BG110012A - Intermediate distribution ring - Google Patents

Intermediate distribution ring Download PDF

Info

Publication number
BG110012A
BG110012A BG110012A BG110012A BG110012A BG 110012 A BG110012 A BG 110012A BG 110012 A BG110012 A BG 110012A BG 110012 A BG110012 A BG 110012A BG 110012 A BG110012 A BG 110012A
Authority
BG
Bulgaria
Prior art keywords
distribution ring
intermediate distribution
ring
circumference
blade profile
Prior art date
Application number
BG110012A
Other languages
Bulgarian (bg)
Inventor
Vlastimil Sedlacek
Original Assignee
Vlastimil Sedlacek
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=38920769&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=BG110012(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Vlastimil Sedlacek filed Critical Vlastimil Sedlacek
Publication of BG110012A publication Critical patent/BG110012A/en

Links

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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/11Shroud seal segments
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/40Use of a multiplicity of similar components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/80Platforms for stationary or moving blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Insulating Bodies (AREA)
  • Welding Or Cutting Using Electron Beams (AREA)
  • Automatic Assembly (AREA)

Abstract

The intermediate distribution ring will find application in power-plants. The problem is solved of the exact installation of the intermediate distribution ring and the stability of the active body flow volume. The assembly is facilitated, the degree of labour-consumption is reduced and so are the production costs. The intermediate distribution ring for turbine wheels consists of a halved ring (1), which is provided throughout its circumference with a through blade profile (2).

Description

ОБЛАСТ НА ТЕХНИКАТАTECHNICAL FIELD

Изобретението се отнася до междинен разпределителен пръстен за турбинни колела, намиращ приложение в електрически централи.The invention relates to an intermediate turbine wheel distribution ring for use in power plants.

ПРЕДШЕСТВАЩО СЪСТОЯНИЕ НА ТЕХНИКАТАBACKGROUND OF THE INVENTION

Известно е досега, че междинните лопатки се произвеждат поотделно и се монтират на отделно звено.It is known so far that the intermediate blades are manufactured individually and mounted on a separate unit.

Значителен недостатък на тази секционна съставна ситема се състои се в това, че монтажът не е точен и обемът на потока от активно тяло не е устойчив. Монтажът е свързан с голяма трудоемкост и производството изисква специални машини за изработване на отделните части. Накрая, без това да е маловажно, производствените разходи са високи, така че, крайната цена на оборудването е твърде висока.A significant disadvantage of this sectional component system is that the assembly is not accurate and the volume of flow from the active body is not stable. The installation is very labor intensive and the production requires special machines for making the individual parts. Last but not least, production costs are high, so the final cost of the equipment is too high.

ТЕХНИЧЕСКА СЪЩНОСТ НА ИЗОБРЕТЕНИЕТОSUMMARY OF THE INVENTION

Техническият проблем, който трябва да се реши е да се създаде междинен разпределителен пръстен, при който монтажът да е точен и обемът на потока от активно тяло да е устойчив. Монтажът да е облекчен с намалена трудоемкост, а производствените разходи да са намалени.The technical problem to be solved is to create an intermediate distribution ring, in which the mounting is accurate and the volume of flow of the active body is stable. Installation should be less labor intensive and production costs reduced.

Този технически проблем е решен посредством междинен разпределителен пръстен, съгласно това изобретение, имащ следната същност: той се състои от разполовен пръстен, осигурен по цялата си обиколка с проходен лопатъчен профил.This technical problem is solved by an intermediate distribution ring according to this invention having the following essence: it consists of a split ring provided along its entire circumference by a passable blade profile.

Междинният разпределителен пръстен, конструиран съгласно това изобретение има предимствата, че дава възможност пръстенът да се монтира с висока точност на потока от активно тяло, без никаква възможност за флуктуация на потока. Трудоемкостта изисквана за съставяне на целия пръстен по време на монтаж се намалява няколко пъти, като многократно се намаляват разходите за монтаж.The intermediate distribution ring constructed in accordance with this invention has the advantage that it enables the ring to be mounted with high precision of the flow of the active body without any possibility of fluctuation of the flow. The complexity required to assemble the entire ring during assembly is reduced several times, reducing installation costs many times over.

ПОЯСНЕНИЕ НА ПРИЛОЖЕНИТЕ ФИГУРИEXPLANATION OF THE FIGURES Attached

Изобретението ще бъде изяснено по-детайлно посредством чертежите, които са изобразени, като е представено наThe invention will be explained in more detail by way of the drawings which are shown, as presented in

Фиг. 1: Изглед отпред на междинен разпределителен пръстен, състоящ се от две части и наFIG. 1: Front view of an intermediate distribution ring consisting of two parts and a

Фиг. 2: Напречно сечение на междинен разпределителен пръстен iFIG. 2: Cross section of an intermediate distribution ring i

ПРИМЕРИ ЗА ИЗПЪЛНЕНИЕ НА ИЗОБРЕТЕНИЕТОEXAMPLES FOR THE IMPLEMENTATION OF THE INVENTION

Междинният разпределителен пръстен, съгласно Фиг. 1, се състои от разполовения пръстен 1, имащ около своята обиколка проходен лопатъчен профил 2.The intermediate distribution ring according to FIG. 1, consists of a split ring 1 having a perforated blade profile 2 about its circumference.

ИНДУСТРИАЛНА ПРИЛОЖИМОСТINDUSTRIAL APPLICABILITY

Междинният разпределителен пръстен, съгласно изобретението, е предназначен за турбини за парни централи, но може да се използва за всякакви задвижващи работни тела, където се изисква висока точност на дозиране на работното тяло.The intermediate distribution ring according to the invention is intended for steam turbines, but can be used for any actuators where high dosing accuracy of the working fluid is required.

• · V • · · fc • · V • · · fc • ·· • • ·· • • · * • · * » • » • · » • » • · • · · · • • • · · · • • • · • · ···· * ···· * • · • · • · · • · · ··· ··· ···♦ ··· ♦ • « ·· • «·· • • • •

ПАТЕНТНИ ПРЕТЕНЦИИPatent Claims

Claims (1)

ПАТЕНТНИ ПРЕТЕНЦИИPatent Claims 1. Междинен разпределителен пръстен, характеризиращ се с това, че се състои от разполовен пръстен (1), осигурен по цялата си обиколка с проходен лопатъчен профил (2).An intermediate distribution ring, characterized in that it consists of a split ring (1) provided throughout its circumference with a through-blade profile (2).
BG110012A 2007-10-11 2007-12-04 Intermediate distribution ring BG110012A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CZ200719269U CZ18174U1 (en) 2007-10-11 2007-10-11 Blade spacer ring

Publications (1)

Publication Number Publication Date
BG110012A true BG110012A (en) 2009-04-30

Family

ID=38920769

Family Applications (1)

Application Number Title Priority Date Filing Date
BG110012A BG110012A (en) 2007-10-11 2007-12-04 Intermediate distribution ring

Country Status (8)

Country Link
CN (1) CN101408113A (en)
BG (1) BG110012A (en)
BR (1) BRPI0705314A2 (en)
CZ (1) CZ18174U1 (en)
HU (2) HUP0700772A2 (en)
PL (2) PL67322Y1 (en)
UA (1) UA39989U (en)
WO (1) WO2009046683A1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4509238A (en) * 1983-03-21 1985-04-09 General Electric Company Method for fabricating a steam turbine diaphragm
US5474419A (en) * 1992-12-30 1995-12-12 Reluzco; George Flowpath assembly for a turbine diaphragm and methods of manufacture
US5807074A (en) * 1995-02-03 1998-09-15 General Electric Co. Turbine nozzle diaphragm joint

Also Published As

Publication number Publication date
WO2009046683A1 (en) 2009-04-16
BRPI0705314A2 (en) 2009-06-23
PL383961A1 (en) 2009-04-14
HU4132U (en) 2012-07-30
CN101408113A (en) 2009-04-15
HU0700772D0 (en) 2008-01-28
CZ18174U1 (en) 2008-01-07
HUP0700772A2 (en) 2009-12-28
UA39989U (en) 2009-03-25
PL67322Y1 (en) 2014-08-29
PL120565U1 (en) 2012-06-04

Similar Documents

Publication Publication Date Title
CL2018003343A1 (en) Uracilpyridines herbicides.
EP2706241A3 (en) Fan blade
EP1780379A3 (en) Steam turbine and hydrophilic coating material used therefor
AR077191A1 (en) HERBICIDE BENZOXAZINONAS
EP2514925A3 (en) Ceramic matrix composite shroud attachment system
IN2012DE00184A (en)
FR2975123B1 (en) ROTOR OF TURBOMACHINE COMPRISING AUBES IN COMPOSITE MATERIAL WITH REPORTED HEEL
EP2749739A3 (en) Axial compressor and operation method of the same
UY36846A (en) USE OF ANNEXINE TO IMPROVE PERFORMANCE IN STRESS CONDITIONS IN PLANTS
EP2762724A3 (en) Ultrasonic sound emitting devices for wind turbines
SA515360112B1 (en) Rotor for an axial flow turbomachine and double nut for connecting two tie-rod elements
BR112021006279A2 (en) pongamy compositions, methods of preparation and analysis thereof and their uses
EP2239424A3 (en) Thermal control system for turbines
WO2017007809A3 (en) Motive air conditioning system for gas turbines
RU2012112418A (en) TURBINE INSTALLATION ROTOR, COMPRESSOR OR TURBINE FOR TURBINE INSTALLATION AND METHOD OF ROTOR MODERNIZATION
RU2013102781A (en) TURBO MACHINE, DOMESTIC BANDAGE FOR TURBO MACHINE AND GUIDE GROUP
EP2514975A3 (en) Flow engine
BG110012A (en) Intermediate distribution ring
EP2672062A3 (en) Nozzle diaphragm inducer
CL2012002925A1 (en) Suspension concentrate comprising agrochemical active substance, oil, emulsifier and at least one triglycerides; use of the suspension concentrate to improve the deposition rate of agrochemical active substances on plants.
MY202003A (en) A rotor for an electricity generator
CL2018000885A1 (en) Management of ethylene in plants through the use of a synergistic agricultural formula comprising diacilo or diarylurea and at least one metal complex.
EP2672068A3 (en) Turbine rotor and blade assembly with multi-piece locking blade
EA201790826A1 (en) HYDRODYNAMIC DROP
RU2012132944A (en) TURBINE SHOVEL AND TURBINE (OPTIONS)