US 12,495,637 B2
Jig for laminating solar cell module
Kwang Young Song, Eumseong-gun (KR); and Ju Hyun Ra, Eumseong-gun (KR)
Assigned to HANWHA SOLUTIONS CORPORATION, Seoul (KR)
Appl. No. 18/254,192
Filed by HANWHA SOLUTIONS CORPORATION, Seoul (KR)
PCT Filed Nov. 26, 2021, PCT No. PCT/KR2021/017611
§ 371(c)(1), (2) Date May 24, 2023,
PCT Pub. No. WO2022/119244, PCT Pub. Date Jun. 9, 2022.
Claims priority of application No. 10-2020-0167123 (KR), filed on Dec. 3, 2020.
Prior Publication US 2023/0411550 A1, Dec. 21, 2023
Int. Cl. H10F 71/00 (2025.01)
CPC H10F 71/00 (2025.01) 10 Claims
OG exemplary drawing
 
1. A jig for laminating a solar cell module, the jig comprising:
a first body including a first upper surface and a first side surface adjacent to the first upper surface and having at least a partial area configured to come in contact with one side surface forming a corner of the solar cell module;
a second body including a second upper surface and a second side surface adjacent to the second upper surface and having at least a partial area configured to come in contact with another side surface forming the corner; and
a fixer disposed in a first groove of the first upper surface and a second groove of the second upper surface and disposed across the first body and the second body to fix the solar cell module,
wherein the first side surface includes a plurality of first protrusions each protruding toward said one side surface of the solar cell module and having a first contact surface that contacts said one side surface, the plurality of first protrusions being disposed to be spaced apart in a longitudinal direction of the first body; and
wherein the second side surface includes a plurality of second protrusions each protruding toward said another side surface of the solar cell module and having a second contact surface that contacts said another side surface, the plurality of second protrusions being disposed to be spaced apart in a longitudinal direction of the second body; and
wherein a length of the first body and a length of the second body are less than ½ of a length of the solar cell module.