SU642520A1 - Centrifugal turbomachine diffuser - Google Patents

Centrifugal turbomachine diffuser

Info

Publication number
SU642520A1
SU642520A1 SU762435114A SU2435114A SU642520A1 SU 642520 A1 SU642520 A1 SU 642520A1 SU 762435114 A SU762435114 A SU 762435114A SU 2435114 A SU2435114 A SU 2435114A SU 642520 A1 SU642520 A1 SU 642520A1
Authority
SU
USSR - Soviet Union
Prior art keywords
centrifugal turbomachine
turbomachine diffuser
diffuser
centrifugal
blades
Prior art date
Application number
SU762435114A
Other languages
Russian (ru)
Inventor
Игорь Константинович Попов
Original Assignee
Popov Igor K
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 Popov Igor K filed Critical Popov Igor K
Priority to SU762435114A priority Critical patent/SU642520A1/en
Application granted granted Critical
Publication of SU642520A1 publication Critical patent/SU642520A1/en

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

ду ними концентричными венцами лопаток, Отличающийс  тем, что, с целью повышени  КПД, лопатки выполнены с шириной, увеличивающейс  от венца к венцу по ходу рабочего нотокз, а внутренние стенки дисков между венцами образуют диффузорные каналы.They have concentric rims of blades, characterized in that, in order to increase efficiency, the blades are made with a width that increases from the rim to the rim along the working path, and the inner walls of the disks between the rims form diffuser channels.

Источники иифорл ацин, прин тые во йн.имание при экспертизе:Sources of iforll, taken in the name of the examination:

1.Стечкин Б. С. Теори  реактивных двнS гателей. М., «Оборонгиз, 1956, с. 103.1.Stechkin B.S. Theory of reactive twin gels. M., “Oborongiz, 1956, p. 103

2.Патент Франции № 2015956, кл. F 04 D 29/00, 1969.2. The patent of France No. 2015956, cl. F 04 D 29/00, 1969.

SU762435114A 1976-12-27 1976-12-27 Centrifugal turbomachine diffuser SU642520A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU762435114A SU642520A1 (en) 1976-12-27 1976-12-27 Centrifugal turbomachine diffuser

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU762435114A SU642520A1 (en) 1976-12-27 1976-12-27 Centrifugal turbomachine diffuser

Publications (1)

Publication Number Publication Date
SU642520A1 true SU642520A1 (en) 1979-01-15

Family

ID=20688645

Family Applications (1)

Application Number Title Priority Date Filing Date
SU762435114A SU642520A1 (en) 1976-12-27 1976-12-27 Centrifugal turbomachine diffuser

Country Status (1)

Country Link
SU (1) SU642520A1 (en)

Similar Documents

Publication Publication Date Title
GB751011A (en) Improvements in or relating to the cooling of turbine blades
GB1357713A (en) Cooled rotor blades for gas turbines
GB1484703A (en) Turbine with internally cooled rim and predetermined rupture regions
GB705387A (en) Improvements relating to radial-flow turbine or centrifugal compressors
GB1340937A (en) Turbomachinery rotors
SE391965B (en) VARIABLE VENTING OPENING FOR A COMPRESSOR SECTION IN A TURBINE TYPE POWER PLANT
GB1053420A (en)
GB1458524A (en) Turbine rotor discs
SU642520A1 (en) Centrifugal turbomachine diffuser
GB1515296A (en) Rotor for centrifugal compressor or centripetal turbine
SE7709108L (en) BLOWER WHEELS FOR RADIAL TYPE GAS TURBINES
GB1148339A (en) Compressors or turbines for gas turbine engines
GB1302661A (en)
GB848465A (en) Rotors of multi-stage axial flow compressors or turbines
GB2010404A (en) Cooling Turbine Rotor Blades
GB1107120A (en) Improvements relating to turbo-machine rotors
GB1527074A (en) Bladed rotors
SU591605A1 (en) Hydraulic turbine runner
JPS5317802A (en) Turbine rotor blade wheel disc
FR2279926A1 (en) TURBOMACHINE, ESPECIALLY STEAM TURBINE WITH HIGH STEAM INLET TEMPERATURE
FR2375440A1 (en) Rotor of axial flow steam turbine - has shroud ring round blade tips with slots to give tangential elasticity
SU779617A1 (en) Radial-axial hydraulic machine impeller
SU1384834A1 (en) Centriugal fan impeller
SU480362A1 (en) Upright rotor
SU723228A1 (en) Centrifugal fan impeller