DE102010045516B4 - Missile with deployable fragmentation warhead - Google Patents
Missile with deployable fragmentation warhead Download PDFInfo
- Publication number
- DE102010045516B4 DE102010045516B4 DE201010045516 DE102010045516A DE102010045516B4 DE 102010045516 B4 DE102010045516 B4 DE 102010045516B4 DE 201010045516 DE201010045516 DE 201010045516 DE 102010045516 A DE102010045516 A DE 102010045516A DE 102010045516 B4 DE102010045516 B4 DE 102010045516B4
- Authority
- DE
- Germany
- Prior art keywords
- warhead
- missile
- sectors
- deployable
- quarter
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/22—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
- F42B12/24—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction with grooves, recesses or other wall weakenings
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Flugkörper (11) mit infolge Anlenkung an die Flugkörper-Struktur (15) aus achsparalleler Verbringungsstellung ausstellbarem Splitter-Gefechtskopf (12), dadurch gekennzeichnet, dass ein dickwandig hohlzylindrischer Gefechtskopf (12) in vier Viertel-Sektoren (19) längsgeteilt ist, von denen zwei (19.5, 19.6) um achsparallele Schwenkwellen (20) bei den Durchmesser-Enden des Gefechtskopfes (12) aus dem Hohlzylinder heraus ausstellbar angelenkt sind.A missile (11) with splinter warhead (12) which can be deployed as a result of linkage to the missile structure (15) from an axially parallel transfer position, characterized in that a thick-walled hollow cylindrical warhead (12) is split longitudinally into four quarter sectors (19), of which two (19.5, 19.6) are articulated about axially parallel pivot shafts (20) at the diameter ends of the warhead (12) out of the hollow cylinder out.
Description
Die Erfindung betrifft einen Flugkörper mit Splittergefechtskopf gemäß dem Oberbegriff des Anspruchs 1.The invention relates to a missile with fragmentation warhead according to the preamble of claim 1.
Derartige Maßnahmen sind aus der
In Erkenntnis dieser Gegebenheiten liegt vorliegender Erfindung die technische Problemstellung zugrunde, ein Gefechtskopf gattungsgemäßer Art für eine bei reduziertem konstruktivem Aufwand dichtere Splitterwirkung in der Zielebene auszulegen.In recognition of these circumstances, the present invention is based on the technical problem of designing a warhead of the generic type for a denser fragmentation effect at a reduced design cost in the target plane.
Diese Aufgabe wird durch den Flugkörper gemäß Anspruch 1 gelöst. Eine bevorzugte Ausführungsform der Erfindung ist im Anspruch 2 angegeben.This object is achieved by the missile according to claim 1. A preferred embodiment of the invention is specified in claim 2.
Gemäß einem nicht zur Erfindung gehörigen Beispiel, welches das eingangs beschriebene speichenförmige Ausstellen von Gefechtskopf-Sektoren weiterbildet, sind vier Viertelsektoren in Flugkörper-Längsrichtung in wenigstens zwei Abschnitte unterteilt, die peripher gegeneinander versetzt über quer zu Flugkörper-Längsachse orientierte Schwenkwellen an die Flugkörper-Struktur angelenkt sind. Daraus resultieren in der Zielebene zweimal vier um ein gemeinsames Zentrum gegeneinander verschwenkte, peripher einander überlappende sternförmige Splitterwirkbereiche und damit eine Belegung auch der bisher nicht erfassten Sektoren bei den Winkelhalbierenden des speichenförmigen Splitterbildes.According to an example not belonging to the invention, which further develops the spoke-shaped issuing of warhead sectors described above, four quarter sectors in the longitudinal direction of the missile are subdivided into at least two sections which are peripherally offset from each other by pivot shafts oriented transversely to the missile longitudinal axis to the missile structure are articulated. This results in the target plane twice four around a common center against each other pivoted, peripherally overlapping star-shaped splitter effective areas and thus occupancy of the previously unrecognized sectors at the bisectors of the spoke-shaped fragmentation image.
Eine noch lückenlosere Splitterbelegung in der Zielebene ergibt der erfindungsgemäße Lösungsansatz, nach dem die Splitter nicht mehr in Flugrichtung voraus, sondern im Zielüberflug abgeliefert werden. Danach ist der dickwandig hohlzylindrische Gefechtskopf mit seiner wieder radial nach außen orientierten Splitterbelegung nun in zwei achsparallele Halbzylinder geteilt, von denen der obere seinerseits in zwei Viertelzylinder-Sektoren geteilt ist. Diese sind um achsparallele Schwenkwellen in eine Stellung seitlich neben dem Halbzylinder herausklappbar, so dass deren Splitterbelegungen dann gleicherweise in Richtung quer zu Flugkörper-Längsachse auf die Zielebene orientiert sind, wie die Splitterbelegung des Halbzylinders. Diese Zielebene ist gewöhnlich der Grund unter der Flugbahn; sie kann aber auch neben oder über der Flugbahn liegen, wenn dort operierende Ziele im Vorbeiflug abgewehrt werden sollen. Zweckmäßigerweise ist die Struktur des Flugkörpers dafür mit Leitflächen ausgestattet, die den Flugkörper um seine Längsachse rotieren lassen. Der Gefechtskopf wird dann gezündet, wenn ein. Ziel gerade in der Richtung erfasst wird, in der die Splitter orientiert sind. Die kurz zuvor schon ausgestellten Gefechtskopfquadranten führen infolge des erhöhten Luftwiderstandes beim Abfeuern der Splitter zu einer für die Splitterwirkung wünschenswerten Verringerung der Geschwindigkeit des Flugkörpers.An even more complete splitter assignment in the target plane results in the inventive approach, according to which the splitter is no longer ahead in the direction of flight, but delivered in the target overflight. Thereafter, the thick-walled hollow cylindrical warhead is now divided with its again radially outwardly oriented splinter assignment in two axially parallel half-cylinder, of which the upper in turn is divided into two quarter-cylinder sectors. These are foldable about axially parallel pivot shafts in a position laterally adjacent to the half cylinder, so that their splitter assignments are then oriented in the same direction in the direction transverse to missile longitudinal axis on the target plane, such as the fragmentation of the half-cylinder. This goal level is usually the ground under the trajectory; but it can also be located next to or above the trajectory, if there operating targets are to be fended off in flyby. Conveniently, the structure of the missile for this purpose is equipped with baffles that rotate the missile about its longitudinal axis. The warhead is then ignited if one. Target is detected in the direction in which the splinters are oriented. Due to the increased air resistance when firing the splinters, the warhead quadrants that have been issued shortly before lead to a reduction in the velocity of the missile which is desirable for the splinter effect.
Zusätzliche Weiterbildungen und weitere Abwandlungen der erfindungsgemäßen Lösungen ergeben sich, auch hinsichtlich deren Vorteilen, aus nachstehender Beschreibung von etwa maßstabsgerecht verkleinert skizzierten bevorzugten Ausführungsbeispielen zur Erfindung. In den Zeichnungen zeigt:Additional refinements and further modifications of the solutions according to the invention emerge, also with regard to their advantages, from the following description of scaled down to approximately scaled preferred embodiments of the invention. In the drawings shows:
Bei dem in
Dieser hohlzylindrische Gefechtskopf
Der Gefechtskopf
Wenn dagegen der Flugkorper
Über die konstruktiv bedingte Endstellung der seitlich bis gegen Anschlage ausgestellten Sektoren
Für moglichst luckenloses Belegen einer Zielebene
BezugszeichenlisteLIST OF REFERENCE NUMBERS
- 1111
-
Flugkorper (mit
12 )Aircraft (with12 ) - 1212
-
Gefechtskopf (zwischen
13 und14 )Warhead (between13 and14 ) - 1313
-
Ogive (von
11 )Ogive (from11 ) - 1414
-
Heck (von
11 )Stern (from11 ) - 1515
-
Struktur (von
11 )Structure (from11 ) - 1616
-
Mantelflache (von
12 )Lateral surface (from12 ) - 1717
-
Splitter (auf
16 )Splitter (up16 ) - 1818
-
Sprengladung (von
12 )Explosive charge (from12 ) - 1919
-
Quadranten-Sektoren (von
12 )Quadrant sectors (from12 ) - 2020
-
Schwenkwellen (an
15 fur19 )Swivel shafts (on15 For19 ) - 2121
-
Langsachse (von
11 )Langsachse (from11 ) - 2222
-
Schubstangen (unter
19 ;1 bis5 )Push rods (under19 ;1 to5 ) - 2323
-
Schubhulsen (für
22 )Thrust sleeves (for22 ) - 2424
-
Zielebene (für
17 )Target level (for17 ) - 2525
-
Splitterwirkbereich (in
24 )Splitter effect area (in24 )
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE201010045516 DE102010045516B4 (en) | 2010-09-15 | 2010-09-15 | Missile with deployable fragmentation warhead |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE201010045516 DE102010045516B4 (en) | 2010-09-15 | 2010-09-15 | Missile with deployable fragmentation warhead |
Publications (2)
Publication Number | Publication Date |
---|---|
DE102010045516A1 DE102010045516A1 (en) | 2012-03-15 |
DE102010045516B4 true DE102010045516B4 (en) | 2015-04-30 |
Family
ID=45756150
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE201010045516 Active DE102010045516B4 (en) | 2010-09-15 | 2010-09-15 | Missile with deployable fragmentation warhead |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE102010045516B4 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2926165C (en) * | 2013-10-02 | 2020-07-21 | Leijona Instituutti Oy | Ground-to-air munition |
EP3171121A1 (en) * | 2015-11-18 | 2017-05-24 | Textron Systems Corporation | Multi-warhead munition with configurable segmented warhead |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2206403A1 (en) * | 1972-02-11 | 1973-08-16 | Messerschmitt Boelkow Blohm | Warhead - with a series of explosive bodies |
DE1924650C1 (en) * | 1969-05-14 | 1977-11-10 | Dynamit Nobel Ag | Warhead |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2340652A1 (en) | 1972-08-18 | 1974-04-04 | Fmc Corp | GUN |
-
2010
- 2010-09-15 DE DE201010045516 patent/DE102010045516B4/en active Active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1924650C1 (en) * | 1969-05-14 | 1977-11-10 | Dynamit Nobel Ag | Warhead |
DE2206403A1 (en) * | 1972-02-11 | 1973-08-16 | Messerschmitt Boelkow Blohm | Warhead - with a series of explosive bodies |
Also Published As
Publication number | Publication date |
---|---|
DE102010045516A1 (en) | 2012-03-15 |
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R016 | Response to examination communication | ||
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R018 | Grant decision by examination section/examining division | ||
R020 | Patent grant now final | ||
R081 | Change of applicant/patentee |
Owner name: DIEHL DEFENCE GMBH & CO. KG, DE Free format text: FORMER OWNER: DIEHL BGT DEFENCE GMBH & CO. KG, 88662 UEBERLINGEN, DE |