FIELD: brush seals dividing two space of different pressures (P1, P2) between stator and rotor of turbo-machine. SUBSTANCE: contact members of brush seal have bent-aside sections whose ends are in contact with surface of rotor being sealed, thus simultaneously ensuring low rigidity of contact members and occupation of small area in radial direction. Provision is made for contact member holder which has stop at distance (a) from bent-aside sections and is located across direction of contact members. Distance is calculated on the condition of obtaining required springing of flexible contact members. EFFECT: enhanced reliability of seal. 5 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
AIR INTAKE FOR TURBO-JET AIRCRAFT ENGINE | 1991 |
|
RU2039880C1 |
POWER PLANT WITH AIRCREW OR PROPELLER (VERSIONS) | 1991 |
|
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|
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|
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PISTON INTERNAL COMBUSTION ENGINE WITH SUPERCHARGING | 1990 |
|
RU2011863C1 |
IMPROVEMENT OF ENGINE EXHAUST SYSTEM | 0 |
|
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EXHAUST PIPELINE OF MULTICYLINDER SUPERCHARGED PISTON I.C. ENGINE | 0 |
|
SU1618284A3 |
Authors
Dates
2000-11-10—Published
1997-03-26—Filed