Process for the production of speherical tetranitroglycouril
US-9512127-B2 · Dec 6, 2016 · US
US11884604B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11884604-B2 |
| Application number | US-201615758808-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 12, 2016 |
| Priority date | Sep 10, 2015 |
| Publication date | Jan 30, 2024 |
| Grant date | Jan 30, 2024 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
The invention is in the field of propellants. In particular the invention is directed to a propellant for ammunition, such as medium and large caliber gun ammunition, having improved performance. In accordance with the present invention a propellant charge comprises one or more longitudinally extending, progressive-externally burning grains having a number of perforations passing through the grains in the length direction and having a cross-sectional shape (perpendicular to the grain's length direction) that is elongated.
Opening claim text (preview).
The invention claimed is: 1. Propellant charge comprising one or more longitudinally extending, progressive-externally burning grains having a number of perforations passing through the grains in the length direction, wherein said grains have a cross-sectional shape (perpendicular to the grain's length direction) that is elongated, wherein said grains have a cross-sectional shape that is line-symmetric in at most two different lines, and wherein said grains are cut under an angle of 45°-90°, relative to their longitudinal axis. 2. Propellant charge according to claim 1 , wherein said grains comprise eight or more perforations. 3. Propellant charge according to claim 1 , wherein said grains have a cross-sectional shape that is diamond shaped having four or five edges, or an elongated polygon having six edges, of which four have the same length. 4. Propellant charge according to claim 1 , wherein said grains are made by extrusion. 5. Propellant charge according to claim 1 , wherein at least part of said grains are provided with an outer layer that has a chemical composition that is less energetic than the inner composition of the respective grain. 6. Ammunition comprising a propellant charge according to claim 1 . 7. Propellant charge according to claim 2 , wherein said grains comprise less than eighteen perforations. 8. Propellant charge according to claim 7 , wherein said grains comprise fourteen perforations. 9. Propellant charge according to claim 8 , wherein said grains comprise nine perforations. 10. Propellant charge according to claim 1 , wherein said grains are cut under an angle of about 60°, relative to their longitudinal axis.
Compositions or products which are defined by structure or arrangement of component of product (explosive charges of particular form or shape F42B1/00, F42B3/00) · CPC title
having contiguous layers or zones · CPC title
characterised by composition or physical dimensions or form of propellant charge, {with or without projectile,} or powder (chemical composition C06B; {F42B5/24 takes precedence}) · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.