FIELD: machine building.
SUBSTANCE: group of inventions relates to machine building. Bowl (35) intended for oil supply of at least two oil distribution circuits (43–44, 45–45a–45b), connected to carrier (13) of reduction gear (10) with epicycloidal transmission, wherein said carrier (13) rotates and oil is supplied from stationary oil spraying device (33), is made with possibility of connection with said carrier (13) and has a substantially cylindrical shape, being open radially inward relative to axis (X). Bowl is divided into circumferential sequence of separate chambers (37a, 37b) made with possibility to communicate with one of said oil distribution contours (43–44, 45–45a–45b). Objects of invention are reduction gear with its oil supply device and method of oil supply to reduction gear.
EFFECT: higher quality of lubrication, as well as higher reliability of bowl and reduction gear with its feeder.
9 cl, 7 dwg
| Title |
Year |
Author |
Number |
| CYCLOIDAL REDUCER, FAN MODULE OF DUAL-FLOW TURBOJET ENGINE AND DUAL-FLOW TURBOJET ENGINE |
2013 |
- Galle Fransua
- Briante Boris
- Serej Zhan-Per
- Tan-Kim Aleksandr
|
RU2627990C2 |
| OIL-DISTRIBUTING RING DIVIDED BY PARTITION IN AXIAL DIRECTION, AND PLANETARY REDUCTION GEAR CONTAINING SUCH RING |
2017 |
- Gedin Patrice
- Autran Pauline Marie Cecille
- Bruot Cecile
- Beck Guillaume Julien
- Dombek Alexis
- Lemoine Julie
- Peltier Jordane
|
RU2731149C2 |
| TRANSMISSION ASSEMBLY INCLUDING TRANSMISSION MEMBER AND OIL DISTRIBUTION SYSTEM |
2015 |
- Kyurle Ogusten
- Krid Yassin
|
RU2681824C2 |
| EPICYCLIC REDUCTION GEAR WITH FLUID TRANSFER PIPES, AND PROPELLER TURBOMACHINE FOR AIRCRAFT WITH SUCH REDUCTION GEAR |
2014 |
- Kyurlie Ogyusten
- Budebiza Tevfik
- Share Zhill Alen
|
RU2653671C2 |
| REDUCTION GEAR WITH EPICYCLOID TRANSMISSION FOR GAS TURBINE ENGINE |
2016 |
- Lao, Jeremy, Phorla
- Belmonte, Olivier
- Mouton, Clementine, Charlotte, Marie
- Nguyen Van, Thomas, Julien
- Patsouris, Emmanuel, Pierre, Dimitri
|
RU2704516C2 |
| SELF-CENTERING PLAIN BEARING |
2015 |
|
RU2701288C2 |
| DEVICE FOR TRANSFERRING OIL BETWEEN TWO COORDINATE SYSTEMS ROTATING RELATIVE TO EACH OTHER AND PROPELLER TURBOMACHINE FOR AIRCRAFT WITH SUCH DEVICE |
2014 |
- Belmont Olive
- Lao Zheremi Forla
|
RU2665194C2 |
| FRONT PART OF AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE AND AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE |
2015 |
- Nowakowski, Nathalie
- Vincent, Thomas, Alain, Christian
|
RU2686248C2 |
| ROTATING ASSEMBLY CONTAINING TRANSMISSION MECHANISM AND OIL DISTRIBUTION SYSTEM |
2014 |
- Bro Mishel Zhilber Rolan
- Limarshan Kevin
|
RU2664086C2 |
| LUBING AND COOLING OF REDUCTION GEARBOX WITH EPICYCLOIDAL GEARING |
2010 |
- Got'E Zherar Filipp
- Morreal' Serzh Rene
|
RU2519305C2 |
