US840771A - Steam turbine-engine. - Google Patents

Steam turbine-engine. Download PDF

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US840771A
US840771A US31654706A US1906316547A US840771A US 840771 A US840771 A US 840771A US 31654706 A US31654706 A US 31654706A US 1906316547 A US1906316547 A US 1906316547A US 840771 A US840771 A US 840771A
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ports
steam
bearing
engine
cylindrical
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Amariah W Jackson
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/022Multi-stage pumps with concentric rows of vanes

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  • My invention relates to that class of engines known as steam-turbines.
  • the object of my invention is to produce a simple and cheaply-constructed engine in which by the fullest application of the principle of deflection to secure the largest percentage of the initial and expansive force of the steam entering the engine and convert it into motion ;A that While constructed of but two parts will be automatic in action.
  • FIG. 1 is a central vertical section on the line 1 1, Fig. 9.
  • y Fig. 2 is a central vertical section on line 1 1, Fig. 9, showing the construction of the main supporting fixed half of the engine.
  • Fig. 3 is a vertical sectional view on the line 1 1, Fig. 9, showing the construction of the supportedrotatableart of the engine.
  • Fig. 4 is a vertical centraIcrosssectional view on the line 6 6, Fig. 8, showing the construction of the main supporting fixed half of engine.
  • Fig. 5 is a vertical central cross-sectional view on the line 6 6, Fig. 8, showing the construction of the supported rotatable half of the engine.
  • Fig. 6 is a central vertical cross-sectional view on the line 6 6, Fig. 8, showingboth halves of the engine in the operating position.
  • Fig. 9 is a front view of the engine.
  • A indicates the main stationary half of the engine, cylindrical ⁇ in form, rovided with a base A.
  • One side A2 of t is forms an integral part of this half i and has a central aperture A3, into which a steam-supply pipe A4 is attached. This aperture opens into a steam-chamber A5.
  • Extending through the wall of this chamber is a series of steam-ports B. The direction of these ports is tangential to the axis of the chamber and engine.
  • the external face A of the wall of this steam-chambery forms a central finished circular tapered bearing A7.
  • Fig. 7'lis agthese ports is in the same tangential'direcsteam-ports B, corresponding in number.
  • ports B in the bearing A7 are V-shaped, the apex of the angle of each port being on an imaginary concentric circle through the longitudinal center of the bearingAS.
  • the tangential direction of the inner half B2 ofthe ports B in the. bearing A8 is opposite to the tangential direction of the ports B in the bearing A7, the tangential direction of the outer half B3 of the ports B2 being the same as that of the portsB.
  • Spaced from the bearing A8 is the outercylindrical part A9 ⁇ of they stationary half A.
  • Extending through this cylindrical part is a series of steam-ports B4, the same in number, shape, and direction as the ports in the bearing A8.
  • These ports open into anI exhaust-chamber B5, which encircles this series of ports and permits the steam therefrom to escape through an exhaust-pipe B".
  • At the bottom of the V-shaped spaces C are' annular channels C.
  • the rotatable half D ⁇ of the engine is adapted to fit the concentric bearingsin the stag y* tionary half A.
  • the central part forms a taper cylinder D', adapted to fit on the bearing A7.
  • the wall D2 of this cylinder is taered externally to fit the inside face of the caring A8. Extending through this Wall is a series of steam-ports E,corresponding in number with the ports B in the bearing A7,.
  • This ring is tapered and adapted to fit in the annular space C formed, 'by the bearing A8 and bearing-surface A10' of IIO the outer cylindrical part AD of the main part A. Extending through this ring is a series of ports E4, corresponding in number with and 'in the same angular shape and direction as ports E in the part D2. These ports are adapted to register with the ports B and B3 in the bearings A8 and A9. At the bottom of the spaces F are channels F. The channels C and F at the bottom of the spaces C and F are adapted to allow a clearance for the ends of the bearing-surfaces, and thereby prevent the wearing of shoulders therein.
  • a steam-supply is turned into the chamber A5 through the supply-pipe A4.
  • the steam passes from this chamber through the ports B and is deflected so that it strikes the inner half E2 of the ports E in the rotatable part D of the engine and is again deflected by the outer half Esof the ports E and then enters the ports B in the part A.
  • the action of the steam against the angular faces of the ports E forces the part D to rotate in the direction of the arrows.
  • the steam is deflected again in the ports B in the direction of the rotation of the part D.
  • the steam then enters the ports E4L in the part D, im-
  • the rotary movement of the part D can be transmitted from the shaft G or by other means affixed or attached to any part of the outer surface of the part D.
  • the stationary body may be made of a back plate and supportingbase and that the steam-chamber and concentric cylindrical bearings can be finished in separate parts and attached to said back plate, and so with the rotatable part.
  • the main body forming the back of that part can be prepared and finished and the concentric cylinders attached thereto.
  • the engine can also be adapted so that the number of ports may vary in both the stationary and rotatable parts and the steam be admitted through the periphery of the engine and exhaust throughout its central part, and any fluid under pressure can be used as the propelling or impelling force.
  • a turbine-engine formed of two members, one of said members being stationary and adapted to stand or be aflixed in a permanent position, said member having a central inlet for admission of steam, a steamchamber forming an extension of said inlet, the walls of said chamber forming an external central cylindrical taper bearing, a series of tangential steam-ports extending through the taper Wall of said chamber and bearing; a taper cylindrical external and internal bearing concentric with said central bearing and spaced therefrom; a series of tangential V-shaped steam-ports extending through said bearing; an internal taper cylindrical bearing, concentric with said external and internal bearing and spaced therefrom; a series of V-shaped tangential steam-ports extending through saicl bearing; an exhaustchamber encircling said ports 1n said internal bearing, said ports opening into said exhaust-chamber, said exhaust-chamber having an oulet through the exterior wall of said member; a rotatable member of said engine, said member having a central external and internal cylindrical taper bearing adapted
  • rotatable member having an internal axial bearing adapted to fit said axial bearing on said stationary member; a plurality of taper cylindrical bearin s adapted to iit and to be rotatable on sai cylindrical bearings on said stationary member radial tangential ports extending through said axial and said cylindrical bearings adapted to register With said ports in said stationary member.
  • a turbine-engine of the kind described comprising a supporting member, having a base and central aperture for a steamnlet; a cylindrical steam-chamber aflixed to said supporting member, said chamber being pierced With a series of tangential steam-ports, and inished externally as a central cylindrical bearing; a cylindrical ring aiiixed to said supporting member concentric Withsaid central bearing, said ring being pierced With a series .of tangential V-sha ed steam-ports; a cylindrical ring afhxe on said supporting member, concentric With the inner rin and central bearing, said ring being finis ed internally and pierced With a series of tangential V-shaped steam-ports, said ⁇ ports opening into an exhaust-chamber forming the bodyl bearings attached to said supporting mem-A ber, and adapted to be rotated in and on said bearings said steam-ports in said rings being adapted to register With each other

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Description

No. 840,771. lATENT-BD JAN. s, 1907.
A A. W. JACKSON,
' STEAM TURBINE ENGINE.
APPL IIIIIIIIIIIII AY 12, 1906,
maf/f xga-575655@ Y new# x d mma/U/fwswp v A 133 my? No. 840,771. PATENTED JAN. 8, 1907.
` A. W. JACKSON.
STEAM TURBINE ENGINE.
APPLIOATION FILED MAY 12. 190e.
2 SHEETS-SHEBT 2.
AMARIAH W. JACKSON, CF CHICAGO, ILLINOIS.v
STEAM TURBINE-ENGINE.
Specication of Letters Patent.
' Patented Jan. 8, 1907.
Application filed May 12, 1906. Serial No. 316,547.
To all whom t nfl/wy concern: l
Be it known that I, AMARIAH W. JACKSON, a citizen of the United States, residing at 315 East Sixty-third street, in the city of Chicago, county of Cook, and State of Illinois, have invented a new and useful Improvement in Steam Turbine-Engines, of which the following is a specification.
My invention relates to that class of engines known as steam-turbines.
The object of my invention is to produce a simple and cheaply-constructed engine in which by the fullest application of the principle of deflection to secure the largest percentage of the initial and expansive force of the steam entering the engine and convert it into motion ;A that While constructed of but two parts will be automatic in action.
The manner in which I accomplish my object is set forth in the following specification and illustrated in the accompanying drawings, in which-- Figure 1 is a central vertical section on the line 1 1, Fig. 9. y Fig. 2 is a central vertical section on line 1 1, Fig. 9, showing the construction of the main supporting fixed half of the engine. Fig. 3 is a vertical sectional view on the line 1 1, Fig. 9, showing the construction of the supportedrotatableart of the engine. Fig. 4 is a vertical centraIcrosssectional view on the line 6 6, Fig. 8, showing the construction of the main supporting fixed half of engine. Fig. 5 is a vertical central cross-sectional view on the line 6 6, Fig. 8, showing the construction of the supported rotatable half of the engine. Fig. 6 is a central vertical cross-sectional view on the line 6 6, Fig. 8, showingboth halves of the engine in the operating position.
etail sec-tional view of one of the steamorts, showing the corrugated faces therein. ig. 8 is a sideview of the engine, and Fig. 9 is a front view of the engine.
` In the drawings, A indicates the main stationary half of the engine, cylindrical `in form, rovided with a base A. One side A2 of t is forms an integral part of this half i and has a central aperture A3, into which a steam-supply pipe A4 is attached. This aperture opens into a steam-chamber A5. Extending through the wall of this chamber is a series of steam-ports B. The direction of these ports is tangential to the axis of the chamber and engine. The external face A of the wall of this steam-chambery forms a central finished circular tapered bearing A7.
Fig. 7'lis agthese ports is in the same tangential'direcsteam-ports B, corresponding in number.
with ports B in the bearing A7. These ports in cross-section are V-shaped, the apex of the angle of each port being on an imaginary concentric circle through the longitudinal center of the bearingAS. i
The tangential direction of the inner half B2 ofthe ports B in the. bearing A8 is opposite to the tangential direction of the ports B in the bearing A7, the tangential direction of the outer half B3 of the ports B2 being the same as that of the portsB. Spaced from the bearing A8 is the outercylindrical part A9 `of they stationary half A. The interior periphery A10 of this partis finished to a taper bearingsurface. Extending through this cylindrical part is a series of steam-ports B4, the same in number, shape, and direction as the ports in the bearing A8. These ports open into anI exhaust-chamber B5, which encircles this series of ports and permits the steam therefrom to escape through an exhaust-pipe B". At the bottom of the V-shaped spaces C are' annular channels C.
` The rotatable half D `of the engine is adapted to fit the concentric bearingsin the stag y* tionary half A. The central part forms a taper cylinder D', adapted to fit on the bearing A7. The wall D2 of this cylinder is taered externally to fit the inside face of the caring A8. Extending through this Wall is a series of steam-ports E,corresponding in number with the ports B in the bearing A7,.
In cross-section these ports are V-shaped,
the apex E of the angle being on an imaginery concentric circle through the longitudiy nal center of the wall D2 of the cylinderl D.v The direction of the inner half E2 of eachof tion as that of the ports B in the bearing A7, the outer half E3 of each port extending at an angle thereto in the opposite direction. The inner openings E2v of` these ports correspond in size and register with the ports Bin the bearing A7, and the outer openings vE3 registerwith the inner openings B of the bearing A8. Spaced from and concentric with the wall D2 of the cylinder D and forming an integral part of the half D is a cylindrical ring D3. This ring is tapered and adapted to fit in the annular space C formed, 'by the bearing A8 and bearing-surface A10' of IIO the outer cylindrical part AD of the main part A. Extending through this ring is a series of ports E4, corresponding in number with and 'in the same angular shape and direction as ports E in the part D2. These ports are adapted to register with the ports B and B3 in the bearings A8 and A9. At the bottom of the spaces F are channels F. The channels C and F at the bottom of the spaces C and F are adapted to allow a clearance for the ends of the bearing-surfaces, and thereby prevent the wearing of shoulders therein.
When the two halves of the engine are constructed and finished as described and shown and the part D is placed into the part A and adjusted therein by any suitable means adapted to hold the parts in adjustment, the operation of the engine is as follows: A steam-supply is turned into the chamber A5 through the supply-pipe A4. The steam passes from this chamber through the ports B and is deflected so that it strikes the inner half E2 of the ports E in the rotatable part D of the engine and is again deflected by the outer half Esof the ports E and then enters the ports B in the part A. The action of the steam against the angular faces of the ports E forces the part D to rotate in the direction of the arrows. The steam is deflected again in the ports B in the direction of the rotation of the part D. The steam then enters the ports E4L in the part D, im-
'pelling the part D in its rotary motion, and
escapes through the ports Blinto the exhaustchambers B5, from whence it passes out of the engine through the exhaust-pipe B". The rotary movement of the part D can be transmitted from the shaft G or by other means affixed or attached to any part of the outer surface of the part D.
Itis obvious that when the steam is turned into the engine if the ports E in the cylindrical part D2 do not register with the ports B of the steam-chamber A5 a slight rotary movement of the part D will bring the ports into line and the engine will rotate at once. It is also apparent that the number of concentric cylindrical bearing-surfaces and series of ports in the fixed and rotatable parts of the engine can be increased 'with the size of the engine and the engine be thereby adapted to utilize the full expansive force of the steam as it passes through the ports from the center to the circumference. For the purpose of retarding the passage of the steam through the ports of the rotating part of the engine and to thereby increase its propelling force l construct the forward wall of each of said ports 'with corrugations H, as shown in the fractional detail sectional view in Fig. 7. It is also obvious that the stationary body may be made of a back plate and supportingbase and that the steam-chamber and concentric cylindrical bearings can be finished in separate parts and attached to said back plate, and so with the rotatable part. The main body forming the back of that part can be prepared and finished and the concentric cylinders attached thereto.
The engine can also be adapted so that the number of ports may vary in both the stationary and rotatable parts and the steam be admitted through the periphery of the engine and exhaust throughout its central part, and any fluid under pressure can be used as the propelling or impelling force.
Vhat l claim, and desire to secure by Letters Patent, is
1. A turbine-engine formed of two members, one of said members being stationary and adapted to stand or be aflixed in a permanent position, said member having a central inlet for admission of steam, a steamchamber forming an extension of said inlet, the walls of said chamber forming an external central cylindrical taper bearing, a series of tangential steam-ports extending through the taper Wall of said chamber and bearing; a taper cylindrical external and internal bearing concentric with said central bearing and spaced therefrom; a series of tangential V-shaped steam-ports extending through said bearing; an internal taper cylindrical bearing, concentric with said external and internal bearing and spaced therefrom; a series of V-shaped tangential steam-ports extending through saicl bearing; an exhaustchamber encircling said ports 1n said internal bearing, said ports opening into said exhaust-chamber, said exhaust-chamber having an oulet through the exterior wall of said member; a rotatable member of said engine, said member having a central external and internal cylindrical taper bearing adapted to lit the corresponding central external bearings in said stationary member, a series of V-shaped tangential steam-ports extending through the wall of said cylinder, said ports corresponding in number and adapted to register with the ports in said corresponding external central bearing in said stationary member; a taper cylindrical external and internal bearing concentric with said central external and internal bearing and spaced therefrom, said bearing being adapted to fit the corresponding internal and external bearings in the stationary member, a series of V-shaped steam-ports, corresponding in number and adapted to register with the ports in said bearings in said stationary part, and means for holding and adjusting said rotatable member in the stationary member substantially as and for the purposes specified.
2. In a turbine-engine of the kind described, the combination of a stationary member, having a central steam inlet and chamber, the external wall of said chamber forming a central external cylindrical bearing, piercedwith a series of tangential steam- ICO IIO
ports, and concentric internal and external cylindrical bearing spaced from said central bearing pierced With aseries of V-shaped tangential steam-ports, and an internal concentric bearing spaced from said external and internal concentric bearing, ierced With a series of V-shaped tangentia ports, and an exhaust-steam chamber encircling said internal concentric bearing and connected with and forming an exhaust-outlet for the said steam-ports; with a rotatable member having taper concentric cylindrical bearings, corresponding With and adapted to ht the bearings in said stationary member, said bearings in said rotatable member being pierced with V-shaped tangential steam-ports, corresponding in number and adapted to register with thesteam-ports in the bearings in said stationary parts; and means for adjustin and holding said rotatable member in sai stationary member.
3. -In a turbine-engine' of the kind described, the combination ofl a stationary member having an external axial taper bearing an axial steam-inlet and chamber Within l said bearing; radial tanglential ports extending from said chamber t rough said bearing; a plurality of taper cylindrical bearings concentric With said axial bearing and spaced therefrom and from each other; radial tangential ports extending through each of said bearings; an exhaust chamber and outlet, said chamber being concentric With said cylindrical bearings; radial tangential ports extending through the outer cylindrical bearinfr into said exhaust-chamber, With a. rotatable member having an internal axial bearing adapted to fit said axial bearing on said stationary member; a plurality of taper cylindrical bearin s adapted to iit and to be rotatable on sai cylindrical bearings on said stationary member radial tangential ports extending through said axial and said cylindrical bearings adapted to register With said ports in said stationary member.
4. In a turbine-engine of the kind described, the combination comprising a supporting member, having a base and central aperture for a steamnlet; a cylindrical steam-chamber aflixed to said supporting member, said chamber being pierced With a series of tangential steam-ports, and inished externally as a central cylindrical bearing; a cylindrical ring aiiixed to said supporting member concentric Withsaid central bearing, said ring being pierced With a series .of tangential V-sha ed steam-ports; a cylindrical ring afhxe on said supporting member, concentric With the inner rin and central bearing, said ring being finis ed internally and pierced With a series of tangential V-shaped steam-ports, said` ports opening into an exhaust-chamber forming the bodyl bearings attached to said supporting mem-A ber, and adapted to be rotated in and on said bearings said steam-ports in said rings being adapted to register With each other and to 'permit the passage of steam therethrough,
and means for adjusting and holdin said members and their bearing parts to et er.
5. In a turbine-engine of the ind described, the combination of one stationary f member With one movable member, said stationary member having an external axial bearing; a central steam-inlet in said bearing radial tangential ports from said inlet through said bearing; cylindrical bearings concentric With said axial bearing, s aced therefrom and from each other; radia tan-l gential ports extending through said bearings, and an exhaust-port concentric With said bearings, radial ports connecting said exhaust-port With said bearings; said movable member having an internal axial bearing and cylindrical concentric bearings adapted to it said bearings on said stationary member and to be revolved thereon; radial tangential ports extending through said axial and cylindrical bearings adapted to register With said ports in said stationary member.
6. In a steam-engine ofthe kind described, the combination of a stationary part consisting of series of concentric cylindrical bearings, pierced by a series of tangential steamports,A the advance face of each of said ports eing corrugated across the line of passage of the steam, and a rotative part consisting of a series of concentric cylindrical bearings pierced by a series of tangential steam-ports, said ports having corru ated faces, said corrgations being across t e line of the passage of the steam, the cylindrical parts of said stationary and said rotatable parts of said engine being adapted to iit each other and the steam-ports to register and permit the passage of steam from the center of said stationary part through all of said stationary and rotative cylinders.
AM ARIAH vv, JACKSON.
Witnesses JOSEPH STAAB, THoMAs J. MoimfAN.`
IOO
ITO
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4466245A (en) * 1983-06-02 1984-08-21 Arold Frank G Power plant having a fluid powered flywheel
US20110020132A1 (en) * 2009-06-25 2011-01-27 Rajendra Kumar Bhogilal Patel DECOMPRESSION MACHINE (SUDARSHAN CHAKRA) SU [good], DARHAN [looking;appearance] CHAKRA [wheel]
US20170314576A1 (en) * 2014-11-10 2017-11-02 Siemens Aktiengesellschaft Method for creating an impeller of a radial turbo fluid energy machine, and stage

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4466245A (en) * 1983-06-02 1984-08-21 Arold Frank G Power plant having a fluid powered flywheel
US20110020132A1 (en) * 2009-06-25 2011-01-27 Rajendra Kumar Bhogilal Patel DECOMPRESSION MACHINE (SUDARSHAN CHAKRA) SU [good], DARHAN [looking;appearance] CHAKRA [wheel]
US20170314576A1 (en) * 2014-11-10 2017-11-02 Siemens Aktiengesellschaft Method for creating an impeller of a radial turbo fluid energy machine, and stage

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