FIELD: control of flying vehicle boundary layer.
SUBSTANCE: proposed device has layer of active material located on outer skin of flying vehicle and intended for generation of mechanical vibrations. Novelty of invention consists in availability of current-conducting film applied over layer of piezo-active material by spraying or painting. Piezo-active material is applied on surface of outer metal skin of flying vehicle. Located on surface of current-conducting film are sensors of parameters of turbulent motions of flow whose signals are used for control of mechanical vibrations of piezo-active material in phase or in anti-phase relative to vibrations in boundary layer. Layer of piezo-active material may be made from piezo-ceramics. Layer of piezo-active material may be polarized at angle 135 deg. for compensation for turbulence and at angle of 45 deg. for reduction of effect of break-down of flow.
EFFECT: enhanced economical efficiency.
3 cl
Title | Year | Author | Number |
---|---|---|---|
PERFORATED STRUCTURE OF AIRCRAFT SKIN WITH COMBINED OPENINGS AND DAMPING CAVITY | 2017 |
|
RU2656918C1 |
PERFORATED OUTER SURFACE OF ROTATION BODY WITH COMBINED HOLES AND SUCTION CHANNEL | 2020 |
|
RU2734664C1 |
FRICTION REDUCTION METHOD FOR AXISYMMETRIC BODY AND RELATED DEVICE | 2007 |
|
RU2357893C1 |
0 |
|
SU1782220A3 | |
METHOD FOR BOUNDARY LAYER CONTROL AT AIRCRAFT SURFACE AND DEVICE FOR ITS IMPLEMENTATION | 2008 |
|
RU2384465C1 |
AIRCRAFT WING | 1986 |
|
SU1840803A1 |
AUTONOMOUS SURVEY FLYING VEHICLE FOR REMOTE OBSERVATION OF TERRAIN | 1998 |
|
RU2159199C2 |
HYPERSONIC FLYING VEHICLE | 1999 |
|
RU2172278C2 |
DEVICE FOR MEASURING FLOW TURBULENCE | 0 |
|
SU1383142A1 |
METHOD FOR TANGENTIAL BLOWING OF AIRCRAFT SURFACE AND DEVICE FOR ITS IMPLEMENTATION | 2020 |
|
RU2748709C1 |
Authors
Dates
2005-01-10—Published
2002-12-11—Filed