FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to devices for starting an aircraft engine and aircraft onboard power supply. Integrated starter-generator of the gas turbine engine includes a stator, a rotor connected to the output shaft of the gas turbine engine, a cooling system with cooling air supply and removal channels. Integrated starter-generator is made modular and comprises a housing in which a stator with a winding and a sealed cylindrical insert is fixed, rotor with permanent magnets pressed to it by bandage, fixed on hub by means of coupling, and installed with possibility of rotation relative to stator in front and rear end shields attached to housing. At the same time the rear end shield is made in the form of a flange, and the cooling system is combined with air and liquid coolant supply and discharge channels.
EFFECT: improving reliability, energy efficiency and simplifying maintenance.
1 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
ELECTRIC DRIVE FOR GAS TURBINE PLANT START-UP | 2018 |
|
RU2694107C1 |
ATOMIC SUBMARINE AND MARINE-VERSION GAS TURBINE ENGINE | 2011 |
|
RU2481233C1 |
GAS-TURBINE ENGINE | 2003 |
|
RU2252316C2 |
TURBINE GENERATOR | 2023 |
|
RU2821119C1 |
GAS TURBINE ENGINE | 2008 |
|
RU2382210C1 |
GAS TURBINE ENGINE | 2008 |
|
RU2382209C1 |
GAS TURBINE ENGINE | 2008 |
|
RU2382208C1 |
HELICAL FAN AVIATION ENGINE | 2007 |
|
RU2358119C1 |
SMALL-SIZE GAS TURBINE ENGINE | 2018 |
|
RU2727655C2 |
TURBOPROP GAS TURBINE ENGINE | 2007 |
|
RU2359131C1 |
Authors
Dates
2024-07-25—Published
2024-03-01—Filed