FIELD: physics.
SUBSTANCE: bench for modeling the aerodynamic load on the aircraft elements contains a base, on which the opening actuator is rigidly fixed with the opening elements equipped with a loading drive. The opening actuator is in the form of an opening hydraulic cylinder that interacts with the dynamometer through the pusher, which drives the opening actuator, which controls the opening elements. The loading drive is made in the form of pneumatic cylinders installed in the aerodynamic center of each of the opening elements, the rods of which are provided with the wheel supports supported on the base and directing a constant force along the whole path of the opening elements.
EFFECT: increasing the accuracy of modeling the impact of aerodynamic loading by applying a load with a constant direction relative to the aerodynamic surface of the opening element, regardless of the opening element bending caused by the action of the aerodynamic load.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
STAND FOR MODELLING IMPACT OF AERODYNAMIC LOAD ON OPENING ELEMENTS OF AIRCRAFTS | 2014 |
|
RU2559396C1 |
BENCH FOR SIMULATING THE EFFECT OF AERODYNAMIC LOAD ON THE EXPANDABLE ELEMENTS OF AIRCRAFT | 2017 |
|
RU2657159C1 |
BENCH TO TEST AIRCRAFT HATCH | 2010 |
|
RU2444715C1 |
DEVICE FOR SIMULATING THE LOAD OF DRIVES FOR DEPLOYING TRANSFORMABLE SPACECRAFT STRUCTURES | 2023 |
|
RU2801954C1 |
MODELING COMPLEX FOR DEBUGGING CONTROL SYSTEM OF AUTONOMOUS MOBILE UNIT | 2017 |
|
RU2662331C1 |
METHOD OF CONTROLLING DRIVING TORQUE MARGIN IN HINGE DEVICES OF LARGE-SIZE MECHANICAL SYSTEMS OF SPACECRAFT ABOVE MOMENTS RESISTANCE | 2014 |
|
RU2586445C1 |
LOAD STAND FOR TESTING STEERING GEARS OF AIRCRAFT AERODYNAMIC SURFACES | 2023 |
|
RU2798624C1 |
STAND FOR TESTING THE DESIGN OF THE FLYING MACHINE FOR MECHANICAL STRENGTH UNDER THE ACTION OF THE BENDING MOMENT | 2016 |
|
RU2643234C1 |
ELECTROMECHANICAL BENCH | 2020 |
|
RU2736347C1 |
CONTROL METHOD OF AIRCRAFT AERODYNAMIC MODEL STEERING SURFACES | 2019 |
|
RU2731425C1 |
Authors
Dates
2017-10-11—Published
2016-05-10—Filed