公开(公告)号：US20240270477A1

公开(公告)日：2024-08-15

申请号：US18647197

申请日：2024-04-26

申请人： ADCO Products, LLC

发明人： Justin Bates ,  Yuwei Liu ,  David W. Carnahan

IPC分类号： B65D83/14 ,  B65D83/44 ,  B65D83/68

CPC分类号： B65D83/752 ,  B65D83/682 ,  B65D83/44

摘要： A substance dispensing system including a first pressure vessel defining a first interior space; a first substance positioned in the first interior space; a first portion of a first propellant positioned in the first interior space; and a first portion of a second propellant positioned in the first interior space. At least 90 percent by weight of the first propellant is at least one of carbon dioxide, nitrous oxide, and combinations thereof. At least 90 percent by weight of the second propellant is at least one of nitrogen, argon, helium, oxygen, and combinations thereof.

公开(公告)号：US20230150752A1

公开(公告)日：2023-05-18

申请号：US18047881

申请日：2022-10-19

申请人： Royal Adhesives and Sealants, LLC ,  ADCO Products, LLC

发明人： David W. Carnahan ,  Yuwei Liu ,  Justin Bates

IPC分类号： B65D83/14 ,  B65D83/68

CPC分类号： B65D83/752 ,  B65D83/682 ,  B65D83/44

摘要： A substance dispensing system including a first pressure vessel defining a first interior space; a first substance positioned in the first interior space; a first portion of a first propellant positioned in the first interior space; and a first portion of a second propellant positioned in the first interior space. At least 90 percent by weight of the first propellant is at least one of carbon dioxide, nitrous oxide, and combinations thereof. At least 90 percent by weight of the second propellant is at least one of nitrogen, argon, helium, oxygen, and combinations thereof.

公开(公告)号：US11999556B2

公开(公告)日：2024-06-04

申请号：US18047881

申请日：2022-10-19

申请人： ADCO Products, LLC

发明人： David W. Carnahan ,  Yuwei Liu ,  Justin Bates

IPC分类号： B65D83/14 ,  B65D83/44 ,  B65D83/68

CPC分类号： B65D83/752 ,  B65D83/682 ,  B65D83/44

摘要： A substance dispensing system including a first pressure vessel defining a first interior space; a first substance positioned in the first interior space; a first portion of a first propellant positioned in the first interior space; and a first portion of a second propellant positioned in the first interior space. At least 90 percent by weight of the first propellant is at least one of carbon dioxide, nitrous oxide, and combinations thereof. At least 90 percent by weight of the second propellant is at least one of nitrogen, argon, helium, oxygen, and combinations thereof.