FIELD: connection of housing of aircraft gas turbine engines. SUBSTANCE: during operation of engine, inertial forces and torque from mating portion of inner housing are transmitted to outer housing by means of projections with grooves of slide blocks and pins. Isolation of housings in axial and radial directions for compensation for thermal expansion and axial displacement is ensured due to absence of limitation in axial direction in joint of slot and slide block and due to radial clearance in radial direction. Inaccuracy in mounting the joint unit of housing is compensated for due to eccentric position of axes and radial pin and cylindrical journal by turning the pin in cylindrical radial bore followed by locking it by means of splined bush and bolts. EFFECT: reliable isolation of engine housings; facilitated assembly of housing. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
ADJUSTABLE INTAKE GUIDE VANE ASSEMBLY OF COMPRESSOR OF GAS TURBINE ENGINE | 2001 |
|
RU2199670C1 |
DEVICE FOR CONNECTING HOUSING OF GAS TURBINE ENGINE | 2001 |
|
RU2200849C2 |
PNEUMATIC CYLINDER OF GAS-TURBINE ENGINE PROPELLING NOZZLE ACTUATOR | 1997 |
|
RU2131988C1 |
SUPPORT ADJUSTING DEVICE FOR CONNECTION OF CASES OF DOUBLE-CIRCUIT GAS-TURBINE MOTOR | 2008 |
|
RU2399775C2 |
GUIDE-VANE ASSEMBLY OF AXIAL-FLOW COMPRESSOR | 2000 |
|
RU2184879C1 |
AFTERBURNER MIXER OF BYPASS OF BYPASS TURBO-JET ENGINE | 1995 |
|
RU2117805C1 |
DEVICE FOR CONNECTING MIXER WITH HOUSING OF OUTER CIRCUIT OF DOUBLE- FLOW GAS-TURBINE ENGINE | 2004 |
|
RU2263220C1 |
DEVICE FOR CONNECTING HOUSING OF GAS-TURBINE BYPASS ENGINE | 2004 |
|
RU2265743C1 |
GAS-TURBINE ENGINE ROTOR SUPPORT | 1991 |
|
RU2075658C1 |
MULTI-STAGE COMPRESSOR | 2001 |
|
RU2196925C1 |
Authors
Dates
1998-08-20—Published
1995-02-15—Filed