Fin deployment mechanism for projectile and method for fin deployment
US-2016252333-A1 · Sep 1, 2016 · US
US11378367B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11378367-B2 |
| Application number | US-201816760469-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 24, 2018 |
| Priority date | Nov 28, 2017 |
| Publication date | Jul 5, 2022 |
| Grant date | Jul 5, 2022 |
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A fuse is provided with a reversible airbrake intended for a projectile, wherein the airbrake is arranged such that errors which occur in the flight path of the projectile can be corrected by performing one or more extensions and retractions of the airbrake. The airbrake includes at least two braking surfaces symmetrically arranged each behind a respective protective device arranged on the casing surface of the fuse, wherein the brake surfaces can be extended and retracted in a rotational direction behind the at least two protective devices via a twist shaft arranged centrally in the fuse.
Opening claim text (preview).
The invention claimed is: 1. A fuse with a reversible airbrake, comprising a casing having a casing surface, protective devices arranged on the casing surface, and a reversible airbrake intended for a projectile, wherein the airbrake comprises at least one brake disc, the at least one brake disc comprising at least two brake surfaces arranged on a brake ring, the at least two brake surfaces being in a form of radially protruding parts on a periphery of the brake ring, the radially protruding parts being evenly distributed around the casing surface and arranged each behind a respective protective device of the protective devices in order to reduce the air resistance of the brake surfaces behind, wherein the brake surfaces are rotationally movable about a longitudinal axis of the fuse between a retracted position behind the respective protective devices and an extended position and, when retracted to the retracted position, the brake surfaces are concealed behind the respective protective devices when viewed from a front end of the fuse. 2. The fuse with a reversible airbrake according to claim 1 , comprising three to ten brake surfaces evenly distributed around the casing surface. 3. The fuse with a reversible airbrake according to claim 1 , wherein the brake surfaces are arranged successively in pairs behind the respective protective devices, the respective protective devices defining a rear plane and being evenly distributed on and around the casing surface, wherein the arranged brake surfaces are formed by a front brake surface arranged closest to the rear plane and a rear brake surface arranged behind the front brake surface in a direction away from the frontend. 4. The fuse with a reversible airbrake according to claim 3 , comprising one or more rear brake surfaces. 5. The fuse with a reversible airbrake according to claim 1 , wherein the brake surfaces are formed with a cross-section which corresponds to the cross-section of the respective protective device, so that in the retracted position, the brake surfaces are concealed behind the protective devices when viewed from the front. 6. The fuse with a reversible airbrake according to claim 1 , wherein the brake surfaces are formed with a rectangular, circular, fin-shaped or arcuate cross-section. 7. The fuse with a reversible airbrake according to claim 1 , wherein the respective protective devices define a rear plane, and the at least one brake disc includes a front brake ring arranged closest to the rear plane and one or more rear brake rings arranged behind the front brake ring in a direction away from the front end, the brake surfaces are evenly distributed on the front brake ring and the one or more rear brake rings. 8. A method of controlling the longitudinal spread of a projectile comprising an existing path-correcting fuse, the method comprising replacing the existing path-correcting fuse with a fuse comprising a reversible airbrake according to claim 1 . 9. A projectile comprising a fuse according to claim 1 .
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