| Eurenco Bofors AB Patent applications |
| Patent application number | Title | Published |
|---|
| 20160137566 | PHLEGMATISATION OF AN EXPLOSIVE IN AN AQUEOUS SUSPENSION - A method for phlegmatising an explosive in an aqueous suspension including a dispersed phlegmatising agent. The phlegmatising agent is deposited on a surface of the explosive at low temperature utilizing opposite electric charges of the phlegmatising agent and the explosive. Also a device and a phlegmatised explosive. | 05-19-2016 |
| 20120097060 | PROGRESSIVE PROPELLANT CHARGE WITH HIGH CHARGE DENSITY - A method for producing propellant charges with progressive combustion characteristic and a higher charge density than previously considered possible to achieve, intended in the first instance for direct-firing barrel weapons such as tank cannons. Combined in the charge are at least two radially perforated propellant tubes, which are arranged in their entirety inside or after one another, and which have at an e-dimension selected in relation to the actual type of propellant and its desired combustion characteristic, combustion or ignition channels, and which have circular outer and inner boundary surfaces, in conjunction with which, before initiation of the charge, at least one of the total number of outer surfaces of these propellant tubes that are available for initiation has been treated with an inhibition, surface treatment or surface intended to delay the propagation of ignition to that surface so that the combustion of the propellant tubes is partially mutually overlapping. | 04-26-2012 |
| 20090148549 | PROPELLANT AND A METHOD AND DEVICE FOR PRODUCING THE SAME - The present invention relates to a method and a device for producing perforated propellant in the geometric form of block, stick, slab, cylindrical or tubular propellant ( | 06-11-2009 |
| 20080282926 | Method and Arrangement For Producing Propellant For Charges With High Charge Density and High Progressivity - The present invention relates to a method and an arrangement for the production of radially perforated, cylindrical propellant tubes ( | 11-20-2008 |
