US1825580A - Elastic fluid turbine - Google Patents

Elastic fluid turbine Download PDF

Info

Publication number
US1825580A
US1825580A US334291A US33429129A US1825580A US 1825580 A US1825580 A US 1825580A US 334291 A US334291 A US 334291A US 33429129 A US33429129 A US 33429129A US 1825580 A US1825580 A US 1825580A
Authority
US
United States
Prior art keywords
fluid
casing
temperature
casings
elastic fluid
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
US334291A
Inventor
Robert H Collingham
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of US1825580A publication Critical patent/US1825580A/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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26Double casings; Measures against temperature strain in casings

Definitions

  • the present invention relates to elastic fluid turbines and more particularly to turbines operating with a fluid of very high temperature. In such turbines the temperature may be such that even low' stresses in the material of which the high pressure end is constructed may cause the phenomenon known as creeping in the material unless some special construction is adopted to prevent it.
  • the object of the present invention is to provide an improved constructioniand arrangement which will overcome the above referred to difliculty, and for a consideration of what I believe to be novel and my invention, attention is directed to the following specification and the claims appended thereto.
  • the high pressure casing that is, the-portion of the casing at the high pressure end of the turbine, in two portions, the portion subjected to the very high temperature being under no tensile stress, any stress to'which it is subjected being either negligible or compression stresses of very low value.
  • Fig. l' is asectional view of thehighpressure end of a turbine embodying my invention, the low pressure. end of the turbine being indicated in outline, and Fig. 2
  • .3 is a section taken on line 2-2, Fig. 1.'
  • the high pressure and high temperatureportion of the turbine casing consists of an external casing 1 providedwith a circumferential flange 2,
  • valve 9 is shown diagrammatically and only by way of example, 1t being linderstood that ausual or desired form of valve gear is utilized.
  • Such valve gears are well known in the art and since the specific arrangement employed embodies no part of the present invention, the same has een indicated diagrammatically only.
  • the external casing 1 is provided with a conduit 14 through which Working fluid at saturation temperature and at the same pressure or substantially the same pressure as the fluid flowing through pipes 7 to the internal casing is led into the space between the external casing 1 and the internalcasing 3.
  • An elastic fluid turbine for use with elastic'fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing surrounding the internal casing in spaced relat-ion thereto, and means whereby a fluid at a; lower temperature, but of substantially the same pressure as that of the high temperature fluid may be circulated through the space between said casings.
  • An elastic fluid turbine for use with elastic fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, an external easing surrounding the internal casing in spaced relation thereto, flexibly mounted conduits for conveying high temperature elastic fluid to the internal casing, and means whereby a fluid at a lowertemperatu're but.
  • An elastic fluid turbine for use with elastic fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing surrounding the internal casing in spaced relation thereto, and means whereby a fluid at a lower temperature but of substantially the same pressure as that of the high tempera ture fluid maybe circulated through the space between said casings, said internal casing being' provided with a heat insulating covering to reduce the transference of heat from the fluid in the internal casing to the fluid in the external casing.
  • An elastic fluid turbine for use with elastic fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing sur rounding the internal casing in spaced relation thereto, flanges on said casings defining an annular discharge passage from the space between said casings, and means whereby a fluid at a lower temperature but of substantially the same pressure as that of the high temperature fluid, may be circulated through the space between said casings and said annular discharge passage.
  • An elastic fluid turbine for use with elastic fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing surrounding the internal casing in spaced relati-on thereto, a shaft which passes through said casings, packings between the casings and the shaft, walls defining an annular chamber between said packings which communicates with the space between the casings, and means whereby a fluid at a lower temperature but of substantially the same pressure as that of the high temperature fluid may be circulated through the space between said casing to the space between said packin-gs whereby said fluid serves as a sealing means for the packings.
  • An elastic fluid turbine for use with elastic fluid at a very high inital temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing surrounding the internal casing in spaced relation thereto and means for circulating fluid, other than the said elastic fluid, through said space between the casings, said second mentioned fluid being of the same pressure 40 as, but of a lower temperature than, said first mentioned fluid.
  • a method of operating elastic fluid turbines having an inner casing for carrying and surrounding diaphragms and bucket wheels respectively, an outer casing surrounding said inner casing, which comprises supplying elastic fluid to the inner turbine casing and supplying another elastic fluid of substantially the same pressure but lower temperature than the first named elastic fluid to the space formed between the inner and outer casing, whereby the elastic fluid supplied to said space is adapted to prevent strains and stresses of said inner casing and creeping eflect with respect to said outer casing.

Description

m u .e A? n 0 h 5r I66 0 5 Tmw 2 0| A t H m 6 wu E mmw pb Hmm U1 mm cc 5mm Rm Sept. 29, 1931.
Patented Sept. 29, 1931 UNITED 'STATES PATENT OFFICE ROBERT H- GOLLINGHAM, oEnUGBY, ENGLAND, nssroivon ro GENERAL COMPANY,'A CORPORATION on NEW YORK ELECTRIC T ELASTIC FLUID TURBINE Application 'filed January 22, 1929, Serial No, 334,291, and in- Great Britain January 27, 1928 The present invention relates to elastic fluid turbines and more particularly to turbines operating with a fluid of very high temperature. In such turbines the temperature may be such that even low' stresses in the material of which the high pressure end is constructed may cause the phenomenon known as creeping in the material unless some special construction is adopted to prevent it. The object of the present invention is to provide an improved constructioniand arrangement which will overcome the above referred to difliculty, and for a consideration of what I believe to be novel and my invention, attention is directed to the following specification and the claims appended thereto.
According to my invention, I construct the high pressure casing, that is, the-portion of the casing at the high pressure end of the turbine, in two portions, the portion subjected to the very high temperature being under no tensile stress, any stress to'which it is subjected being either negligible or compression stresses of very low value.
In the drawings, Fig. l'is asectional view of thehighpressure end of a turbine embodying my invention, the low pressure. end of the turbine being indicated in outline, and Fig. 2
.3 is a section taken on line 2-2, Fig. 1.'
Referring to the drawings, the high pressure and high temperatureportion of the turbine casing consists of an external casing 1 providedwith a circumferential flange 2,
"1.3 and an internal casing 3 provided with acircumferential flange 4 which is suitably fastened to flange 2 for fixing the internal casing 3 rigidly relative to the external casing 1. The internal casing 3 is provided .4 with an annular extension piece5 which extends into a corresponding'annular portion 6 forming a part of external casing 1. A deflnite small clearance radially and circumferentially is provided between parts 5 and 6.
1 The working fluid at the initially very high temperature is admitted to the internal casing '3 by pipes 7 which are provided with swivellingconduits 8 between the external and the internal casings to permit of differences in expansion between the two casings.
' It will be understood that the turbine beyond so the first stagev nozzles and wheel comprises a usual or desired construction of diaphragms and wheels. Also the valve 9 is shown diagrammatically and only by way of example, 1t being linderstood that ausual or desired form of valve gear is utilized. Such valve gears are well known in the art and since the specific arrangement employed embodies no part of the present invention, the same has een indicated diagrammatically only.
The external casing 1 is provided with a conduit 14 through which Working fluid at saturation temperature and at the same pressure or substantially the same pressure as the fluid flowing through pipes 7 to the internal casing is led into the space between the external casing 1 and the internalcasing 3.
With the construction illustrated, a small flow of saturated or slightly superheated elastic fluid is obtained in the space between" the external and internal casings through the clearance space between annular portions 5 and 6, and this flow is usefully employed for sealing the shaft 18 of the turbine where it passes throughthe packings 15 and 16 between the shaft and the casings 1 and 3 respectively. It is necessary to maintain a slight flow of the saturated fluid led in by the conduit 14 between the internal and external casings, in order to prevent this fluid from becoming too highlysuperheated. The internal casing is lagged with non-conducting material 17 to reduce to a minimum transference of heat to the initially saturated fluid circulating between casings 1 and 3.
Since the pressure of the saturated working fluid led in by conduit 14 to the space between the two casings is practically the same pressure as that of the very highly superheated fluid led in through pipes 7 and flexible conduits 8, negligible stress exists in the portions of the internal casing carrying the initially very highly superheated fluid. As the fluid expands inside the internal casing 3, the temperature and the pressure fall simultaneously, and the pressure of the saturated or slightly superheated .fluid in the space between the two casings is higher than that of the expanding fluid in the internal casing 3,
which means that the stresses in the internal swivelling conduits 8 have to seal against temperature only, and not against pressure difference, and can therefore be a comparatively easy fit in the casings 1. and 3.
Thus it will be understood that the construction of elastic fluid" turbines and the method of operating them according to my invention is adapted tosuccess'tully prevent substantial strains and stresses within the inner turbine casing and is also adapted tov prevent strains within the outer casing thereof, as well as the creeping effect of this outer casing which heretofore was a great obstacle in the turbine art. To make this clear, attention is called to the fact that tests have shown that, for instance, bolts of the outer turbine casing which were applied with a tensile strength of 28,000 pounds lost about-70% of this strength after less than one year of operation at temperatures in the neighborhood of 750 F; These obstacles are overcome by supplying a fluid to the space between the inner and outer casing of a temperature which is lower than the temperature of the operative fluid within the inner casing. This may be performed by supplying the fluid to this space directly from the boiler, whereas the operative fluid is supplied from a superheater. The lower temperature of the fluid between the inner and outer casing further more permits the use of cheaper packing ma terial and also has less wearing effect on this material, ,as would be the case if a fluid of high temperature were used, and finally, the
low temperature necessitates less heat insu- 'lating material and causes less heat losses through the outer casing.
I have referred above to saturated and superheated working fluid, but it is to be understood that the invention is not confined only to fluid having a saturation point in the working cycle, such as steam, as obviously I could employ a compressed gas which would be led at a very high temperature through pipes 7 into internal casing 3, and a supply of cooled gas at the same pressure as that initially supplied to the turbine pipes 7 would be led through conduit 14 into the space between casings l and 3, the temperature of the cooled gas being such that reasonably high tensile stresses could be carried in the external casing 1.
In accordance with the provisions of the patent statutes I have described the principle of operation of my invention together with the apparatus which I now consider to represent thebest embodiment thereof, and it is to be understood that the arrangement shown isonly illustrative and that the invention may-be carried out by other means.
lVhat I claim as new and desire to secure by Letters Patent of the United States is:
1. An elastic fluid turbine for use with elastic'fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing surrounding the internal casing in spaced relat-ion thereto, and means whereby a fluid at a; lower temperature, but of substantially the same pressure as that of the high temperature fluid may be circulated through the space between said casings.
2. An elastic fluid turbine for use with elastic fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, an external easing surrounding the internal casing in spaced relation thereto, flexibly mounted conduits for conveying high temperature elastic fluid to the internal casing, and means whereby a fluid at a lowertemperatu're but.
of substantially the same pressure at that of the high temperature fluid may be circulated throughthe space between said casings.
'3. An elastic fluid turbine for use with elastic fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing surrounding the internal casing in spaced relation thereto, and means whereby a fluid at a lower temperature but of substantially the same pressure as that of the high tempera ture fluid maybe circulated through the space between said casings, said internal casing being' provided with a heat insulating covering to reduce the transference of heat from the fluid in the internal casing to the fluid in the external casing.
4. An elastic fluid turbine for use with elastic fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing sur rounding the internal casing in spaced relation thereto, flanges on said casings defining an annular discharge passage from the space between said casings, and means whereby a fluid at a lower temperature but of substantially the same pressure as that of the high temperature fluid, may be circulated through the space between said casings and said annular discharge passage.
5. An elastic fluid turbine for use with elastic fluid at a very high initial temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing surrounding the internal casing in spaced relati-on thereto, a shaft which passes through said casings, packings between the casings and the shaft, walls defining an annular chamber between said packings which communicates with the space between the casings, and means whereby a fluid at a lower temperature but of substantially the same pressure as that of the high temperature fluid may be circulated through the space between said casing to the space between said packin-gs whereby said fluid serves as a sealing means for the packings. V
6. An elastic fluid turbine for use with elastic fluid at a very high inital temperature comprising an internal casing, inlet nozzles carried by the internal casing, means for conveying elastic fluid of high initial temperature to said nozzles, an external casing surrounding the internal casing in spaced relation thereto and means for circulating fluid, other than the said elastic fluid, through said space between the casings, said second mentioned fluid being of the same pressure 40 as, but of a lower temperature than, said first mentioned fluid.
7. A method of operating elastic fluid turbines having an inner casing for carrying and surrounding diaphragms and bucket wheels respectively, an outer casing surrounding said inner casing, which comprises supplying elastic fluid to the inner turbine casing and supplying another elastic fluid of substantially the same pressure but lower temperature than the first named elastic fluid to the space formed between the inner and outer casing, whereby the elastic fluid supplied to said space is adapted to prevent strains and stresses of said inner casing and creeping eflect with respect to said outer casing.
In witness whereof, I have hereunto set my hand this 2nd day of January, 1929.
ROBERT H. COLLINGHAM.
US334291A 1928-01-27 1929-01-22 Elastic fluid turbine Expired - Lifetime US1825580A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1825580X 1928-01-27

Publications (1)

Publication Number Publication Date
US1825580A true US1825580A (en) 1931-09-29

Family

ID=10891451

Family Applications (1)

Application Number Title Priority Date Filing Date
US334291A Expired - Lifetime US1825580A (en) 1928-01-27 1929-01-22 Elastic fluid turbine

Country Status (1)

Country Link
US (1) US1825580A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2425177A (en) * 1943-05-11 1947-08-05 United Aircraft Corp Turbine construction
US2855178A (en) * 1954-07-14 1958-10-07 Vickers Armstrongs Ltd Turbines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2425177A (en) * 1943-05-11 1947-08-05 United Aircraft Corp Turbine construction
US2855178A (en) * 1954-07-14 1958-10-07 Vickers Armstrongs Ltd Turbines

Similar Documents

Publication Publication Date Title
US2282894A (en) Elastic fluid turbine
US2552239A (en) Turbine rotor cooling arrangement
US2304994A (en) Turbine cylinder cooling
US1562019A (en) Shaft packing for elastic-fluid turbines and the like
US3630635A (en) Turbine casing with raised horizontal joint
US1352277A (en) Elastic-fluid turbine
US1825580A (en) Elastic fluid turbine
US1536014A (en) Packing for elastic-fluid turbines and the like
US2112738A (en) Elastic fluid turbine
US1505924A (en) Shaft packing for elastic-fluid turbines and the like
US2547300A (en) Diaphragm for reheat elastic fluid turbines
US2367134A (en) Steam chest construction
US2920867A (en) Reheat turbine apparatus
US2524724A (en) Turbine apparatus
GB1059435A (en) Shaft seals for thermal machines
US2823890A (en) Housing for gas or steam turbines
US2279814A (en) Packing arrangement
US2235547A (en) Elastic fluid turbine
US2394125A (en) Tandem compound elastic fluid turbine arrangement
US1541834A (en) Axial turbine
GB733537A (en) Improvements in or relating to housings for gas or steam turbines
US2503914A (en) Elastic fluid turbine casing
US1554230A (en) Steam turbine
US2181744A (en) Turbine casing joint
US2925995A (en) Turbine apparatus