Experimental bench for a UAV power system and avionics equipment
An experimental bench for an unmanned aerial vehicle (UAV) power system and avionics equipment, which relates to the technical field of UAV test, comprising a support component, a power system load-bearing component, an avionics equipment load-bearing component, a jacking component and a roller component. A plurality of power system load-bearing components are provided, and are fixedly arranged on the support components, respectively, and each power system load-bearing component is configured to carry the power system of a UAV; the avionics equipment load-bearing component is fixedly arranged on the support component, and the avionics equipment load-bearing component is configured to bear the avionics equipment of the UAV; the output end of the jacking component is fixedly connected to the bottom end of the support component.
1. An experimental bench for a UAV (unmanned aerial vehicle) power system and avionics equipment, which is characterized in that, comprising:
a support component ( 1 );
a first plurality of power system load-bearing components ( 2 ), which are provided, and are fixedly arranged on the support component ( 1 ) in a linear fashion from a top view, respectively, and each of which is configured to bear a UAV power system;
a second plurality of power system load-bearing components ( 2 ), which are provided, and are fixedly arranged on the support component ( 1 ) in a linear fashion from a top view parallel to the first plurality of power system loan-bearing components, and each of which is configured to bear a UAV power system;
avionics equipment load-bearing component ( 3 ), which is fixedly arranged on the support component ( 1 ), and is configured to bear the UAV avionics equipment;
a jacking component ( 4 ), the output end of which is fixedly connected to the bottom end of the support component ( 1 ); and
a roller component ( 5 ), comprising a roller stand ( 51 ) and a guide wheel ( 52 ) connected to the roller stand ( 51 ), which is fixedly connected to the jacking component ( 4 ).
2. The experimental bench for a UAV power system and avionics equipment according to claim 1 , which is characterized in that the power system load-bearing component ( 2 ) comprises a mounting plate ( 21 ), a fixing seat ( 22 ) and a connector ( 23 ), and the mounting plate ( 21 ) is fixedly connected to the support component ( 1 ), and the fixing seat ( 22 ) and the mounting plate is spaced and connected to the mounting plate ( 21 ) through the connector ( 23 ).
3. The experimental bench for a UAV power system and avionics equipment according to claim 2 , which is characterized in that the fixing seat ( 22 ) has a mounting hole ( 221 ).
4. The experimental bench for a UAV power system and avionics equipment according to claim 1 , which is characterized in that the support component ( 1 ) comprises an outer frame and a cross frame ( 11 ) connected in the outer frame, wherein the first and second pluralities of the power system load-bearing component ( 2 ) are fixedly arranged on the outer frame, respectively, the avionics equipment load-bearing component ( 3 ) is fixedly connected at the intersection of the cross frame ( 11 ), and the output end of the jacking component ( 4 ) is fixedly connected to the outer frame.
5. The experimental bench for a UAV power system and avionics equipment according to claim 4 , which is characterized in that the outer frame comprises two oppositely arranged X-direction frames ( 12 ) and oppositely arranged Y-direction frame ( 13 ) connected between the two X-direction frames ( 12 ), and the cross frame ( 11 ) is connected to the two X-direction frames ( 12 ) and the two Y-direction frames ( 13 ), respectively, and each X-direction frame ( 12 ) is spaced with two power system load-bearing components ( 2 ).
6. The experimental bench for a UAV power system and avionics equipment according to claim 5 , which is characterized in that the outer frame also comprises a beam ( 14 ), the two ends of which ( 14 ) are connected to the two X-direction frames ( 12 ) and is fixedly connected to one of the power system load-bearing component ( 2 ), respectively.
7. The experimental bench for a UAV power system and avionics equipment according to claim 5 , which is characterized in that the outer frame also comprises two side brackets ( 15 ), the two side brackets ( 15 ) correspond to the two Y-direction frames ( 13 ), and the side brackets ( 15 ) include an mounting rod ( 151 ) and two first inclined rods ( 152 ), one end of the two first inclined rods ( 152 ) is fixedly connected to the corresponding Y-direction frame ( 13 ), respectively, the other end of the two first inclined rods ( 152 ) is fixedly connected to the mounting rod ( 151 ), respectively, and the mounting rod ( 151 ) is fixedly connected with a power system load-bearing component ( 2 ).
8. The experimental bench for a UAV power system and avionics equipment according to claim 7 , which is characterized in that the Y-direction frame ( 13 ) comprises two first connecting rods ( 131 ) arranged at intervals, the side brackets ( 15 ) also comprise a second inclined rod ( 153 ), and one end of the two first inclined rods ( 152 ) is fixed to one of the first connecting rods ( 131 ) of the corresponding Y-direction frame ( 13 ), respectively, one end of the second inclined rod ( 153 ) is fixedly connected to the other first connecting rod ( 131 ) of the corresponding Y-direction frame ( 13 ), and the other end of the second inclined rod ( 153 ) is fixedly connected to the mounting rod ( 151 ).
9. The experimental bench for a UAV power system and avionics equipment according to claim 1 , which is characterized in that the avionics equipment load-bearing assembly ( 3 ) has a plurality of wire holes ( 31 ).
10. The experimental bench for a UAV power system and avionics equipment according to claim 1 , which is characterized in that the jacking component ( 4 ) comprises a trailer jack.