SU1434854A2 - Cooled blade of gas turbine - Google Patents
Cooled blade of gas turbine Download PDFInfo
- Publication number
- SU1434854A2 SU1434854A2 SU864167276A SU4167276A SU1434854A2 SU 1434854 A2 SU1434854 A2 SU 1434854A2 SU 864167276 A SU864167276 A SU 864167276A SU 4167276 A SU4167276 A SU 4167276A SU 1434854 A2 SU1434854 A2 SU 1434854A2
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- shell
- deflector
- cavity
- gas turbine
- cooled blade
- Prior art date
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Изобретение м.б, использовано ,;в авиациОниых двигател х Цель изобретени - упрощение изготовлени лопатки . Лопатка содержит полую оболочку 1 и установленный в ее полости 2 дефлектор 3. Торец А дефлектора консольно закреплен в оболочке 1«Оболочка 1 снабжена бобыйкой 5, образующей с. ее внутренней поверхностью профильную щель, торец 8 дефлектора размещен в этой щели. Бобышка 5 со стороны полости 2 снабжена поперечны- ш пазами 9, Воздух поступает в дефлектор 3, перетекает в полость 2 и проходит ме /ду дефлр.ктором внутренней поверхностью оболочки 1, охлажда оболочку. 2 ил.Invention mb, used,; in aircraft engines. The purpose of the invention is to simplify the manufacture of a blade. The paddle contains a hollow shell 1 and a deflector 3 installed in its cavity 2. The end face A of the deflector is cantilevered in the shell 1 “The shell 1 is provided with a leg 5, which forms c. its internal surface profile gap, the end face 8 of the deflector is placed in this gap. Lug 5 on the side of cavity 2 is provided with transverse slots 9, Air enters deflector 3, flows into cavity 2 and passes through the inner surface of shell 1 to the deflector of the shell 1, cooling the shell. 2 Il.
Description
1212
Фив.Thebes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU864167276A SU1434854A2 (en) | 1986-12-24 | 1986-12-24 | Cooled blade of gas turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU864167276A SU1434854A2 (en) | 1986-12-24 | 1986-12-24 | Cooled blade of gas turbine |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1261359A Addition SU278988A1 (en) | METHOD OF MANUFACTURING MULTILAYERED GLASS |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1434854A2 true SU1434854A2 (en) | 1991-06-23 |
Family
ID=21275124
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU864167276A SU1434854A2 (en) | 1986-12-24 | 1986-12-24 | Cooled blade of gas turbine |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1434854A2 (en) |
-
1986
- 1986-12-24 SU SU864167276A patent/SU1434854A2/en active
Non-Patent Citations (1)
Title |
---|
Авторское свидетельство СССР 1261359, кл. F 01 D 5/18, 1985. * |
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