Brake panel for a detonator or a projectile

US9702675B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9702675-B2
Application numberUS-201314375997-A
CountryUS
Kind codeB2
Filing dateJan 28, 2013
Priority dateFeb 6, 2012
Publication dateJul 11, 2017
Grant dateJul 11, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The invention relates to a brake panel ( 3, 3 ′) for a projectile ( 1 ), in which those surfaces (A) of the brake panel ( 3, 3 ′) which are facing in the direction of travel of the projectile are wholly or partially angled in such a way that the normal from the said surfaces (A) is not parallel with the center line (C) of the projectile ( 1 ) in order to reduce or counteract the Magnus torque generated during and after the extension of the brake panel ( 3, 3 ′). The invention further relates to a detonator ( 2 ) for a projectile ( 1 ) and a projectile ( 1 ) comprising such a brake panel.

First claim

Opening claim text (preview).

The invention claimed is: 1. A brake panel as part of a projectile, which projectile is for firing from a launcher, wherein those surfaces of the brake panel which are facing in the direction of travel of the projectile are angled in such a way that the normal from the said surfaces (A) is not parallel with the centre line (C) of the projectile, and that the rear side of the brake panel, situated opposite to the direction of travel of the projectile, is flatly configured with a normal from the surface having the same angulation as the centre line of the projectile. 2. The brake panel according to claim 1 , wherein an angulation of the normal from that surface (A) of the brake panel which is facing in the direction of travel is in the order of magnitude of 1 degree relative to the centre line (C) of the projectile. 3. The brake panel according to claim 2 , wherein an angulation of those surfaces (A) of the brake panel which are facing in the direction of travel of the projectile is variably adjustable relative to the centre line (C) of the projectile. 4. The brake panel according to claim 1 , wherein an angulation of those surfaces (A) of the brake panel which are facing in the direction of travel of the projectile is variably adjustable relative to the centre line (C) of the projectile. 5. A projectile comprising a detonator having one or more extensible brake panels, which projectile is for firing from a launcher, wherein those surfaces (A) of the brake panel which are facing in the direction of travel of the projectile are angled in such a way that the normal from the said surfaces (A) is not parallel with the centre line (C) of the projectile, and that the rear side of the brake panel, situated opposite to the direction of travel of the projectile, is flatly configured with a normal from the surface having the same angulation as the centre line (C) of the projectile. 6. The projectile comprising a detonator having one or more extensible brake panels according to claim 5 wherein the angulation of the normal from that surface of the brake panel which is facing in the direction of travel is in the order of magnitude of 1 degree relative to the centre line (C) of the projectile. 7. The projectile comprising a detonator having one or more extensible brake panels according to claim 5 wherein the angulation of those surfaces of the brake panel which are facing in the direction of travel of the projectile is variably adjustable relative to the centre line (C) of the projectile. 8. A projectile for firing from a launcher, which projectile comprises one or more extensible brake panels, those surfaces (A) of the brake panels which are facing in the direction of travel of the projectile are angled in such a way that the normal from the said surfaces (A) is not parallel with the centre line (C) of the projectile, and that the rear side of the brake panel, situated opposite to the direction of travel of the projectile, is flatly configured with a normal from the surface having the same angulation as the centre line (C) of the projectile. 9. The projectile according to claim 8 , wherein the number of brake panels is two or four or six or eight. 10. The projectile according to claim 9 , wherein the brake panel is variably adjustable between the fully extended state and the wholly retracted state. 11. The projectile according to claim 8 , wherein the number of brake panels is one or three or five or seven. 12. The projectile according to claim 11 , wherein the brake panel is variably adjustable between the fully extended state and the wholly retracted state.

Assignees

Inventors

Classifications

  • F42B10/50Primary

    Brake flaps {, e.g. inflatable} · CPC title

  • Fuze bodies; Fuze housings · CPC title

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Frequently asked questions

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What does patent US9702675B2 cover?
The invention relates to a brake panel ( 3, 3 ′) for a projectile ( 1 ), in which those surfaces (A) of the brake panel ( 3, 3 ′) which are facing in the direction of travel of the projectile are wholly or partially angled in such a way that the normal from the said surfaces (A) is not parallel with the center line (C) of the projectile ( 1 ) in order to reduce or counteract the Magnus torque g…
Who is the assignee on this patent?
Bae Systems Bofors Ab
What technology area does this patent fall under?
Primary CPC classification F42B10/50. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jul 11 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).