FIELD: aeronautical engineering. SUBSTANCE: box has housing 1 and silencer 4 and is provided with device for sucking the boundary layer made in form of passage 7 with ejector 8 whose free end holds wing 9. Passage 7 is brought in communication with interior of housing 1 through perforated panel 10. In the course of operation when jet of exhaust gases moves upward, suction hole of ejector 8 moves towards core of jet due to lifting force of wing, thus providing for reliable operation of ejector and suction of boundary layer. EFFECT: enhanced reliability of trying-out the engines and enhanced efficiency at idling.
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT JET ENGINE TEST BOX | 1987 |
|
SU1434694A1 |
0 |
|
SU1784530A1 | |
0 |
|
SU1784531A1 | |
SURFACE PROTECTIVE DEVICE FOR PROTECTION OF PASSAGE OF AIR-JET ENGINE AGAINST FOREIGN MATTER | 1989 |
|
RU1669140C |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT - DISK-TYPE FLYING VEHICLE | 1999 |
|
RU2174484C2 |
TESTING INSTALLATION | 1991 |
|
RU2049939C1 |
DEVICE FOR SUCTION OF BOUNDARY LAYER AND FOR MONITORING OF SHOCK BOUNDARY LAYER FOR AIRCRAFT | 1999 |
|
RU2168445C2 |
PLANAR NOZZLE WITH CENTRAL BODY | 1995 |
|
RU2153591C2 |
TRANSPORT AIRCRAFT WITH BLUNTED TAIL SECTION OF FUSELAGE | 1994 |
|
RU2094307C1 |
METHOD OF CONDUCTING AERODYNAMIC TESTS ON MODEL AIRCRAFT AND STAND FOR REALISING SAID METHOD | 2009 |
|
RU2421701C1 |
Authors
Dates
1995-03-10—Published
1991-12-27—Filed