FIELD: engines and pumps.
SUBSTANCE: invention relates to elements of breathing system of aircraft gas turbine engine (GTE). Before support bearing is installed through radial hole in shaft lock in form of cylindrical pin so that protruding beyond side surface of shaft cylindrical sections of pin are located in front end of internal shoulder of support bearing fixed relative to body.
EFFECT: end sections of pin are hidden inside made in impeller at input of annular groove, ruling out ingress of destruction elements towards drive mechanism (drive box of propulsion units), which increases reliability of breather design.
1 cl, 2 dwg
Title |
Year |
Author |
Number |
GAS TURBINE ENGINE ROTARY BREATHER |
2015 |
- Golubov Aleksandr Nikolaevich
- Fomin Vyacheslav Nikolaevich
- Voznesenskij Viktor Aleksandrovich
|
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2013 |
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|
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1999 |
- Korolev O.G.
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|
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2016 |
- Marchukov Evgenij Yuvenalevich
- Bibaeva Anna Viktorovna
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- Simonov Sergej Anatolevich
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- Shishkova Olga Vladimirovna
|
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|
RU2786876C1 |
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2016 |
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- Polyakov Konstantin Sergeevich
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|
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|
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- Marchukov Evgenij Yuvenalevich
|
RU2614469C1 |
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|
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2016 |
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|
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