RU100134U8 - TURBINE SHOVEL - Google Patents

TURBINE SHOVEL Download PDF

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Publication number
RU100134U8
RU100134U8 RU2010124165/06U RU2010124165U RU100134U8 RU 100134 U8 RU100134 U8 RU 100134U8 RU 2010124165/06 U RU2010124165/06 U RU 2010124165/06U RU 2010124165 U RU2010124165 U RU 2010124165U RU 100134 U8 RU100134 U8 RU 100134U8
Authority
RU
Russia
Prior art keywords
turbine
blade
flange
turbine shovel
cooling channels
Prior art date
Application number
RU2010124165/06U
Other languages
Russian (ru)
Other versions
RU100134U1 (en
Inventor
Юрий Михайлович Бурматнов
Станислав Мечиславович Пиотух
Андрей Николаевич Поткин
Original Assignee
Открытое акционерное общество "Научно-производственное объединение "Сатурн"
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 Открытое акционерное общество "Научно-производственное объединение "Сатурн" filed Critical Открытое акционерное общество "Научно-производственное объединение "Сатурн"
Priority to RU2010124165/06U priority Critical patent/RU100134U8/en
Application granted granted Critical
Publication of RU100134U1 publication Critical patent/RU100134U1/en
Publication of RU100134U8 publication Critical patent/RU100134U8/en

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Abstract

1. Лопатка турбины, содержащая перо, включающее корыто, спинку и торец, на котором со стороны спинки выполнена реборда, при этом в лопатке выполнены охлаждающие каналы, выходы которых расположены на торце, и их оси наклонены в сторону реборды, отличающаяся тем, что оси соседних каналов пересекаются. ! 2. Лопатка турбины по п.1, отличающаяся тем, что охлаждающие каналы расположены парами. 1. The blade of the turbine containing a feather, including a trough, back and end, on which the flange is made from the back side, while the cooling channels are made in the blade, the outlets of which are located at the end, and their axes are inclined towards the flange, characterized in that the axis adjacent channels intersect. ! 2. The turbine blade according to claim 1, characterized in that the cooling channels are arranged in pairs.

RU2010124165/06U 2010-06-11 2010-06-11 TURBINE SHOVEL RU100134U8 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2010124165/06U RU100134U8 (en) 2010-06-11 2010-06-11 TURBINE SHOVEL

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2010124165/06U RU100134U8 (en) 2010-06-11 2010-06-11 TURBINE SHOVEL

Publications (2)

Publication Number Publication Date
RU100134U1 RU100134U1 (en) 2010-12-10
RU100134U8 true RU100134U8 (en) 2011-03-10

Family

ID=46306830

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010124165/06U RU100134U8 (en) 2010-06-11 2010-06-11 TURBINE SHOVEL

Country Status (1)

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RU (1) RU100134U8 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU177804U1 (en) * 2017-10-20 2018-03-13 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Cooled hollow turbine blade

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU177804U1 (en) * 2017-10-20 2018-03-13 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Cooled hollow turbine blade

Also Published As

Publication number Publication date
RU100134U1 (en) 2010-12-10

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Legal Events

Date Code Title Description
TH1K Reissue of utility model (1st page)