US2768808A - Turbines - Google Patents

Turbines Download PDF

Info

Publication number
US2768808A
US2768808A US275693A US27569352A US2768808A US 2768808 A US2768808 A US 2768808A US 275693 A US275693 A US 275693A US 27569352 A US27569352 A US 27569352A US 2768808 A US2768808 A US 2768808A
Authority
US
United States
Prior art keywords
rotor
casing
intake
ducts
steam
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
US275693A
Inventor
Worre Tony Eden
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US275693A priority Critical patent/US2768808A/en
Application granted granted Critical
Publication of US2768808A publication Critical patent/US2768808A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines

Definitions

  • a turbine of this character which comprises a single compact casing and a single rotor mounted within the casing and wherein the rotor is provided with nozzles working against fixed buckets formed in the casing and also wherein the power of the steam is utilized throughout its entire travel from the inlet to the exhaust of the turbine.
  • Figure 1 is a sectional side elevation of a turbine made in accordance with my invention, and taken along the line 1-1 of Figure 2.
  • Figure 2 is an axial sectional view taken approximately along the line 2-2 of Figure 1.
  • FIG. 3 is a fragmentary sectional detail plan View of a modified arrangement of buckets Referring now more particularly to the drawing:
  • the invention comprises a circular main body member in the form of a casing made up of two identical sections indicated at 1 and 2, and secured together with bolts as at 2A with a suitable gasket between the sections.
  • the sections are enlarged and bored at their centers to provide aligned bearings 3 and 4 for a hollow shaft 5 cast integral with or secured to a rotor 6 adapted to be located in the interior of the casing.
  • annular recesses 7 and 8 which, when the casing sections are bolted together, form a channel which embraces by a working fit an annular sealing flange 9 cast integral with the rotor.
  • the annular marginal portion of the casing is formed with a plurality of fixed spaced-apart buckets each in the form of a U-shaped duct 10 whose open ends are spaced-apart equal to the spacing between the open ends of intake and outlet ducts 11 and'12, respectively, formed in the rotor 6 and curved outwardly as shown toward the periphery of the rotor in the direction opposite to the direction of rotation of the rotor.
  • the U-shaped ducts and the intake and outlet ducts are of uniform inside diameter.
  • the tubes 11 serves as nozzles for directing the steam in the direction indicated by the arrows applied to the tubes into one leg or one end of a bucket while the tubes 12 serve as an exhaust for the steam after it has passed through the bucket.
  • a rotary engine comprising in combination a casing made of two identical disc-shaped sections secured together at abutting annular surfaces at their periperies to form a chamber centrally of the casing, axially and radially extending mating annular recesses formed on the abutting surfaces of said sections to form a circumferential channel opening into said chamber, U-shaped circumferentially spaced apart axially extending ducts formed in said abutting surfaces of the casing astraddle said channel and open at both ends into said chamber, a hollow intake shaft extending into one side of said casing, a hollow outlet shaft extending outwardly from the other side of the casing, said intake shaft being of lesser inside diameter than the inside diameter of said outlet shaft, a rotor secured to said shafts, a circumferential sealing flange formed about the periphery of said rotor and operatively disposed within said circumferential channel to seal off the interior of said chamber on one side of the rotor from the interior of the chamber on the opposite side of

Description

\ JNVENTOR.
TDA/Y E- wpa/QE T. E. WORRE TURBINES Filed March l0, 1952 @i V f////,
Oct. 30, 1956 United States Patent TURBINES Tony Eden Worte, Estacada, Oreg.
Application March 10, 1952, Serial No. 275,693
1 Claim. (Cl. 253-89) This invention relates to improvements in steam turbines. n
It is one of the principal objects of the invention to provide a turbine of this character which comprises a single compact casing and a single rotor mounted within the casing and wherein the rotor is provided with nozzles working against fixed buckets formed in the casing and also wherein the power of the steam is utilized throughout its entire travel from the inlet to the exhaust of the turbine.
These and other objects will appear as my invention is more fully hereinafter described in the following specification, illustrated in the accompanying drawing, and finally pointed out in the appended claim.
In the drawing:
Figure 1 is a sectional side elevation of a turbine made in accordance with my invention, and taken along the line 1-1 of Figure 2.
Figure 2 is an axial sectional view taken approximately along the line 2-2 of Figure 1.
Figure 3 is a fragmentary sectional detail plan View of a modified arrangement of buckets Referring now more particularly to the drawing:
The invention comprises a circular main body member in the form of a casing made up of two identical sections indicated at 1 and 2, and secured together with bolts as at 2A with a suitable gasket between the sections. The sections are enlarged and bored at their centers to provide aligned bearings 3 and 4 for a hollow shaft 5 cast integral with or secured to a rotor 6 adapted to be located in the interior of the casing.
The inner edges of the abutting surfaces of the casing sections 1 and 2 are formed with annular recesses 7 and 8 which, when the casing sections are bolted together, form a channel which embraces by a working fit an annular sealing flange 9 cast integral with the rotor.
The annular marginal portion of the casing is formed with a plurality of fixed spaced-apart buckets each in the form of a U-shaped duct 10 whose open ends are spaced-apart equal to the spacing between the open ends of intake and outlet ducts 11 and'12, respectively, formed in the rotor 6 and curved outwardly as shown toward the periphery of the rotor in the direction opposite to the direction of rotation of the rotor. The U-shaped ducts and the intake and outlet ducts are of uniform inside diameter. In operation, the tubes 11 serves as nozzles for directing the steam in the direction indicated by the arrows applied to the tubes into one leg or one end of a bucket while the tubes 12 serve as an exhaust for the steam after it has passed through the bucket.
With particular reference to Figure 2, it will be noted that the interior of the hollow shaft 5 on the intake side is of lesser diameter than the outlet side thereof and that steam passes through the turbine from the left to the right hand side as viewed in Figure 2.
As steam enters the tubes 11 from the intake side of lCC the shaft it will impart rotation to the rotor in the direction of the arrow applied thereto in Figure 1 because of the resistance of the curved tubes against the steam pressure which, as is well known, will travel in a straight line when not restricted.
When the steam leaves the nozzle end of each tube and impinges upon each bucket an additional power thrust is obtained. Then as the steam leaves the bucket and enters the curved outlet tube 12 further pressure is applied to the rotor in the same direction as that applied by the steam in the intake tubes.
For clearness of illustration I have shown in Figure l a number of buckets equal to the number of nozzles and outlet tubes, but it is to be understood that a greater number of buckets may be formed in the casing as illustrated in Figure 3 in order to obtain maximum efficiency.
While I have shown particular forms of embodiment of my invention I am aware that many minor changes therein will readily suggest themselves to others skilled in the art without departing from the spirit and scope of the invention. Having thus described the invention, what I claim as new and desire to protect by Letters Patent is:
A rotary engine comprising in combination a casing made of two identical disc-shaped sections secured together at abutting annular surfaces at their periperies to form a chamber centrally of the casing, axially and radially extending mating annular recesses formed on the abutting surfaces of said sections to form a circumferential channel opening into said chamber, U-shaped circumferentially spaced apart axially extending ducts formed in said abutting surfaces of the casing astraddle said channel and open at both ends into said chamber, a hollow intake shaft extending into one side of said casing, a hollow outlet shaft extending outwardly from the other side of the casing, said intake shaft being of lesser inside diameter than the inside diameter of said outlet shaft, a rotor secured to said shafts, a circumferential sealing flange formed about the periphery of said rotor and operatively disposed within said circumferential channel to seal off the interior of said chamber on one side of the rotor from the interior of the chamber on the opposite side of the rotor, a plurality of curved and substantially radially extending intake ducts formed in said rotor and in open communication at their inner ends with the interior of said hollow intake shaft, the opposite ends of said intake ducts being adapted for intermittent and progressive communication with one end of each of said U-shaped ducts, a plurality of curved and substantially radially extending outlet ducts formed in said rotor and in open communication at their inner ends with the interior of said hollow outlet shaft, the outer ends of said outlet ducts being adapted for intermittent and progressive communication with the opposite end of each of said U-shaped ducts, the spacing between the terminal ends of said U-shaped ducts being equal to the spacing between the outer terminal ends of said intake and outlet ducts, all of said ducts being of uniform inside diameter and all of said intake and outlet ducts being curved away from the direction of rotation of said rotor.
References Cited in the file of this patent UNITED STATES PATENTS 715,152 Roeske Dec. 2, 1902 727,698 Schenck May 12, 1903 745,409 Zahikjanz Dec. 1, 1903 FOREIGN PATENTS 6,196 Great Britain 1902 375,304 France May 10, 1907
US275693A 1952-03-10 1952-03-10 Turbines Expired - Lifetime US2768808A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US275693A US2768808A (en) 1952-03-10 1952-03-10 Turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US275693A US2768808A (en) 1952-03-10 1952-03-10 Turbines

Publications (1)

Publication Number Publication Date
US2768808A true US2768808A (en) 1956-10-30

Family

ID=23053419

Family Applications (1)

Application Number Title Priority Date Filing Date
US275693A Expired - Lifetime US2768808A (en) 1952-03-10 1952-03-10 Turbines

Country Status (1)

Country Link
US (1) US2768808A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2944785A (en) * 1955-05-18 1960-07-12 Thompson Ramo Wooldridge Inc Impeller for turbine engine and the like
US3690784A (en) * 1970-10-14 1972-09-12 Desmond J Farrow Turbine
US3804549A (en) * 1972-07-17 1974-04-16 Spector G Internally propelled flywheel engine
US3854841A (en) * 1973-10-09 1974-12-17 M Eskeli Turbine
US3915589A (en) * 1974-03-29 1975-10-28 Gast Manufacturing Corp Convertible series/parallel regenerative blower
US4068975A (en) * 1975-04-17 1978-01-17 Michael Eskeli Fluid pressurizer
US20060257242A1 (en) * 2003-03-28 2006-11-16 Aegerter Karl M Gas-jet driven rotary device for generating a field and a process for treating items within the field for increased performance
WO2007104973A2 (en) * 2006-03-14 2007-09-20 Goodman, Simon, John, Nye Rotor and nozzle assembly for a radial turbine and method of operation
WO2013177706A1 (en) * 2012-05-28 2013-12-05 Worldiscoveries Mechanism for enhanced energy extraction and cooling pressurized gas
EP3315716A1 (en) * 2016-07-22 2018-05-02 Brent Wei-Teh Lee Rotary device and method of using the same
US10495353B2 (en) 2012-05-28 2019-12-03 The University Of Western Ontario Mechanism for enhanced energy extraction and cooling of pressurized gas at low flow rates

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB190206196A (en) * 1902-03-13 1902-06-05 Johann Wennemar Scherrer An Improved Rotary Motor or Pump
US715152A (en) * 1902-03-13 1902-12-02 Henry Roeske Rotary steam-motor.
US727698A (en) * 1900-09-18 1903-05-12 Alexander Schenck Turbine.
US745409A (en) * 1902-12-24 1903-12-01 Bergmann Elektricitaet Ag Turbine.
FR375304A (en) * 1907-03-02 1907-07-05 Paul Ostertag Compound turbine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US727698A (en) * 1900-09-18 1903-05-12 Alexander Schenck Turbine.
GB190206196A (en) * 1902-03-13 1902-06-05 Johann Wennemar Scherrer An Improved Rotary Motor or Pump
US715152A (en) * 1902-03-13 1902-12-02 Henry Roeske Rotary steam-motor.
US745409A (en) * 1902-12-24 1903-12-01 Bergmann Elektricitaet Ag Turbine.
FR375304A (en) * 1907-03-02 1907-07-05 Paul Ostertag Compound turbine

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2944785A (en) * 1955-05-18 1960-07-12 Thompson Ramo Wooldridge Inc Impeller for turbine engine and the like
US3690784A (en) * 1970-10-14 1972-09-12 Desmond J Farrow Turbine
US3804549A (en) * 1972-07-17 1974-04-16 Spector G Internally propelled flywheel engine
US3854841A (en) * 1973-10-09 1974-12-17 M Eskeli Turbine
US3915589A (en) * 1974-03-29 1975-10-28 Gast Manufacturing Corp Convertible series/parallel regenerative blower
US4068975A (en) * 1975-04-17 1978-01-17 Michael Eskeli Fluid pressurizer
US20060257242A1 (en) * 2003-03-28 2006-11-16 Aegerter Karl M Gas-jet driven rotary device for generating a field and a process for treating items within the field for increased performance
US20090220329A1 (en) * 2006-03-14 2009-09-03 Pickard John D Rotor and nozzle assembly for a radial turbine and method of operation
US8287229B2 (en) * 2006-03-14 2012-10-16 Cambridge Research And Development Limited Rotor and nozzle assembly for a radial turbine and method of operation
GB2450061A (en) * 2006-03-14 2008-12-10 John D Pickard Rotor and nozzle assembly for a radial turbine and method of operation
WO2007104973A2 (en) * 2006-03-14 2007-09-20 Goodman, Simon, John, Nye Rotor and nozzle assembly for a radial turbine and method of operation
GB2450061B (en) * 2006-03-14 2011-12-21 Cambridge Res And Dev Ltd Rotor for a Radial-Flow Turbine and Method of Driving a Rotor
US8162588B2 (en) 2006-03-14 2012-04-24 Cambridge Research And Development Limited Rotor and nozzle assembly for a radial turbine and method of operation
US20120223526A1 (en) * 2006-03-14 2012-09-06 Cambridge Research And Development Limited Rotor and nozzle assembly for a radial turbine and method of operation
WO2007104973A3 (en) * 2006-03-14 2008-01-03 Albonia Innovative Technologie Rotor and nozzle assembly for a radial turbine and method of operation
US8485775B2 (en) * 2006-03-14 2013-07-16 Cambridge Research And Development Limited Rotor and nozzle assembly for a radial turbine and method of operation
WO2013177706A1 (en) * 2012-05-28 2013-12-05 Worldiscoveries Mechanism for enhanced energy extraction and cooling pressurized gas
US10495353B2 (en) 2012-05-28 2019-12-03 The University Of Western Ontario Mechanism for enhanced energy extraction and cooling of pressurized gas at low flow rates
EP3315716A1 (en) * 2016-07-22 2018-05-02 Brent Wei-Teh Lee Rotary device and method of using the same
US10519858B2 (en) 2016-07-22 2019-12-31 Brent Wei-Teh LEE Engine, rotary device, power generator, power generation system, and methods of making and using the same
US20200123975A1 (en) * 2016-07-22 2020-04-23 Brent Wei-Teh LEE Engine, rotary device, power generator, power generation system, and methods of making and using the same

Similar Documents

Publication Publication Date Title
US2768808A (en) Turbines
US2577179A (en) Cooling device for radial gas turbines
GB1088360A (en) Improvements in gas turbine ducted fan engine sealing means
DE1601690B2 (en) DOUBLE SHELL TURBINE HOUSING
JP2002349287A5 (en)
GB695724A (en) Improvements in or relating to structural elements for axial-flow turbo-machines such as compressors or turbines of gas-turbine engines
KR980003340A (en) Variable pipe diffuser for centrifugal compressors
ES410317A1 (en) Centrifugal flow gas turbine engine with annular combustor
US2282894A (en) Elastic fluid turbine
GB712051A (en) Improvements in or relating to axial-flow fluid machines
US2440069A (en) High-temperature elastic fluid turbine
GB610113A (en) Improvements in or relating to gas-turbine engines
RU2003131958A (en) ENSURING SEALING AND LAMINAR FLOW CONFIGURATION OF FLOW TRAJECTORY IN A TUBE
CN103512046A (en) Transition duct for a gas turbine
GB904138A (en) Improvements in or relating to stator structures, for example for axial flow gas turbine engines
US3824030A (en) Diaphragm and labyrinth seal assembly for gas turbines
US3902314A (en) Gas turbine engine frame structure
US4003672A (en) Internal combustion engine having coaxially mounted compressor, combustion chamber, and turbine
GB1161186A (en) A Gas Turbine Ducted Fan Engine.
US3228190A (en) Gas turbine plant
US2972441A (en) Variable blade system
US2841362A (en) Multistage turbine
GB797445A (en) Improvements in or relating to rotary fluid machines, for example turbines and compressors
US2643085A (en) Gas turbine apparatus
GB787666A (en) Improvements in blades for gas turbine engines