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US737042A - Wheel or disk for steam-engines. - Google Patents

Wheel or disk for steam-engines. Download PDF

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Publication number
US737042A
US737042A US15094403A US1903150944A US737042A US 737042 A US737042 A US 737042A US 15094403 A US15094403 A US 15094403A US 1903150944 A US1903150944 A US 1903150944A US 737042 A US737042 A US 737042A
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US
United States
Prior art keywords
wheel
steam
disk
engines
rim
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
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US15094403A
Inventor
Johann Stumpf
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Individual
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Priority to US15094403A priority Critical patent/US737042A/en
Application granted granted Critical
Publication of US737042A publication Critical patent/US737042A/en
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Expired - Lifetime legal-status Critical Current

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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
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/08Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
    • F04D25/088Ceiling fans

Definitions

  • Attorn ym Noam: PETERS co. moYoumn. WASHINGTON. n, c
  • the invention is not limited, of course, to the particular kind of turbine employed nor to the shape or disposition of the blades, while the invention is, moreover, applicable to turbines of any system in which wheels, cylinders, or their equivalent are employed for mounting and carrying the moving blades.
  • a steam-turbine wheel having the rim constituted of. a number of separate segmental parts, free spaces between the said parts, and

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

Description

PATENTED AUG. 25, 1 903.
J. STUMPF. WHEEL OR DISK FOR STEAM ENGINES.
APPLIGATION FILED APR. 3. 1903.
no MODEL.
Inventor W'Ltnesses- {M ,1 Q
Attorn ym: Noam: PETERS co. moYoumn. WASHINGTON. n, c
Patented August 25, 1903.
, PATENT OFFICE.
JOHANN STUMPF, OFBERIJIN, GERMANY.
WHEEL OR DISK FOR S TEAM-ENGINES.
SPECIFICATION forming'part of Letters ram NQ.'737,042, dated August 25,1903.
Application filed April 3. 1903.
To all whom it may concern:
Be it known that I, JOHANN STUMPF, a subject of the German Emperor, residing at 27 Rankestrasse, Berlin, Germany, have invented certain new and useful Improvements Relating to the Wheels or Disks of Steam- Turbines, of which the following is aspecification.
In steam-turbines which are f urnished-with relatively large wheels the radiation of heat from the casing indicates a temperature of the rim of the wheel which is very considerably higher than the temperature of the disk or web of the wheel. If steam is introduced into the casing of a somewhat high pressure, the rim of the wheel becomes of a temperature of 150 and more, as trials have confirmed, while the disk or web of the Wheel has the temperature corresponding to that of the condenser, which amounts to about from to Afurther increase of temperature ofthe rim of the wheel results fromthe friction of the steam on the blade-surfaces. The superheating resulting from the friction on the wall of the casing is transmitted partly to the steam, but also partly to the wheel. In practice with such turbine-wl1eels splits and cracks result, and in order to prevent the durability. of the whole turbine being endangered thereby therim of the wheel according to the present invention is allowed to expand or to eX- tend. This is effected in the simplest manner by the provision of incisions on the rim of the wheel at certain distances apart, determined according to the dimensions and the Serial Nol50,944=. (No model.)
metal of the turbine-wheel as well as to the temperatures involved.
The accompanying drawings; represent in Figures 1 and 2 a partial cross-section and partial elevation of a turbine-wheel provided according to the invention. In the drawings a comparatively thin disk a has the rim 1) overhanging on each side, and on the circumference of the rim blades 0 are indicated. On the rim at certain distances apart radial incisionsor saw-cuts d are provided, which terminate in transversely-bored holes f in the disk a. y
' The invention is not limited, of course, to the particular kind of turbine employed nor to the shape or disposition of the blades, while the invention is, moreover, applicable to turbines of any system in which wheels, cylinders, or their equivalent are employed for mounting and carrying the moving blades.
What I claim as my invention, and desire to secure by Letters Patent, is
A steam-turbine wheel having the rim constituted of. a number of separate segmental parts, free spaces between the said parts, and
blades or vanes intermediate of said free spaces, substantially as described.
In testimony whereof I have signed my name to this specification in the presence of two subscribing witnesses.
Witnesses:
HENRY HASPER, WOLDEMAR HAUPT.
JOHANN s'rU PF.
US15094403A 1903-04-03 1903-04-03 Wheel or disk for steam-engines. Expired - Lifetime US737042A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US15094403A US737042A (en) 1903-04-03 1903-04-03 Wheel or disk for steam-engines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15094403A US737042A (en) 1903-04-03 1903-04-03 Wheel or disk for steam-engines.

Publications (1)

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US737042A true US737042A (en) 1903-08-25

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US15094403A Expired - Lifetime US737042A (en) 1903-04-03 1903-04-03 Wheel or disk for steam-engines.

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3847506A (en) * 1973-11-29 1974-11-12 Avco Corp Turbomachine rotor
US20060039791A1 (en) * 2004-08-20 2006-02-23 Samsung Techwin Co., Ltd. Radial-flow turbine wheel
EP2075411A1 (en) * 2007-12-28 2009-07-01 United Technologies Corporation Integrally bladed rotor with slotted outer rim and gas turbine engine comprising such a rotor
US20150118048A1 (en) * 2013-10-24 2015-04-30 Honeywell International Inc. Gas turbine engine rotors including intra-hub stress relief features and methods for the manufacture thereof
US9273563B2 (en) 2007-12-28 2016-03-01 United Technologies Corporation Integrally bladed rotor with slotted outer rim
US10040122B2 (en) 2014-09-22 2018-08-07 Honeywell International Inc. Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities
US20190226342A1 (en) * 2018-01-19 2019-07-25 MTU Aero Engines AG Rotor, in particular blisk of a gas turbine, having a broken-up rim and method for producing the same

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3847506A (en) * 1973-11-29 1974-11-12 Avco Corp Turbomachine rotor
US20060039791A1 (en) * 2004-08-20 2006-02-23 Samsung Techwin Co., Ltd. Radial-flow turbine wheel
US7481625B2 (en) * 2004-08-20 2009-01-27 Samsung Techwin Co., Ltd. Radial-flow turbine wheel
US9133720B2 (en) 2007-12-28 2015-09-15 United Technologies Corporation Integrally bladed rotor with slotted outer rim
US20110182745A1 (en) * 2007-12-28 2011-07-28 Suciu Gabriel L Integrally bladed rotor with slotted outer rim
EP2075411A1 (en) * 2007-12-28 2009-07-01 United Technologies Corporation Integrally bladed rotor with slotted outer rim and gas turbine engine comprising such a rotor
US9273563B2 (en) 2007-12-28 2016-03-01 United Technologies Corporation Integrally bladed rotor with slotted outer rim
US20150118048A1 (en) * 2013-10-24 2015-04-30 Honeywell International Inc. Gas turbine engine rotors including intra-hub stress relief features and methods for the manufacture thereof
US9714577B2 (en) * 2013-10-24 2017-07-25 Honeywell International Inc. Gas turbine engine rotors including intra-hub stress relief features and methods for the manufacture thereof
US10040122B2 (en) 2014-09-22 2018-08-07 Honeywell International Inc. Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities
US10807166B2 (en) 2014-09-22 2020-10-20 Honeywell International Inc. Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities
US11305348B2 (en) 2014-09-22 2022-04-19 Honeywell International Inc. Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities
US20190226342A1 (en) * 2018-01-19 2019-07-25 MTU Aero Engines AG Rotor, in particular blisk of a gas turbine, having a broken-up rim and method for producing the same

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