A cargo restraint system includes a driving shaft, a first restraint, and a second restraint. The first restraint is operatively coupled to the driving shaft via a first indexing mechanism arrangement. The second restraint is operatively coupled to the driving shaft via a second indexing mechanism arrangement. The first and second indexing mechanism arrangements are arranged such that rotation of the driving shaft in a first rotational direction causes the first restraint to rotate between a lowered position and a raised position, and further rotation of the driving shaft in the same rotational direction causes the second restraint to rotate between the lowered position and the raised position. The first restraint may be axially offset from the second restraint to allow sequential loading and unloading of cargo.
SYSTEMS AND METHODS FOR RESTRAINING CARGO ON AIRCRAFT LOADING SYSTEMS USING INDEXING MECHANISMS
2022-10-13
Patent
Elektronische Ressource
Englisch
Systems and methods for restraining cargo on aircraft loading systems using indexing mechanisms
Europäisches Patentamt | 2024
|CARGO RESTRAINING ASSEMBLY, CARGO LOADING SYSTEM AND AIRCRAFT
Europäisches Patentamt | 2015
|Cargo restraining barrier, cargo loading system and aircraft
Europäisches Patentamt | 2019
|Cargo restraining assembly, cargo loading system and aircraft
Europäisches Patentamt | 2018
|Cargo restraining barrier, cargo loading system and aircraft
Europäisches Patentamt | 2017
|