FIELD: physics.
SUBSTANCE: invention relates to the field of experimental aerodynamics and is intended for determining the aerodynamic characteristics of the model of aircraft, missiles, etc. in transonic wind tunnels. Device contains a holder, a crescent-shaped rack, a drive and a bed frame, the drive is made in the form of three linear cylinders, one end of which is hinged at three points on the bed frame, and the other at two points of the rack. In this case, the cylinders are oriented so as to ensure maximum rigidity of the mechanism and the least effort in the drive under the operating loads and movements of the model. In addition, two linear cylinders are located in the direction of air flow, and the third – perpendicular to the direction of air flow. Device further includes stops for moving the rack in a direction, which is perpendicular to its plane.
EFFECT: technical result consists in expanded experimental capabilities of the aerodynamic plant, in reduced labor intensity.
3 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR MODEL POSITION CHANGING IN WORKING PART OF WIND TUNNEL | 2016 |
|
RU2629696C1 |
| METHOD FOR CONTROLLING THE POSITION OF A MODEL IN A WIND TUNNEL | 2017 |
|
RU2660225C1 |
| GEAR FOR ANGULAR AND LINEAR MOVEMENT OF MODEL OF AIRCRAFT IN WIND TUNNEL | 1994 |
|
RU2102714C1 |
| DEVICE FOR CHANGING POSITION OF MODEL IN WORKING PART OF AERODYNAMIC PIPE | 2019 |
|
RU2708681C1 |
| DEVICE FOR TERMINATION OF UNCONTROLLED MOTION OF AIRCRAFT MODEL AT ITS DYNAMIC TESTS FOR STABILITY AND CONTROLLABILITY | 2015 |
|
RU2612848C9 |
| DEVICE FOR CHANGING POSITION OF MODEL IN WORKING PART OF AERODYNAMIC PIPE | 2018 |
|
RU2690097C1 |
| DEVICE FOR ANALYSIS OF NON-STATIONARY AERODYNAMIC CHARACTERISTICS OF MODEL IN WIND TUNNEL | 2019 |
|
RU2717748C1 |
| METHOD OF CONTROLLING MODEL POSITION IN WIND TUNNEL | 2019 |
|
RU2722854C1 |
| DEVICE FOR CHANGING POSITION OF MODEL IN WORKING PART OF AERODYNAMIC PIPE | 2019 |
|
RU2708680C1 |
| 0 |
|
SU1779969A1 |
