US1473690A - Serial-flow turbine - Google Patents

Serial-flow turbine Download PDF

Info

Publication number
US1473690A
US1473690A US564758A US56475822A US1473690A US 1473690 A US1473690 A US 1473690A US 564758 A US564758 A US 564758A US 56475822 A US56475822 A US 56475822A US 1473690 A US1473690 A US 1473690A
Authority
US
United States
Prior art keywords
steam
rotor
serial
blades
exhaust
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
US564758A
Inventor
Oscar H Wolner
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 US564758A priority Critical patent/US1473690A/en
Application granted granted Critical
Publication of US1473690A publication Critical patent/US1473690A/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

  • lMy invention relates to serial How turbines, and consists in providing means whereby the steam is admitted at a pluralm ity-of points about the periphery of the turbinel casing through controlled nozzles.
  • the steam from each nozzle acts on the rotor blades a plurality of times, and is divided each time into two lateral streams by a 25 ycentral'- rib on ,the rotor and then exhausts 'laterally to two exhaust chambers, one on each'side of the biedingl and is conducted to a 'common discharge.
  • the turbine may. operate in 30' with acondenser or not, as desired.
  • Fig.. ⁇ 3 is an end view, partly 1n section, .45 and-"- y l l' Y.
  • Figa 4 isa longitudinal section through the entire turbine.
  • the rotor 6 has a hub or annular flange 14C that fits against theinner edges of the two lateral dished cover members 15 and 16. Annular external ribs 17 near the center of these members provide sucient metal for the holding bolts 18 for securing packing glands 19. Y
  • the valves 26 are tapered and have screw-threaded portions 28 of at least as tQreat a diameter as the valves so that each individual valve may be readily removed without removing the bushing' 29,
  • the rotor '6 has a central rib 30 between lateral flanges 31 forming two continuous grooves 32 having rounded bottoms, the outer sides of the grooves being decidedly inclined to the central vertical plane through the rib tu facilitate the enit vof steam.
  • the rotor is slotted from sidente side and inserted in these slots are the dat plate turbine 'blades 33 which ⁇ with their rounded 'Shanks 34 are slightly tapered for a proper ldriving lit. 1
  • the guide blades 35 are similarly made. ln the middle member 2() the dividing portion 36 has inwardly projectile" danges- 37 which some O the guide bla es are' tted charge openings 40, Fig. 2, to the exhaust channels 22, and behind each exhaust chamber 39 are two expansion chambers 38, which arrangement prevails between each two successive steam supply nozzles 27, the
  • Live steam is admitted, to the turbine through inlet union 24 and fills the steam channel 21.
  • the cone valves 26 are gradually opened andj steam passesthrough the nozzles 27 and impi'nges on the rotor blades 33, being divided into two streams by the rib 30.
  • stator blades 35 are somewhat wider than the bevelled ends of the rotor blades 33, so that there will be a period of time when there will not be a continuous open passage from an inlet nozzle 27 to the exhaust.
  • a bladed stator having a peripheral ⁇ steam channel and a peripheralexhaustv channel' at each side 'tion with a bladed rotor and seated in iheslots of rotor.
  • a bladed'stator having live steam'and exhaust channels, a plurality of angularly spaced, valve-controlled steam inlet nozzles to admit steam from said live steam channel, an expansion chamber between successive nozzles, an ex ⁇ - haust chamber back of each nozzle and a bladed rotor having a rib dividing the steam into lateral streams tolsaid expansion chamber and exhaust.
  • a stator having a middle member having a peripheral steam channel, and Hat blades arranged' in transverse slots in said stator and extending from side to side thereof, steam inlet nozzles to admit steam between a pair'of blades, aplurality ot expansion chambers between suceessive nozzles, an exhaust chamber behind each nozzle and peripheral exhaust channels flanking the steam channel, each exhaust chamber having ports leading to both of said exhaust channels.
  • the combinaldisc having a central flange, (lished covers spaced from said disc and :formingr leakage chambers, and a packing gland between said flange and Covers.
  • stator transversely'slotted, a rotor transversely slotted, and laterally removable flat transversely tapered plate blades havng enlarged Shanks said stator and steam distributing member having a middle steam channel and a continuous exhaust channel on each side of sald steam channel, steam nozzles Supplied from said channel, a bladed rotor .having a mid rib forming pairs of buckets between each two su'cceeding blades, dished covers secured .tol

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

NGV. 13,1923, www
O. H. VVOLNER SERIAL .FLOW TURBINE Filed May 31 1922 3 Sheets-Sheet 1 Nm 13A, 3923i, 4 lpgg@ O. H. WOLNER SERIAL FLow TURBINE Filed May s1, 1922 :s sneetsushwf; S
v vivente/c @am/Wmv Sw @M953 Patented hier. ld, i223.
entre erts artnr OSC'AR H. WOLNER, OlF ELCGR, MINNESOTA.
snaren-rauw runnrnn.
Application le May 31,. 19222. Serial No. 564,758.
To aZZ whom t 'may concern:
A Beit known that l, OSCAR Hnnnn'r WOLNER, a citizen of the United States of Aunerica, and -a resident of Elcor, in the d county-of St. Louis and State of Minnesota,
m scriptlon of the invention, such as will en! able others skilled in the 'art to which it 'appbrtains to make and use the same. refl erence being had to the accompanying drawings, and to letters or gures'of reference )1li marked thereon, which form a part of this specification.
lMy invention relates to serial How turbines, and consists in providing means whereby the steam is admitted at a pluralm ity-of points about the periphery of the turbinel casing through controlled nozzles. The steam from each nozzle acts on the rotor blades a plurality of times, and is divided each time into two lateral streams by a 25 ycentral'- rib on ,the rotor and then exhausts 'laterally to two exhaust chambers, one on each'side of the biedingl and is conducted to a 'common discharge. y The turbine may. operate in 30' with acondenser or not, as desired.
' The steam distribution is such that the turbine starts with great facility and the separately controlled steam nozzlesA enable vutilization of the steam variable in accord` 35 '.ancewitha wide range of power requirements v Referring to the drawings, which illustrate my invention, Vand in which like parts are similarly designatedl 40 Figure 1 is an enlarged partial longitudinal-section through a steam supply nozzle and the adjacent blades. l
Fig. 2jis 'a section von line 2-2, Fig. 1.
Fig..`3 is an end view, partly 1n section, .45 and-"- y l l' Y.Figa 4 isa longitudinal section through the entire turbine.
Lhavfe chosen to illustrate my invention lin connection with a turbine ofthe discou type having' a central rotor ldisc t, Fig, 3,
conjunction secured by bolts 7 or otherwise between flanges 8 of two alinedshafts 9 and 10.
and 12 on a base 13.
The rotor 6 has a hub or annular flange 14C that fits against theinner edges of the two lateral dished cover members 15 and 16. Annular external ribs 17 near the center of these members provide sucient metal for the holding bolts 18 for securing packing glands 19. Y
These shafts are mounted in pedestals l1v At the periphery these covers 11.5 and 16 (which are somewhat dished are wider apart than at their center, an secured between them is the annular steam distributing member 20, having a middle peripheral live steam channel 2l and two lateral peripheral exhaust channels 22 that terminate or discharge into the exhaust lpipe union 23. A
The uve steam 'pipe union 24, rig, 4., .is
shown located in a horizontal position, but
may be located at any other point of the' periphery to suit the conditions existing at the plant where it is to be used.
There are also provided supports 25' for lthe turbine that are bolted tothe base 13.
iltl
Around the steam distributing member are steam valves 26 controlling steam supply nozzles 27. The valves 26 are tapered and have screw-threaded portions 28 of at least as tQreat a diameter as the valves so that each individual valve may be readily removed without removing the bushing' 29,
shown in enlarged View, Figs. l and 2.
The rotor '6 has a central rib 30 between lateral flanges 31 forming two continuous grooves 32 having rounded bottoms, the outer sides of the grooves being decidedly inclined to the central vertical plane through the rib tu facilitate the enit vof steam.
The rotor is slotted from sidente side and inserted in these slots are the dat plate turbine 'blades 33 which `with their rounded 'Shanks 34 are slightly tapered for a proper ldriving lit. 1 The guide blades 35 are similarly made. ln the middle member 2() the dividing portion 36 has inwardly projectile" danges- 37 which some O the guide bla es are' tted charge openings 40, Fig. 2, to the exhaust channels 22, and behind each exhaust chamber 39 are two expansion chambers 38, which arrangement prevails between each two successive steam supply nozzles 27, the
object being to cause the steal 1 from the steam nozzles 27 to act directly on the rotor blades 33,`and' as these pass the vstationary 'guide blades 35 to expand'it a plurality of times in. pockets 38 and cause the Steam after each expansion'to act again on the rotor blades, finally exhausting justbehind the next 'inlet nozzle 27.
The operation is as `it'ollows:
Live steam is admitted, to the turbine through inlet union 24 and fills the steam channel 21. The cone valves 26 are gradually opened andj steam passesthrough the nozzles 27 and impi'nges on the rotor blades 33, being divided into two streams by the rib 30. As the rotor moves past the stationary guide blades steam from the pocket formed between two successive rotor lblades issues in twostreams between the next successive guide' blades 35 into the first expansion c amber 38, passes around the root of blade 37 therein tothe opposite side blade and is directed again against the rotor blades, this operation, in the present instance, is repeated in the following expansion chamber 38, and the steam finally leaves the rotor through exhaust chamber 39' and passages 40 in a divided stream to the two exhaust channels 22 to the exhaust pipe at 23. The steam in .passing from between a moving pair of rotor blades while expanding in an expansion chamber is of course augmented by, steam from the next following blade.
Any leakage at the joint between the rotor and stator passes into lateral chambers 4l between the rotor'disc 6 and the casing' members 15 and ltlvproducing a counter pressure, while radiation of heat from the live steam channel 212i is guarded against by arranging it between the exhaust channels 22. i
The bevelled ends .of the stator blades 35 are somewhat wider than the bevelled ends of the rotor blades 33, so that there will be a period of time when there will not be a continuous open passage from an inlet nozzle 27 to the exhaust.
I claim--4 l. In a serial flow turbine, a bladed stator having a peripheral `steam channel and a peripheralexhaustv channel' at each side 'tion with a bladed rotor and seated in iheslots of rotor.
7. In a serial flow tubine, an annularY Jfrom said live steam channel, expansion chambers between successive nozzles in the rotor plane, a bladed rotor havingfia midrib forming a pair of buckets between each two succeeding blades, said pair of buckets not exceeding the width of said nozzles and expansion chambers, there being lateral exhaust ports in Said stator to exhaust cham be s behind each nozzle,v
'il In a serial How turbine, a bladed'stator having live steam'and exhaust channels, a plurality of angularly spaced, valve-controlled steam inlet nozzles to admit steam from said live steam channel, an expansion chamber between successive nozzles, an ex`- haust chamber back of each nozzle and a bladed rotor having a rib dividing the steam into lateral streams tolsaid expansion chamber and exhaust.
4. In a serial li'ow turbine, a stator having a middle member having a peripheral steam channel, and Hat blades arranged' in transverse slots in said stator and extending from side to side thereof, steam inlet nozzles to admit steam between a pair'of blades, aplurality ot expansion chambers between suceessive nozzles, an exhaust chamber behind each nozzle and peripheral exhaust channels flanking the steam channel, each exhaust chamber having ports leading to both of said exhaust channels.
5. In a serial flow turbine, the combinaldisc having a central flange, (lished covers spaced from said disc and :formingr leakage chambers, and a packing gland between said flange and Covers.
6. In a serial flow turbine, a stator transversely'slotted, a rotor transversely slotted, and laterally removable flat transversely tapered plate bladeshavng enlarged Shanks said stator and steam distributing member having a middle steam channel and a continuous exhaust channel on each side of sald steam channel, steam nozzles Supplied from said channel, a bladed rotor .having a mid rib forming pairs of buckets between each two su'cceeding blades, dished covers secured .tol
said member and between, which said rotor points behind the respec-Y turns, and packing means between the rotor and covers. v
8. In a Serial iow turbine, a biaded peripheral steam distributing member, dished 5 covers secured to said member, a bladed rotor disc mounted between said covers,v a
packing between said rotor and Covers, e
continuous elef tinuous eiiiane steam channel in testimony het as my inentien i here Si hereto.,
US564758A 1922-05-31 1922-05-31 Serial-flow turbine Expired - Lifetime US1473690A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US564758A US1473690A (en) 1922-05-31 1922-05-31 Serial-flow turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US564758A US1473690A (en) 1922-05-31 1922-05-31 Serial-flow turbine

Publications (1)

Publication Number Publication Date
US1473690A true US1473690A (en) 1923-11-13

Family

ID=24255762

Family Applications (1)

Application Number Title Priority Date Filing Date
US564758A Expired - Lifetime US1473690A (en) 1922-05-31 1922-05-31 Serial-flow turbine

Country Status (1)

Country Link
US (1) US1473690A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060034683A1 (en) * 2004-08-16 2006-02-16 Honeywell International Inc. Adjustable flow turbine nozzle
US20100178153A1 (en) * 2007-06-08 2010-07-15 Walter Gehringer Turbine Having Compact Inflow Housing Thanks to Internal Control Valves

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060034683A1 (en) * 2004-08-16 2006-02-16 Honeywell International Inc. Adjustable flow turbine nozzle
US7165936B2 (en) * 2004-08-16 2007-01-23 Honeywell International, Inc. Adjustable flow turbine nozzle
US20100178153A1 (en) * 2007-06-08 2010-07-15 Walter Gehringer Turbine Having Compact Inflow Housing Thanks to Internal Control Valves

Similar Documents

Publication Publication Date Title
US2651496A (en) Variable area nozzle for hightemperature turbines
US3945758A (en) Cooling system for a gas turbine
US1022683A (en) Turbine.
US1473690A (en) Serial-flow turbine
US1883868A (en) Turbine nozzle block
US2316813A (en) Bearer for the stationary vanes of rotary motors
US1896809A (en) Multistage turbine
US1741957A (en) Cooling device for the reversing stator blades of turbines
US714074A (en) Steam-turbine.
US791949A (en) Turbine.
US1012813A (en) Turbine.
US1865551A (en) Reversing steam turbine with variable velocity
US753769A (en) Supply-nozzle for turbines.
US1405091A (en) Steam turbine
US1375075A (en) gaumann
US735107A (en) Turbine.
US798106A (en) Steam-turbine nozzle.
US927658A (en) Steam-turbine.
US868653A (en) Turbine.
US1741072A (en) Rotary engine
US1490907A (en) Steam turbine
US970106A (en) Steam-turbine.
US794606A (en) Turbine.
US1383916A (en) Rotary engine
US1671967A (en) Turbine