RU2013118499A - REPEATED SAFETY MECHANISM - Google Patents
REPEATED SAFETY MECHANISM Download PDFInfo
- Publication number
- RU2013118499A RU2013118499A RU2013118499/11A RU2013118499A RU2013118499A RU 2013118499 A RU2013118499 A RU 2013118499A RU 2013118499/11 A RU2013118499/11 A RU 2013118499/11A RU 2013118499 A RU2013118499 A RU 2013118499A RU 2013118499 A RU2013118499 A RU 2013118499A
- Authority
- RU
- Russia
- Prior art keywords
- engine
- anchor
- stopper
- anchors
- electromagnet
- Prior art date
Links
- 238000013459 approach Methods 0.000 claims abstract 2
- 239000004568 cement Substances 0.000 claims abstract 2
Landscapes
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Dowels (AREA)
Abstract
1. Предохранительный механизм многократного взведения, характеризующийся тем, что он содержит движок, открывающий или закрывающий в одном из двух устойчивых положений огневой канал, при этом движок размещен между торцами двух, установленных соосно электромагнитов и имеет два цилиндрических якоря, каждый из которых входит в один из электромагнитов, а с внешних торцов электромагнитов размещены якоря, закрепленные на плечах поворотных стопоров, вторые плечи которых поджаты пружинами к движку, причем стопор, якорь которого имеет зазор с торцем электромагнита, входит в зацепление с движком, препятствуя его возможному перемещению, а стопор, якорь которого соприкасается с торцем электромагнита без зазора (с малым зазором), опирается на движок, не препятствуя его возможному перемещению, при этом на движке выполнены наклонные плоскости, к которым пружинами поджаты шарики, причем тяговое усилие, создаваемое электромагнитом на якоре движка, превосходит силу сопротивления шариков только после сближения якоря стопора с якорем движка и выхода стопора из зацепления с движком.2. Предохранительный механизм по п.1, отличающийся тем, что на торцах якорей движка выполнены углубления конической формы, а на торцах якорей стопоров выполнены конические выступы ответной формы.1. The safety mechanism of multiple cocking, characterized in that it contains an engine that opens or closes the fire channel in one of two stable positions, while the engine is located between the ends of two coaxially mounted electromagnets and has two cylindrical anchors, each of which is included in one from electromagnets, and from the external ends of the electromagnets placed anchors mounted on the shoulders of the rotary stoppers, the second shoulders of which are spring-loaded to the engine, and the stopper, the anchor of which has a gap with the torus The cement of the electromagnet engages with the engine, preventing it from moving, and the stopper, whose anchor is in contact with the end of the electromagnet without a gap (with a small gap), rests on the engine without preventing it from moving, inclined planes are made on the engine to with which the balls are pressed by springs, and the traction force created by the electromagnet at the engine’s anchor exceeds the resistance of the balls only after the stopper’s anchor approaches the engine’s anchor and the stopper disengages from the engine. 2. The safety mechanism according to claim 1, characterized in that the ends of the anchors of the engine have recesses of the conical shape, and the ends of the anchors of the stoppers have conical protrusions of the reciprocal form.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2013118499/11A RU2541619C2 (en) | 2013-04-23 | 2013-04-23 | Safety mechanism of repeated cocking |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2013118499/11A RU2541619C2 (en) | 2013-04-23 | 2013-04-23 | Safety mechanism of repeated cocking |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2013118499A true RU2013118499A (en) | 2014-10-27 |
| RU2541619C2 RU2541619C2 (en) | 2015-02-20 |
Family
ID=53289124
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2013118499/11A RU2541619C2 (en) | 2013-04-23 | 2013-04-23 | Safety mechanism of repeated cocking |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2541619C2 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2708424C1 (en) * | 2019-09-24 | 2019-12-06 | Акционерное общество "Научно-исследовательский технологический институт им. П.И. Снегирева" | Multiple arming safety mechanism |
| RU2760863C1 (en) * | 2021-02-11 | 2021-12-01 | ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ | Safety-type initiator for detonation separation systems of space vehicles |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3658009A (en) * | 1969-05-08 | 1972-04-25 | Lockheed Aircraft Corp | Safe arm initiator |
| RU2186335C1 (en) * | 2001-10-08 | 2002-07-27 | Федеральное государственное унитарное предприятие "Научно-исследовательский институт "Поиск" | Contact fuse for guided missiles |
| RU2255302C1 (en) * | 2004-02-17 | 2005-06-27 | Федеральное государственное унитарное предприятие "Научно-исследовательский институт "Поиск" | Safety-and-actuating mechanism of fuse |
-
2013
- 2013-04-23 RU RU2013118499/11A patent/RU2541619C2/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2541619C2 (en) | 2015-02-20 |
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| PD4A | Correction of name of patent owner | ||
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Free format text: LICENCE FORMERLY AGREED ON 20181001 Effective date: 20181001 |