US1777450A - Turbine - Google Patents

Turbine Download PDF

Info

Publication number
US1777450A
US1777450A US115105A US11510526A US1777450A US 1777450 A US1777450 A US 1777450A US 115105 A US115105 A US 115105A US 11510526 A US11510526 A US 11510526A US 1777450 A US1777450 A US 1777450A
Authority
US
United States
Prior art keywords
nozzles
casing
turbine
apertures
wheel
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
US115105A
Inventor
Rix Carl
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
Application granted granted Critical
Publication of US1777450A publication Critical patent/US1777450A/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
    • F01D1/02Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/026Impact turbines with buckets, i.e. impulse turbines, e.g. Pelton turbines

Definitions

  • This invention relates to a turbine for use with steam or water and consists essentially in the provision of a blade wheel having a rim which presents, when viewed in axial direction, alternate circular and substantially V-shaped recesses forming blades of corniform cross-section turned alternately in opposite directions.
  • This arrangement enables the wheel, which works with tangentially admitted fluid,to be rotated with equal effect in bothdirections; the pressure is taken up gradually by the blades, and the fluid is enabled to clear the blades readily after its energy has beenspent on the same.
  • the turbine is controlled by means of hollow cylindrical valves by the rotary adjustment of which a plurality of nozzles can be put in varying numbers into and out of operation.
  • Fig. 1 of the accompanying drawings represents a vertical section of the turbine
  • Fig. 2 a section on the line 2 2 of Fig. 1 and on an enlarged scale of the casing of a twin turbine
  • FIG. 3 a cross-section of one of the valves, Fig. 4, a side view of one of the control levers, y Fig. 5, a sectional side view of the blade wheel,
  • FIG. 6 an axial section of the wheel
  • Figs. 7 and 8 are sectional views at right angles of one of the nozzle arrangements.
  • FIGs. 9 and 10 similar views of another nozzle arrangement, i Fig. 11, a view of the first nozzlearrangement showing a modified structure,
  • Fig. 12 a cross-section of a valve cylinder of modified construction
  • the turbine has a U-shaped, double-walled casing 3 in the end walls of which the turbine shaft 2 is rotatably mounted.
  • the casing is divided horizontally on a level with the turbine shaft into two parts.
  • the upper, segmental part has at the top a segmental slot 59 through which minor repairs of the blade 115,105, and in Germany .Tune 15, 1925.
  • This slot is normally closed by a correspondingly shaped lid 4 which fits the slot and which is held in position by gravity without astenings.
  • the chambers formed between the double walls of the casing and of the lid 4 are utilized for the storage of oil and the like.
  • the casing is formed withtwo cylindrical chambers 6 and 7 4arranged parallel with the shaft, one in the upper and one in the lower part of the casing. These chambers contain and form a tight it with hollowT cylindrical valves 13 and 14 respectively which receive driving fluid through the medium of pipes 11 from a distributing pipelQ and delivers such iiuid through nozzles 10 tangentially to the blade wheel.
  • the latter consists of a wheelbody 1 on to which a blade rim 9a is forced.
  • This rim presents, when viewed axially as in Fig. v5, alternate circular and substantially V-shaped recesses forming between them blades 9 of corni-form cross-section turned alternately in opposite directions.
  • the V-shaped recesses are of the same depth as the circular ones, the distance between the tips of adjacent blades is substantially uniform and the convex sides of the blades aretherefore extensiveenough for reacting effectively with the driving fluid.
  • the rim 93L is divided axially intofive sections l1& 1e which are situated between flanges 8, the blades of alternate sections being in a staggered position.
  • the power outpt is normally controlled by means of the valves 13 and 14 which are adjusted rotatively for putting one or more nozzles into operation.
  • the nozzles for each valve are arranged in alignment, and the valve is formed' with feed apertures arranged in rows each of which supplies a different number of nozzles.
  • the valve 14 has three rows of apertures 17a, 17b and 17C each of Vwhich can be turned into register with the nozzles, one row supplying three, the next two, and the third only one nozzle. Segmental slots 16 in the valve cylinders remain in communication with the supply pipes 11 in all three adjustments.
  • the valve cylinders Diametrically opposite the feed apertures 17, the valve cylinders have apertures 19, and diametrically opposite the nozzes 10, the casing 3 has apertures 18. rlhese apertures, when in register, allow a tool to be inserted for cleaning theapertures themselves as well as the nozzles. Normally the apertures 18 in the casing are closed by plugs 20 so as to prevent escape of fluid.
  • the valve cylinders arelitted with shafts ⁇ 15 whereby the adjustment is made. All the control levers are at the same side of the turbine.
  • the near-side valve is adjusted by means of a lever 26 which is secured direct to the shaft 15.
  • the far-side valve is adjusted by means of a bell-crank 22, 23 loosely arranged on the near-side shaft and connected by a link 25 to a lever 24 which is rigidly secured to the far-side shaft.
  • Fig. 2 where two turbines are arranged in juxtaposition so as to act on the same driving shaft 2 ⁇ the control shafts 15 of the two turbines are in alignment and coupled by clutches 27 so that both turbines can be controlled by a single lever if desired.
  • nozzles and blade rim sections may be varied according to requirements, the valves being modified to correspond.
  • Figs. l2 and 13 show an arrangement of eleven nozzles.
  • the valve cylinder 14 is formed with lseven rows of feed apertures 10a-10g, the i'irst six of which increase their number of apertures progressively from one to six, apertures of adjacent rows being arranged in a staggered position.
  • the last row has eleven apertures and is put into operation when for some reason, for instance in the case of a sudden reversal of the turbine, full power is required.
  • the nozzles are ,preferably connected to a bushing 28 which allows of rotary adjustment within the valve chamber, the turbine casing being provided with a slot 22which .admits the nozzle and which is widened to allow its adjustment.
  • the casing is preferably recessed for the reception of anexchangeable guide fillet 23 the thickness of which is chosen according to the required depth of the passage. rlhis arrangement also allows an easy compensation for wear. Behind the fillet 23 which prevents the fluid from slipping off the convex sides of the blades too easily, the casing has a recess 24 through which the fluid can readily escape so as to clear the blades after its force has been spent on the latter.
  • a turbine comprising a casing, a blade wheel in said casing, rows of nozzles fitted at the inside of said casing for supplying driving fluid to the wheel and rotatable hollow valve cylinders fitted in the casing for feeding fluid to different rows of nozzles, each valve cylinder being provided with feeding apertures arranged in parallel rows all having different numbers of apertures, the number of apertures in one of the rows being equal to the number of nozzles.
  • a blade wheel having ak rim which presents, when viewed in an axial direction, alternate circular and substantially V-shaped recesses forming blades of corniform cross-section turned alternately in opposite directions, the V-shaped recesses being of the saine depth as the circular ones, a casing enclosing the blade wheel, rows of nozzles fitted at the inside of the casing for supplying driving fluid to the wheel, and a rotatable hollow valve cylinder tted in the casing for feeding fluid to each row of nozzles, each valve cylinder being provided with feeding apertures arranged in parallel rows, all hav ⁇ ing different numbers of apertures, two of said rows of apertures being longer than the others and of equal length but provided with different numbers of apertures, the number of apertures in one of said rows being equal to the number of nozzles.
  • a turbine comprising a blade wheel, a casing enclosing the blade wheel, rows of nozzles fitted at the inside of the casing for supplying driving fluid to the wheel, a rotatable hollow va ive cylinder fitted in the casing and provided with apertures for feeding fluid to a row of nozzles, casing and cylinder being also formed with cleaning apertures arranged diamet-rically opposite the nozzles and the feeding apertures respectively so as to admit a cleaning tool through the nozzles from the outside, and plugs whereby the cleaning apertures of the casing are normally closed.
  • a turbine comprising a blade wheel, a casing enclosing the blade wheel, nozzles fitted at theinside of said casing, for feeding driving fluid to the wheel, and rotatably adjustable bushings arranged parallelly with the turbine axis and holding the nozzles so that the position of the latter relative to the blades can be regulated by a rotary adjustment of said bushings.
  • a turbine comprising a blade wheel a casing enc-losing the blade wheel, nozzles ted at the inside of the casing for feeding driving fluid to the wheel, rotatably adjustable bushings arranged parallelly with the turbine axis and holding the nozzles so that the position of the latter relative to the blades can be regulated by a rotary adjustment of the bushings, and valves arranged in said bushings for controlling the fluid supply to the latter.
  • a turbine comprising a blade wheel a casing enclosing the blade wheel, nozzles ted at the inside of said casing for feeding driving fluid to the wheel, and exchangeable i fillets arranged in recesses in the casing so as to determine the depth of the passage between the blades and the casing immediately behind the nozzles.
  • a turbine comprising a blade wheel, a casing enclosing the blade wheel, said casing being formed at the top with al segmental slot giving access to the blade wheel, and a lid fitting said slot and normally held therein by gravity so as to maintain the slot closed, the lid being formed with an aperture through which the interior of the turbine can be observed.
  • a vblade wheel having a rim divided into a plurality of annular sections, each section presenting, when viewed in an axial direction7 alternate circular and substantially V-shaped recesses forming blades of corniform cross-section turned alternately in opposite directions, the circular recesses comprising each substantially twothirds of a circle, the V-shaped recesses being of the same depth as the circular ones, flanges separating the different sections, a wheel body to which said sections and flanges'are independently secured, alternate sections having their blades in a staggered position, a casing enclosing the blade wheel, and rows of nozzles, having a diameter of substantially one-tenth of the diameter of the circular recesses of the rim, fitted at the inside of the casing for supplying driving fluid to the wheel.
  • a blade wheel having a rim which, when viewed in an axial direction, presents alternate circular and substantially V-shaped recesses forming blades of corniform cross-section turned alternately in opposite directions, the V-shaped recesses being of the same depth as the circular ones, the distance between the tips of adjacent blades being substantially uniform, a casing enclosing the blade wheel and rows of nozzles, having a diameter of substantially one-tenth of the diameter of the circular recesses of the rim, fitted at the inside of the casing for supplying driving fluid to the wheel.
  • a blade wheel having a rim divided into a plurality of annular sections, flanges separating the different sections, rows of nozzles for supplying driving fluid to the wheel, rotatable hollow valve cylinders for feeding fluid to different rows of nozzles, each valve cylinder being provided with feeding apertures arranged in parallel rows all having different numbers of apertures, the apertures of adjacent rows being in a staggered relative position.
  • a blade wheel having a rim divided into a plurality of annular sections, llanges separating the different sections, rows of nozzles for supplying driving fluid to the wheel, rotatable hollow valve cylinders for feeding fluid to different rows of nozzles, each valve cylinder being provided with feeding apertures arranged in arallel rows all having different numbers o apertures, the apertures of adjacent rows being in a staggered relative position, one of said rows having as'many apertures as there are nozzles and being adjacent to a row having about half that number of apertures.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)

Description

C. RIX
TURBINE Oct. 7, 1930.
Filed June 10. 1926 3 Sheets-Sheet 2 The oct. 7, 1930. C. mx 1,777,450
TURBINE Filed June 1o. 192e s sheets-sheet :5
V//////// .//A Q Patented Oct. 7, 1930 CARL IRIX, OF EMDEN, EAST FRIESLAND, GERMANY PATENT or-Plc TURBINE Application filed .Tune 10, 1928, SerialV No.
This invention relates to a turbine for use with steam or water and consists essentially in the provision of a blade wheel having a rim which presents, when viewed in axial direction, alternate circular and substantially V-shaped recesses forming blades of corniform cross-section turned alternately in opposite directions. f
This arrangement enables the wheel, which works with tangentially admitted fluid,to be rotated with equal effect in bothdirections; the pressure is taken up gradually by the blades, and the fluid is enabled to clear the blades readily after its energy has beenspent on the same.
The turbine is controlled by means of hollow cylindrical valves by the rotary adjustment of which a plurality of nozzles can be put in varying numbers into and out of operation.
Fig. 1 of the accompanying drawings represents a vertical section of the turbine,
Fig. 2, a section on the line 2 2 of Fig. 1 and on an enlarged scale of the casing of a twin turbine,
Fig. 3, a cross-section of one of the valves, Fig. 4, a side view of one of the control levers, y Fig. 5, a sectional side view of the blade wheel,
Fig. 6, an axial section of the wheel, Figs. 7 and 8 are sectional views at right angles of one of the nozzle arrangements.
Figs. 9 and 10, similar views of another nozzle arrangement, i Fig. 11, a view of the first nozzlearrangement showing a modified structure,
Fig. 12, a cross-section of a valve cylinder of modified construction, l
Fig. 13, a `development of this valve cylinder, and Fig. 1i, a 1
section on the line 14-14 of Fig. 1
The turbine has a U-shaped, double-walled casing 3 in the end walls of which the turbine shaft 2 is rotatably mounted. The casing is divided horizontally on a level with the turbine shaft into two parts. The upper, segmental part has at the top a segmental slot 59 through which minor repairs of the blade 115,105, and in Germany .Tune 15, 1925.
wheel may be executed. This slot is normally closed by a correspondingly shaped lid 4 which fits the slot and which is held in position by gravity without astenings. There is an aperture 5 in the lid through which the interior of the turbine can be observed. The chambers formed between the double walls of the casing and of the lid 4 are utilized for the storage of oil and the like. At each side of the shaft 2, the casing is formed withtwo cylindrical chambers 6 and 7 4arranged parallel with the shaft, one in the upper and one in the lower part of the casing. These chambers contain and form a tight it with hollowT cylindrical valves 13 and 14 respectively which receive driving fluid through the medium of pipes 11 from a distributing pipelQ and delivers such iiuid through nozzles 10 tangentially to the blade wheel. The latter consists of a wheelbody 1 on to which a blade rim 9a is forced. This rim presents, when viewed axially as in Fig. v5, alternate circular and substantially V-shaped recesses forming between them blades 9 of corni-form cross-section turned alternately in opposite directions. The V-shaped recesses are of the same depth as the circular ones, the distance between the tips of adjacent blades is substantially uniform and the convex sides of the blades aretherefore extensiveenough for reacting effectively with the driving fluid. In the construction shown, the rim 93L is divided axially intofive sections l1& 1e which are situated between flanges 8, the blades of alternate sections being in a staggered position. Two of these sect-ions, whose blades are in alignment are fed 'from the upper valve chambers 6 and the other three, whose blades are also in alignment, are fed from the lower valve chambers 7. The nozzles 10 direct the fluid tangentially on to the blade wheel, the fluid acti-ng on the convex side of one blade `and on vthe concave side of the next, as shown in- Figs. 7 and 9. In the circular blade pre vcesses about 'two thirds 4of the surface reacts with the fluid so as to impart rotation tothe wheel, the other third of the surface serving to guide the spent iiuid back into 'the discharge ,passage between the wheel and the casing. Thenozzles at one side of the turbine are set so as to drive the blade wheel in one direction and those at the other side, in the opposite direction. Valves 21 in the pipes 11 allow the fluid to be supplied as desired to either side.
The power outpt is normally controlled by means of the valves 13 and 14 which are adjusted rotatively for putting one or more nozzles into operation. For this purpose the nozzles for each valve are arranged in alignment, and the valve is formed' with feed apertures arranged in rows each of which supplies a different number of nozzles. In Fig. 2, for in stance, whereinwthree nozzles are to be dealt with, the valve 14 has three rows of apertures 17a, 17b and 17C each of Vwhich can be turned into register with the nozzles, one row supplying three, the next two, and the third only one nozzle. Segmental slots 16 in the valve cylinders remain in communication with the supply pipes 11 in all three adjustments. Diametrically opposite the feed apertures 17, the valve cylinders have apertures 19, and diametrically opposite the nozzes 10, the casing 3 has apertures 18. rlhese apertures, when in register, allow a tool to be inserted for cleaning theapertures themselves as well as the nozzles. Normally the apertures 18 in the casing are closed by plugs 20 so as to prevent escape of fluid.
The valve cylinders arelitted with shafts` 15 whereby the adjustment is made. All the control levers are at the same side of the turbine. The near-side valve is adjusted by means of a lever 26 which is secured direct to the shaft 15. The far-side valve is adjusted by means of a bell- crank 22, 23 loosely arranged on the near-side shaft and connected by a link 25 to a lever 24 which is rigidly secured to the far-side shaft. In Fig. 2, where two turbines are arranged in juxtaposition so as to act on the same driving shaft 2` the control shafts 15 of the two turbines are in alignment and coupled by clutches 27 so that both turbines can be controlled by a single lever if desired.
Further regulation of the power output can be obtained by a throttling of the individual nozzles.
The number of nozzles and blade rim sections may be varied according to requirements, the valves being modified to correspond. Figs. l2 and 13 show an arrangement of eleven nozzles. The valve cylinder 14 is formed with lseven rows of feed apertures 10a-10g, the i'irst six of which increase their number of apertures progressively from one to six, apertures of adjacent rows being arranged in a staggered position. The last row has eleven apertures and is put into operation when for some reason, for instance in the case of a sudden reversal of the turbine, full power is required.
For regulating the position of the nozzles relative to the blades, the nozzles are ,preferably connected to a bushing 28 which allows of rotary adjustment within the valve chamber, the turbine casing being provided with a slot 22which .admits the nozzle and which is widened to allow its adjustment.
In order to allow the discharge passage between the blades and the adjacent casing wall to be varied according to requirements, the casing is preferably recessed for the reception of anexchangeable guide fillet 23 the thickness of which is chosen according to the required depth of the passage. rlhis arrangement also allows an easy compensation for wear. Behind the fillet 23 which prevents the fluid from slipping off the convex sides of the blades too easily, the casing has a recess 24 through which the fluid can readily escape so as to clear the blades after its force has been spent on the latter.
I claim 1. A turbine comprising a casing, a blade wheel in said casing, rows of nozzles fitted at the inside of said casing for supplying driving fluid to the wheel and rotatable hollow valve cylinders fitted in the casing for feeding fluid to different rows of nozzles, each valve cylinder being provided with feeding apertures arranged in parallel rows all having different numbers of apertures, the number of apertures in one of the rows being equal to the number of nozzles.
2. In a turbine, a blade wheel having ak rim which presents, when viewed in an axial direction, alternate circular and substantially V-shaped recesses forming blades of corniform cross-section turned alternately in opposite directions, the V-shaped recesses being of the saine depth as the circular ones, a casing enclosing the blade wheel, rows of nozzles fitted at the inside of the casing for supplying driving fluid to the wheel, and a rotatable hollow valve cylinder tted in the casing for feeding fluid to each row of nozzles, each valve cylinder being provided with feeding apertures arranged in parallel rows, all hav` ing different numbers of apertures, two of said rows of apertures being longer than the others and of equal length but provided with different numbers of apertures, the number of apertures in one of said rows being equal to the number of nozzles.
3. A turbine comprising a blade wheel, a casing enclosing the blade wheel, rows of nozzles fitted at the inside of the casing for supplying driving fluid to the wheel, a rotatable hollow va ive cylinder fitted in the casing and provided with apertures for feeding fluid to a row of nozzles, casing and cylinder being also formed with cleaning apertures arranged diamet-rically opposite the nozzles and the feeding apertures respectively so as to admit a cleaning tool through the nozzles from the outside, and plugs whereby the cleaning apertures of the casing are normally closed.
lOQ
llO
4;. A turbine comprising a blade wheel, a casing enclosing the blade wheel, nozzles fitted at theinside of said casing, for feeding driving fluid to the wheel, and rotatably adjustable bushings arranged parallelly with the turbine axis and holding the nozzles so that the position of the latter relative to the blades can be regulated by a rotary adjustment of said bushings.
5. A turbine comprising a blade wheel a casing enc-losing the blade wheel, nozzles ted at the inside of the casing for feeding driving fluid to the wheel, rotatably adjustable bushings arranged parallelly with the turbine axis and holding the nozzles so that the position of the latter relative to the blades can be regulated by a rotary adjustment of the bushings, and valves arranged in said bushings for controlling the fluid supply to the latter. i
G. A turbine comprising a blade wheel a casing enclosing the blade wheel, nozzles ted at the inside of said casing for feeding driving fluid to the wheel, and exchangeable i fillets arranged in recesses in the casing so as to determine the depth of the passage between the blades and the casing immediately behind the nozzles.
7. A turbine comprising a blade wheel, a casing enclosing the blade wheel, said casing being formed at the top with al segmental slot giving access to the blade wheel, and a lid fitting said slot and normally held therein by gravity so as to maintain the slot closed, the lid being formed with an aperture through which the interior of the turbine can be observed.
8. In a turbine, a vblade wheel having a rim divided into a plurality of annular sections, each section presenting, when viewed in an axial direction7 alternate circular and substantially V-shaped recesses forming blades of corniform cross-section turned alternately in opposite directions, the circular recesses comprising each substantially twothirds of a circle, the V-shaped recesses being of the same depth as the circular ones, flanges separating the different sections, a wheel body to which said sections and flanges'are independently secured, alternate sections having their blades in a staggered position, a casing enclosing the blade wheel, and rows of nozzles, having a diameter of substantially one-tenth of the diameter of the circular recesses of the rim, fitted at the inside of the casing for supplying driving fluid to the wheel.
9. In a turbine, a blade wheel having a rim which, when viewed in an axial direction, presents alternate circular and substantially V-shaped recesses forming blades of corniform cross-section turned alternately in opposite directions, the V-shaped recesses being of the same depth as the circular ones, the distance between the tips of adjacent blades being substantially uniform, a casing enclosing the blade wheel and rows of nozzles, having a diameter of substantially one-tenth of the diameter of the circular recesses of the rim, fitted at the inside of the casing for supplying driving fluid to the wheel.
10. In a turbine, a blade wheel having a rim divided into a plurality of annular sections, flanges separating the different sections, rows of nozzles for supplying driving fluid to the wheel, rotatable hollow valve cylinders for feeding fluid to different rows of nozzles, each valve cylinder being provided with feeding apertures arranged in parallel rows all having different numbers of apertures, the apertures of adjacent rows being in a staggered relative position.
1l. In a turbine, a blade wheel having a rim divided into a plurality of annular sections, llanges separating the different sections, rows of nozzles for supplying driving fluid to the wheel, rotatable hollow valve cylinders for feeding fluid to different rows of nozzles, each valve cylinder being provided with feeding apertures arranged in arallel rows all having different numbers o apertures, the apertures of adjacent rows being in a staggered relative position, one of said rows having as'many apertures as there are nozzles and being adjacent to a row having about half that number of apertures.
CARL RIX.
US115105A 1925-06-15 1926-06-10 Turbine Expired - Lifetime US1777450A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1777450X 1925-06-15

Publications (1)

Publication Number Publication Date
US1777450A true US1777450A (en) 1930-10-07

Family

ID=7742861

Family Applications (1)

Application Number Title Priority Date Filing Date
US115105A Expired - Lifetime US1777450A (en) 1925-06-15 1926-06-10 Turbine

Country Status (1)

Country Link
US (1) US1777450A (en)

Similar Documents

Publication Publication Date Title
US2316408A (en) Reciprocating cam mechanism
US1777450A (en) Turbine
US1317370A (en) Pump.
US1349487A (en) Turbine-engine
US1873199A (en) Jordan engine
US853999A (en) Propeller.
US274479A (en) Territory
US1207306A (en) Motor and pressure-distributer.
US168114A (en) Improvement in rotary engines
US784129A (en) Boiler-tube cleaner.
US1030679A (en) Engine.
US1019223A (en) Rotary engine.
US1008529A (en) Marine steam-turbine.
US98626A (en) Rotary steam-engine
US713798A (en) Impact-engine.
US961087A (en) Reaction-turbine.
US235844A (en) Paper-pulp engine
US1292038A (en) Turbine-engine.
US1198209A (en) Rotary motor.
US396759A (en) Rotary engine
US274478A (en) Tereitoey
US173744A (en) Improvement in rotary engines
US848587A (en) Elastic-fluid turbine.
US762449A (en) Elastic-fluid turbine.
US659265A (en) Apparatus for heating and dampening oleaginous meal.