Method to test a power system and an avionics equipment of an unmanned aerial vehicle (uav)

Abstract

A method to test a power system and an avionics equipment of an unmanned aerial vehicle (UVA) including providing a support component, a power system load-bearing component, an avionics equipment load-bearing component, a jacking component and a roller component. The method further includes providing a plurality of power system load-bearing components that 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 . A method to test a power system and an avionics equipment for an unmanned aerial vehicle (UAV), said method comprising:
 providing a support component ( 1 );   providing 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 the power system;   providing 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 the power system;   providing an avionics equipment load-bearing component ( 3 ), which is fixedly arranged on the support component ( 1 ), and is configured to bear the avionics equipment;   providing a jacking component ( 4 ), the output end of which is fixedly connected to a bottom end of the support component ( 1 ); and   providing a roller component (5), which includes a roller stand ( 51 ) and a guide wheel (52) which is connected to the roller stand (51), which is fixedly connected to the jacking component (4).   
     
     
         2 . The method to test a power system and an avionics equipment for an unmanned aerial vehicle as recited in  claim 1 , wherein 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 method to test a power system and an avionics equipment for an unmanned aerial vehicle as recited in  claim 2 , further providing a mounting hole ( 221 ) on the fixing seat ( 22 ). 
     
     
         4 . The method to test a power system and an avionics equipment for an unmanned aerial vehicle as recited in  claim 1 , wherein 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 method to test a power system and an avionics equipment for an unmanned aerial vehicle as recited in  claim 4 , wherein 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 method to test a power system and an avionics equipment for an unmanned aerial vehicle as recited in  claim 5 , wherein the outer frame also comprises a beam ( 14 ), a first end and a second end of said beam ( 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 method to test a power system and an avionics equipment for an unmanned aerial vehicle as recited in  claim 5 , wherein the outer frame further 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 method to test a power system and an avionics equipment for an unmanned aerial vehicle as recited in  claim 7 , wherein 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 method to test a power system and an avionics equipment for an unmanned aerial vehicle as recited in  claim 1 , wherein the avionics equipment load-bearing assembly ( 3 ) has a plurality of wire holes ( 31 ). 
     
     
         10 . The method to test a power system and an avionics equipment for an unmanned aerial vehicle as recited in  claim 1 , wherein the jacking component ( 4 ) comprises a trailer jack.