FIELD: measurement equipment.
SUBSTANCE: invention relates to experimental equipment for detection of rotary productive aerodynamic forces and moments of the model in an aerodynamic pipe, also near a screen. The bench comprises a model with a strain-gage weigher, installed on the stand with a stem, and a mechanism of its movements. It also comprises an energy drive in the form of a linear electric motor with an extended traction rod, by means of a lever and a double-link mechanism with a leash, which is kinematically connected by the second link in its turn to a model. Arrangement of the kinematic joint of the second link of the double-link mechanism in the form of a bracket installed on the stem or in the form of a slider with brackets provides for oscillations of the model by height and at angles of pitch or list. Equipment of the bench with a screen moving in guides with a slot for a stand with a stem provides for tests near the screen.
EFFECT: expansion of bench capabilities in production of rotary productive forces and moments.
8 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
STAND FOR DERIVATIVE ROTATION AERODYNAMIC FORCE AND MOMENT DETERMINATION FOR MODEL IN WIND TUNNEL | 2012 |
|
RU2522794C1 |
STAND FOR DETERMINING AERODYNAMIC CHARACTERISTICS OF MODEL IN PRESENCE OF FIXED SCREEN | 2014 |
|
RU2574326C1 |
WING-IN-GROUND EFFECT CRAFT, ITS TAKE-OFF AND LANDING GEAR AND WING FOLDING ACTUATOR | 1995 |
|
RU2099217C1 |
STRAIN GAUGE AERODYNAMIC WEIGHING APPARATUS | 0 |
|
SU566141A1 |
STAND FOR MEASURING AERODYNAMIC FORCES AND MOMENTS | 2021 |
|
RU2781860C1 |
SUMMING MECHANISM FOR CONTROL SYSTEMS OF COMMON AND CYCLIC PITCH OF HELICOPTERS OF THREE-POINT CONTROL SYSTEM WITH INCLINED ARRANGEMENT OF HYDRAULIC ACTUATORS | 2014 |
|
RU2578706C1 |
METHOD OF DEFINING FACTORS OF AERODYNAMIC FORCES AND MOMENTS AT STEADY-STATE ROTATION OF AIRCRAFT MODEL AND DEVICE TO THIS END | 2011 |
|
RU2477460C1 |
METHOD OF DETERMINING AERODYNAMIC DAMPING CHARACTERISTICS OF PROPELLER AEROPLANES AND METHOD TO THIS END | 2009 |
|
RU2402005C1 |
METHOD OF DETERMINING ROTATION AND NON-STATIONARY DERIVATIVES OF COEFFICIENTS OF LINEAR AERODYNAMIC FORCES AND MOMENTS USING FORCED OSCILLATION METHOD AND DEVICE TO THIS END | 2007 |
|
RU2358254C1 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2012 |
|
RU2518143C2 |
Authors
Dates
2014-05-10—Published
2012-10-11—Filed