parts 23 and 1 of the inner cylinder.
film-ii- 1.2 t-Xtuiiils inward on -\hat't is to ll -ai -l -lm-viadjacent to wiiil \'2t ll("-- '31. l Hi llllll a third *-"I "-t UrXttl'ith. L3. llll llll."- rim -2'' lt' tltf 'l't tl" diw-iila-d to lit n L'-' itt-t th -liiiint'cri-d --urf;icioi" lmi-d -H ltt'l that of i tliiidi'r it on the tilli 't'. The pi t' 'nli'w ,5 is, in general, similar till to that of \tlllts "2 Surat-ding vanes 35, are tixcd [\ttllillfllh'. 37. ext nding radially from a hub 38, Hit-rounding \lt't'\'t l2. to and ht't'tttcil to the shell ll. The space It!) ll(.l\\tCll the outer line of partitions 37 and llt'tltl 2, is no open chiinilwr and front it, an exhaust )ipe it! extends to a convenient point of discharge. A lly \\'ltt'|'l 4;. is mount ed on shaft 8 and in a hrackct 43 l'nioiint a shaft -14 carrying a .:eaiwheel 45 and a pulley wheel -l i. Gear 45 meshes with a gen r 47 mounted on sleeve 12 and pulley l t'ttt'l'lt a belt 48 ruunin to shaft it and thereby any power developed by the movement of vanes 35 will be transmitted to shaft ti. Sparking plugs'lt) are located in each explosion chamber 50, (formed by hub 15. partitions 10, cover 17, disks 13 and 20, langea t8 and 2t and ring 10), and from thcni. wires, preferably buried in said pai'ti llulw, run to contacts 51 at. the inner face of lllt' central aperture in disk 17 and four circuit closers .32 are hcddctl in the face of t-tlt't\'t7 9, evenly spaced, in such positioim that they register wit 1 contacts-i 5t and, upon the movement of said sleeve ll, will sequentially close the respective (:lt't'llllrt from a 'source f electrical power. not shown, to the respectit'e spark plu s.
54 is the car l iui'eter. It consists of a long tube open at. one end and at the other end communicating with tho equalizing chamber 33 lyin r within cylinder i lit-tween head 'i' and'dis 14. In standards 55 in said tube, l mount a slut ft 56 and on that shaft a balance wheel 57 whose spokes SS-arc vanes,- and a siu'itrfi of fan blades 59 all pitched in the hill? direction. lludial partitioinc tit) of Might width hut 'tipprcciailc lt'ltgllt ltt a dire tion parallel with the shaft bin-arc iiiltt])ti 't'(l in the seriea of tuna to i'..ti-i'iupt hi litiit'i' cameo a Th. a small tube 78'leade from the carllueter to the uppker part of the ti tly eolene ten (not shown) an analt-er be 74, shorter than tube 78, leads 6 the lower part of said tank to the q'ace between heads 70.
On that rt of shaft 8 projectin out 7 and beyond the end offieeve O, I mount a friction disk 75. In two brack- 76 and 77 Jxojecti t a-sliaft.7 and feet cred on' shaft 78 to more up and down thereon, I at a friction wheel 79 so as to make frietiona contact with Near the upper end of shaft 78 I whezl'SO and re(an a es in m a cot seen to bracedb beach gig I i ind from et 77, I secures aecon diskuglacedandarra tomake 1th w 6e! 80. Shaft also ear-.
tley gout whighda belt 85 o a v a exten also" 9 outside of head 7. The bra cket77 a is bifurcated or forked and through readed acrew 86 provided The thread of screw'86 carries an arm 88, from the end of which-a rod cord or line extends down to the hub wheel 79, to which it is-securely attached "means of a ring or collar thereon.
is hollow for a considerable porlersh and a tube 90 is connected its open a suitable joint. From space 98 within the hollow'shaft,
.. or channels 91 through the thickeat parts of vanes 29 lead to the ope pace m and cylinder 1. Similar throufh the thickest 40 5:. o! vanes 85 and open in o the same at 'r i ends. These channels 92 extend cut I space to e sur ace shaft that the passage turning of t c .8 in llelve 12, the face of the shaft is from a see of the a aft. through head 8 into the ca 97, betwem cylinders 1 and 8 and anomr diacharfe tube .98 leads from the annular 1 so a throu tubes 71 become charged the gas r a king material isauing from hoes 72 and willpese on and into equalizing mher 58- ea an explosive compoun Further motion otfahaft 56 and, its vanes 59 from head 7, I
' plosive mixture from laced and 'ary an arm 82 extendin will comprem the mixture in chamber 53. es Now the ehflft 8 is also started and through the connections already mentioned its motion will be communicated to sleeve 9 and its rigidly attached disks and 13, their motion icing of course always .synchronouta, The motion of disk 20 will speet ily cause it to be in to uncover apertures 22 and 24 and thereby provide free passage for the exc amber 53 intofour evenly spaced Cllfill'lbfll'fi 50. Not only so, but as disk 20 movceon, it. will uncover the four chambers 50, respectively succecdin those first uncovered and thus throughout its motion. When four chambers 50 have thus been filled under pressure,'the further movement of disk 20 will close thecntrance ports and at the samc instant, the movement of.
disk-'13 will begilrtoiopcn ports 23 0f said four. chambers 50, thc'positionsof disk 13 and disk'2O 'ltcing co ad pasted on sleeve 9 as to produce such ctlect: 'hcn apertures 23 are about one-third .open (any'othcr distance may be selected if desired) the circuit closer! 52 reach and make contact between the contacts 51 of the tour chambers 50 already .90 named, s iarks are created at the spark plugs 49 and t 1e charges in those four chambers are tired. The gases produced by the explosions rush through ports 23 into chamber 99 and thence between thec'ntire series of vanes 96- 26, then 29 and then 35 and the pitch of each succeeding set of vanes'bcing reversed, such 7 passage will cause the vanes 29 to rotate in one direction, carrying the-shaft 8 with them,
and the vanes 35 to rotatc in the o iposite direction, carrying sleeve 12 with t em, such power as is developed by such rotation of s eeve 12 being added to the shaft power through gears 47 and 45, pulley '46 and belt 48. 1025 When the explosion ha. taken place and the gas passed out a described, disk 13 again closes ports 23 and in due course the movement of disk 20 brings the apertures in its llange 21 to register with the said four discharged chambers 50 and any remninin gas therein'may escape through the flan ports in cylinder 0 and into and through the annular chamber 11 and out of its exhaust 98, being hastened in that movement by the fresh incomin r explosive mixture which will by that time ie againcnteringthose chambore 50 under pressure. The rcepectivcly Succeeding i'our (:hambcls .lllvarc likewise charged. closed, opened and their charges 120 exploded and delivered into chamber 99and thence to their work as described, and the cycle continues so long as material is furnished and movement permitted. The purpose of chamber 99 is to cll'cct amore evenly continuous movement of the van and therefore the shaft than if the dirt-harm's were directly against the vanes. The gases fill a chamber and in it become a species of butler. From thence they flow agatnat each set of vanes. and not merely the ones opposite the diacharginp chambers. Again the incomin gases ldt to the general pressure in chain r99 which acts as a reservoir from which the power is continually roceeding with a less pulsatory character than would otherwise be the ease. Meanwhile the shaft. 8 has developed motion under the influences named and thenceforth will actuate all f its connected devices, including shaft 6. Its movement of course causes the air forced through pipe 73 to create a pressure on the gaaolene tank and when the pressure in chamber as and tube 54 is momentaril lest ened by the opening of ports 22 and 2 thatpressure already in the gasolene tank acting through the shorter pipe 74 will cause the gssolene enterin below heads 70 to issue in a jet like spray rem holes 72 in tubes 71 and thereb continue to furnish the material needet for the explosive mixture. If shaft 8 should momentarily slow down the action of fans 59 would not necessarily be thereby retarded, for the balance wheel may for that moment proceed at its already acquired speed, clutch 69 being alwa s ready to again seize and turn shaft 56. w ten the speed of shaft 8 again equals that of shaft 50. As they issucfroni between the blades 35, the gases will have acquired a rotary motion of considerable force and might therefore create an objectionable noise if nothing intervened between said blades andexbaust 40. I have therefore introduced the radial plates 37 at this place to guide those gases in the exit and in overcoming the rotary motion muned, obviate the objection the noise might otherwise present. To cool the parts I introduce a stream of water through tube 90. It passes thence to and through space 93 and y centrifugal force 'will tlo out through chamber til and ports 94 an '9" and channels 92 into chamber 07 and ti nce to and out of discharge tube on. tluis furnishing a very convenient means for eii'eeting the desired end; and to enhance the cooling etlect. l sometime-s make so iplementary channels in the thick parta of t tea-anesleading from and to channch ill and it: (as indicated in dotted lines in Fig. 4). 1
As will be manifest. there are times when it is advisable to change the rate of explosion. relative to the revolutions of the shaft and this may herein be rcadilv accoin dished (within the limits set by the location of wheel 80) by rotating screw 86 and thereb lifting or lowering arm 88 and its link which will carry wheel to a lar r or smaller track upon the face of disk 9 and thus decreaseor increase its s as related. I do not limit myself to-t to exact form. proportions or arran meat of tarts herein shown and desert Many oi them'may be changed in various particulars and some may be omitted without departing from the spirit of my invention. I do not limit myself to the number of vanes employed nor to the number of ditferent series of vanes nor to any other details other than as set forth ,m the clatmaor necessarily implied by the terms used.
What I claim'as m invention and desire to'secureby Letters atent, is: 1. In a gas engine, a cylinder, a shaft. extctaling through said cylinder and provided wt said shaft and secured to said cylinder, a series of vanes surrounding said shaft and secured thereto, a series of vanes mounted on said'slceve, each series of vanes having its ccdin series. reversin gears interm said s eeve and said shaft and means for forcin gases between said vanes, all substantially as set forth.
2. In a gas engine. the combination ofa cylinder, a shaft extending through said cylinder, a series of vanes surrounding said shaft. and a series of radial partitions succeeding said vanes and interposed between them and the exhaust. all substantially asset forth.
8. In a gas engine, the combination of a cylinder, a shaft extending through said cylinder, a series of vanes surrounding said shaft, a series of explosion chambers, an intcrmediutc chamber between the explosion chambers and the vanes. pas ages from each explosion chamber to the one intermediate chamber, approximating in size the proximate face of the contiguous explosion chamher. and valves for controllin said pas sages; the explosion chambers. t e inn-sages into the intermediate chamber and t It intermediate chamlwr opening into the vane containing cylinder. lines. \\'llereb \"the motive tluid created i'n'the explosion chambers may pass in a right has to and im )illgt directly upon the vanes, all substantiuily as set forth.
4. In a gas engine. the combination of a qvlinder, a shaft extending through said cyla sleeve, a series of vanes surrounding wing arranged in right pitch arranged reversely to that of thgdpre-bz I tate too
indcr. a sleeve mounted on said shaft. pcraaid ports,
shaft, one of them provided with a set screw whereby it mav be adnsted on its shaft. and the other feathered t ereto but movable n and, down upon said shaft, together witii means for moving it. thereon, all substantially as set forth.
5. In a gas en ine, the combination of a cylinder, at sha t extending through said cylinder, a series of radial explosion chambers secured to the c 'liuder arranged about said shaft and provided with a series of gas inlets and outlets. a rotary sleeve surrounding said shaft and carrying two disks, each provided with a series of apertures, those in one disk'being arran ed to suceemively register with the gas ililets, and those in the other to successively register with the gas outlets. and mechanism interposed between the said sleeve, and the shaft, wherebv one will partake of motion of the other, all substantially as set forth.
6. In a gas engine, the combination of a cylinder, a shaft extendin through saidocylinder an explosion eluun r, an equalizing chamber, a port in the exiplooion chamber, a port in the equalizing ciamber, registering with that in the explosion chamber, and a movable a iertured disk interposed between ut so connected with the shaft as to move in unison therewith, whereby passage from one to the other of said )orts will )0 alternately opened and close all substantially as set forth.
7. In a gas engine, the combination of an equalization chamber, a series of explosion chambers and a third chamber or s nice anccecding the ex loaion chambers an located intermediate t e explosion chambers and the vanes, pas ages from the equalization chamber to the explosion chambers and from the ex loaion chambers to the succeeding third 0 iamber, the latter series of passages respectively approximating in awe the prommate face of the conti nous explosion chamber. valves interposed tween the equalizing and the explosion chambers and between the explosion chambers and the said third chamber, substantially as set forth, whereby the gas may pass from the equalizing to the respective explosion chum iera in succession and the motive fluid may pass frour the reapcctive explosion chambers to the and third 0 mmber. for thc purposes set forth.
8. In a gas engine, the combination of a cylinder, a shaft extending through sa d cylinder,'a series of radial explosionchambers secured to the cylinder arranged about said shaft and irovided with a series of nsinlets, a don ile series of outlets, e series at the side and one at the ends of said chum hers, a rotary sleeve surrounding said shaft and earr ing two disks, one beyond the explosion c numbers, rovided with a series of with the gas outlets on the sides of,thc explosion chambers, the other on the opposite s de of the explosion chambers bein provided with a llan extending over t a and outlets of the exp osion chambers, both face and flange being rovided with'a series of a rturcs arranget to successively register t ose in the flange with the end outlets and those in the face with the inlets, together with mechanism interposed between the shaft and the sleeve whercb one will artake of the motion of the otli er, all an ntially as set forth.
9. In a gas engine, the combination of a cylinder, a shaft extending through said cylinder, a series of radial explosion chambers secured to the cylinder arranged about said shaft and lets, a don the side and one at the ends of said chambers, an annular chamber surroundin the explosion chambers and provided wi an outlet and a series of apertures, registering ies ieetively with but at a distance om the out ets in the ends of the explosion chambers, a rotary sleeve surrounding said shaft and carrying two disks, one be. and them:- ploaion chambers rovidcd wit a series of apertures arran to successively register with the gas out eta on the sides of the explosion chambem, the other on the oppoaite side of the elfrploaion chambers bein provided with'a ango extending over t e end outlets of the ex losion chambers, and between them and t to apertures in the annular chamber, both face and flange being rovided with a series of apertures arran to successively register, those in the flan with the end outlets and those in the face with the inlets, to ther with mechanism interposed between t to shaft and the sleeve whereby one will partake of the motion of the other, all
substantially as set forth.
10. In a gas engine the combination of a cylinder, a shaft extending through said cylinder, a series of radial explosion chambers aecnred to the cylinder, arran about the -ahaft and provided with apnea of gas mlets and outlets, an equalizing chamber adjacent to the explosion chambers, means for forcing an explosive mixture into said cquah'i 15 izing chamber, outlets therefrom'regialering with the inlets of the explosion chambers, a,
rota sleeve surrounding said shaft and carrying two disks, each provided with a series of'aperturea, those in one their being arranged to successively register with the gas inleta-ofthe explosion chamber, and those in the other to successively-register with the gas outlets from said ehamber meuns for communicating motion from said shaft to said sleeve, an intermediate chamber, in the cylinder, .inunediatel succeeding the exploapertures arrange to successively register l sion chamber and a opted to receive gases provided with a series of gas inle series of outlets, one series at land therefrom, s series of vsnes lttf- 5 mm to this specification in the resence of round the shsjt and secured to the cylmtwo subscribing witnesses, this 15th day of dersseeodsenesofvsnessecurcdtothel 906 shalt but via; their pitch the reverse of those secured to the calinder, sad an exhaust Witnenes: outlet; s11 suhstsntis Is asthma Junel ss set forth. Claus B. D v 3 end, I has signed my vA. G. N. mi ht.
DWIGHT H. BENNET'1.
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