US875515A - Rotary engine. - Google Patents

Rotary engine. Download PDF

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US875515A
US875515A US37542407A US1907375424A US875515A US 875515 A US875515 A US 875515A US 37542407 A US37542407 A US 37542407A US 1907375424 A US1907375424 A US 1907375424A US 875515 A US875515 A US 875515A
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Prior art keywords
vanes
tongue
disk
flanges
pipe
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US37542407A
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Mortimer Frauenthal
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00Machines or engines of reaction type; Parts or details peculiar thereto

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  • . ⁇ l invention is an improvement in rotary engines. and eonsists in certain novel eontruetions and combinations of parts as will he here-inal'ter des rihed and elaimed.
  • Figure I is a vertieal eetion through the engine.
  • Fig. 2 is a plan view of the rotor and supporting frame, and
  • Fig. I; is a detail perspeetive view of the inlet pipe and the adjustable tongue.
  • the rotor comprises a disk (I seeured to a shalt u, journalled in hearings II. on a supporting frame I).
  • the peripher v ol the disk at the sides thereof is provided with radial annular llanges u, and a plurality ol" radial blades, wings or vanes a are arranged transversely of the periphery of the disk he tween the flanges, the said vanes extending from flange to flange and heing ol' lzfih't'l h ight than the said flanges, as shown in Figs. i and 2.
  • the upper face ol' the pipe at its free end is provided with an upwardly projecting flange 1', having spaeed slots e, for a purpose to he hereafter deserihed and the flange is blurred against the pipe. h v ahutments 1".
  • the lower face of the pipe (I is also provided wit. longitudinal grooves c for reeeiving the llanges ol' the disk, and the HJltl pipe is o arranged with relation to the disk, that the lower grooved l'aee thereof is spaced apart a slight. distaisze from the free ends of the tongues, as shown in Fig. l-
  • a directing tongue 1) is adjustahlv connected with the free end of the inlet pipe, the 1 easing having an iuottve thud having one laee t'tHYtt to eorresaid tongue comprising open hottom, as shown Hi lugs] and 35, and
  • the inner url' 'e f the upper fare of the tongue is eat 2:. rs shown at ii in Fig. l to properly lielleet ttt dil'tt't the motive 'llltid against the rear hir s ol' the hlades or va re and the extreme outer end of the tongue is -urved eoneentri aflv as at (F with the disk and such eurveo.
  • tn'l aee is adapted for engagelnent the free ends of the tongue during the rot: tion of the disk.
  • the improved engine is esperiallv adapted for use as an explosive engine. that is, with mot ive fluids whose expansion is of short duration.
  • . ⁇ n v .suitahle meehanism may he lnade use of for su ur-l aparthe motive fluid at predetermined intervals, hni sinee surlt meehanism forms no part of my present invention, 1 have not thoughtit neeessary to further deserihe the samev l elaim l.
  • rotary engine eomprising a disk supported fora rotary movement and provided at eaeh side of its )tll
  • said inlet provided with a flange at its free end.
  • said flange having spaeed slots, a tongue for defleet-ing the motive fluid against the vanes, Said tongue having a flange abutting against the flange of the inlet pipe and provided with openings registering with the slots, bolts traversing the openings and the slots for seeuring the tongue to the pipe, said tongue having grooves for reeeiving the flanges of the disk and having a portion at the free end thereof eurved ('oneentrieallv with the disk 5 and against whieh the ends of the vanes move.
  • a rotary engine comprising a disk supported for rotary movement and provided at. 1 ea'eh side of its peripherv with annular radial flanges and with radia wings or vanes arranged transversely, the said ones being of lesser height than the flanges and extending between the flanges, an inlet pipe for the l motive lluid having one face curved to correpath of travel of the free ends of the vanes and provided with grooves for receiving the flanges and a tongue for de- 5 fleeting the motive lluid against the vanes and ('onneeted with the end of the inlet ripe and adjustable toward and from the d grooves for pipe being 1 i l l i l isk, said tongue having grooves for reeeiving the l flanges and having a portion at the free end 1 thereof eurved t'oneentrie with the disk and l against which the free ends of the vanes or wings move.
  • a rotary engine eomprising a disk supported for rotary movement and provided 1 with the pipe with radiai wings, or vanes, arranged trans versely of the periphery thereof, an inlet pipe for the motive fluid having one face curved to correspond with the path of travel of the free ends of the vanes, a tongue connected with the inlet pipe for deflecting the motive fluid against the vanes, said tongue having a portion at the free. end thereof curved coneentrie with the disk and a ainst which the ends of the hlades move, am means whereby to adjust said tongue toward and from the disk.
  • a rotary engine eomprising a disk supported for rotary moven-ientand provided with radial vanes or wings, an inlet pipe for he motive fluid having one of its faces arranged adjaeent tothe path of travel of the free ends of the vanes, a tongue connected with the pipe for defleeting'the motive fluid against the vanes.
  • said tongue hein" adjustahle toward and from the disk and aavin' a portion at the free end thereof against which the ends of the vanes move.
  • a rotary engine eomprising a disk supported for rotary movement and provided with radial wings or vanes, an inletpipe for the motive fluid, and having one of its faces arranged adjacent to the path of travel of the tree ends-of the vanes, a tongue adjustably eonneetedwith -the ipe for deflecting the motive fluid against t he wings or vanes, said tongue having a portion at the free end thereof against which the ends of the vanes move.
  • a rotary engine eomprising a disk supported for rotary movement and provided on its periphery with radial vanes and with radial annular flanges of greater length than the vanes,'het.veen ⁇ Ylllt'll the vanes extend, an inlet pipe having one of its fares arrzmged adjat'ent to the free end of the vanes and between the flanges. and a tongue eonneeted for deflertin the motive fluid against. the vanes, the, free end of said tongue having a. portion bet-ween the flanges curved eoneentrie with the disk and against which the free ends of the vanes move.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Description

No. 875,515. PATENTED DEC. 31, 1907. M. FRAUENTHAL.
ROTARY ENGINE.
APPLICATION FILED MAY 24, 1907.
INVENTOR WITNESSES A Tram/53's ROTARY ENGINE.
Specification of Letters Patent.
Patented Dec. 31 ,1907- Aypliezuon iie". 311:: 2-1. 1907. Serial NF:- 375-424.
To all whom it may cuuu rn:
Be it known that l, )lon'rmit': FlLH'i-ZN- "UL-u, a citizen of the ['nited $tatt's'. and a residentof Conway, in the county of Faulkner and btate of Arkansas. have ivented certain new and useful lmprovelnens in liotar Engines, of whie-h the following is a speeilieation.
.\l invention is an improvement in rotary engines. and eonsists in certain novel eontruetions and combinations of parts as will he here-inal'ter des rihed and elaimed.
Referring to the drawings, forming part hereof. Figure I is a vertieal eetion through the engine. Fig. 2 is a plan view of the rotor and supporting frame, and Fig. I; is a detail perspeetive view of the inlet pipe and the adjustable tongue.
in the present embodiment of my invention, the rotor comprises a disk (I seeured to a shalt u, journalled in hearings II. on a supporting frame I). The peripher v ol the disk at the sides thereof is provided with radial annular llanges u, and a plurality ol" radial blades, wings or vanes a are arranged transversely of the periphery of the disk he tween the flanges, the said vanes extending from flange to flange and heing ol' lzfih't'l h ight than the said flanges, as shown in Figs. i and 2.
.B'aekets b projeet upwardly from the I ante B and supported u ion the upper ends ul' the brackets" is the motive fluid inlet pipe (Y. the said pipe heing reetangoh.r in eross section, a shown in Fig. 23, and the lower face of the said pipe :uljaeent to the fr e end 'Ulll't'fll is eurved to eor espond with th path of travel of the free ends of the lnlades It".
The upper face ol' the pipe at its free end is provided with an upwardly projecting flange 1', having spaeed slots e, for a purpose to he hereafter deserihed and the flange is blurred against the pipe. h v ahutments 1". The lower face of the pipe (I is also provided wit. longitudinal grooves c for reeeiving the llanges ol' the disk, and the HJltl pipe is o arranged with relation to the disk, that the lower grooved l'aee thereof is spaced apart a slight. distaisze from the free ends of the tongues, as shown in Fig. l-
A directing tongue 1) is adjustahlv connected with the free end of the inlet pipe, the 1 easing having an iuottve thud having one laee t'tHYtt to eorresaid tongue comprising open hottom, as shown Hi lugs] and 35, and
.having its sides provided with grooves (l for;
thr ugh the inlet pipe reeeiving the flanges ol' the di k. Th inner end of the easing i provided with an upwardly projeeting flange d hraeed against the ea ing h ahutments (1 and provided with openings 1/. registering with the slots hel'ore deserihed when th flange ol' the tongue nlnlt against the flange ol' the inletpipe. Bolts 1! traverse the sl ts and openings an nuts :1 engage the holts l'orseeuring the parts t-rgether.
The inner url' 'e f the upper fare of the tongue is eat 2:. rs shown at ii in Fig. l to properly lielleet ttt dil'tt't the motive 'llltid against the rear hir s ol' the hlades or va re and the extreme outer end of the tongue is -urved eoneentri aflv as at (F with the disk and such eurveo. tn'l aee is adapted for engagelnent the free ends of the tongue during the rot: tion of the disk.
in o a' r.-uiou the motive fluid is admitted and i direeted l) the surl'aee 1/ agauetthe rear lures ol' the hlazdes or vanes. thus eausin 't'ne disk to rolate.
.\s the hlades or vane pass from eontart \\llll lllt .sttl'l at't iii! motive lltlltl permitted to exhaust. llt'l'\\1'tll the free ends ol the vanes and the url'aee 1/ hetome imperl'eet through wear. by loosening the nuts 41" the tongue l) ma v he miusted towards the renter of the disk to eolupensale for the wear.
lt will lH notlt'til lloln the tleslliplion. that the l'rietion is redueed t a minimum. the onl l'rietion against the periphery ol'the disk living that between the free ends of the tongue and the sin-fare (1 The improved engine is esperiallv adapted for use as an explosive engine. that is, with mot ive fluids whose expansion is of short duration.
.\n v .suitahle meehanism may he lnade use of for su ur-l vingthe motive fluid at predetermined intervals, hni sinee surlt meehanism forms no part of my present invention, 1 have not thoughtit neeessary to further deserihe the samev l elaim l. rotary engine eomprising a disk supported fora rotary movement and provided at eaeh side of its )tll|)llt*|' with annular radial flanges, and with radial vanes or wings arranged transversely and extending hetween the flanges, said vanes being of lesser height than the flanges, an inlet pi )t for the spend with the path of travel of the free ends Should the eoutaet.
spond with the v dial flanges, and
of the vanes and provided with receiving the flanges, said inlet provided with a flange at its free end. said flange having spaeed slots, a tongue for defleet-ing the motive fluid against the vanes, Said tongue having a flange abutting against the flange of the inlet pipe and provided with openings registering with the slots, bolts traversing the openings and the slots for seeuring the tongue to the pipe, said tongue having grooves for reeeiving the flanges of the disk and having a portion at the free end thereof eurved ('oneentrieallv with the disk 5 and against whieh the ends of the vanes move. l
1 2. A rotary engine comprising a disk supported for rotary movement and provided at. 1 ea'eh side of its peripherv with annular radial flanges and with radia wings or vanes arranged transversely, the said ones being of lesser height than the flanges and extending between the flanges, an inlet pipe for the l motive lluid having one face curved to correpath of travel of the free ends of the vanes and provided with grooves for receiving the flanges and a tongue for de- 5 fleeting the motive lluid against the vanes and ('onneeted with the end of the inlet ripe and adjustable toward and from the d grooves for pipe being 1 i l l i l isk, said tongue having grooves for reeeiving the l flanges and having a portion at the free end 1 thereof eurved t'oneentrie with the disk and l against which the free ends of the vanes or wings move.
A" rotary engine eomprising a disk sup- I ported for rotary movement. and provided at I eaeh side of its periphery with annular rawith radial wings arranged transvrselv and extending between the said ones being of lesser height than the'flanges, an inlet pipe for the motive fluid 5 having one faee eurved to eorrespond with the path of travel of the free ends of th vanes, and provided with grooves i'or receiving the flanges, and a tongue eonneeted with the pipe fordefleetingtho motive lluid against the vanes, said tongue being adjustable toward and from the disk and being provided with grooves for reeeiving the flanges.
4. A rotary engine eomprising a disk supported for rotary movement and provided 1 with the pipe with radiai wings, or vanes, arranged trans versely of the periphery thereof, an inlet pipe for the motive fluid having one face curved to correspond with the path of travel of the free ends of the vanes, a tongue connected with the inlet pipe for deflecting the motive fluid against the vanes, said tongue having a portion at the free. end thereof curved coneentrie with the disk and a ainst which the ends of the hlades move, am means whereby to adjust said tongue toward and from the disk.
5. A rotary engine eomprising a disk supported for rotary moven-ientand provided with radial vanes or wings, an inlet pipe for he motive fluid having one of its faces arranged adjaeent tothe path of travel of the free ends of the vanes, a tongue connected with the pipe for defleeting'the motive fluid against the vanes. said tongue hein" adjustahle toward and from the disk and aavin' a portion at the free end thereof against which the ends of the vanes move.
6. A rotary engine eomprising a disk supported for rotary movement and provided with radial wings or vanes, an inletpipe for the motive fluid, and having one of its faces arranged adjacent to the path of travel of the tree ends-of the vanes, a tongue adjustably eonneetedwith -the ipe for deflecting the motive fluid against t he wings or vanes, said tongue having a portion at the free end thereof against which the ends of the vanes move.
- 7. A rotary engine, eomprising a disk supported for rotary movement and provided on its periphery with radial vanes and with radial annular flanges of greater length than the vanes,'het.veen \Ylllt'll the vanes extend, an inlet pipe having one of its fares arrzmged adjat'ent to the free end of the vanes and between the flanges. and a tongue eonneeted for deflertin the motive fluid against. the vanes, the, free end of said tongue having a. portion bet-ween the flanges curved eoneentrie with the disk and against which the free ends of the vanes move.
US37542407A 1907-05-24 1907-05-24 Rotary engine. Expired - Lifetime US875515A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3169746A (en) * 1959-09-11 1965-02-16 Moosmann Alois Fluid pressure operated turbines
US4927081A (en) * 1988-09-23 1990-05-22 Graco Inc. Rotary atomizer

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3169746A (en) * 1959-09-11 1965-02-16 Moosmann Alois Fluid pressure operated turbines
US4927081A (en) * 1988-09-23 1990-05-22 Graco Inc. Rotary atomizer

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