EP1533589B1 - Control system using a transversal jet - Google Patents
Control system using a transversal jet Download PDFInfo
- Publication number
- EP1533589B1 EP1533589B1 EP04023729A EP04023729A EP1533589B1 EP 1533589 B1 EP1533589 B1 EP 1533589B1 EP 04023729 A EP04023729 A EP 04023729A EP 04023729 A EP04023729 A EP 04023729A EP 1533589 B1 EP1533589 B1 EP 1533589B1
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- EP
- European Patent Office
- Prior art keywords
- contact element
- control block
- ignition
- control apparatus
- lateral
- 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.)
- Expired - Lifetime
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- 239000012777 electrically insulating material Substances 0.000 claims abstract description 7
- 239000004020 conductor Substances 0.000 claims description 42
- 238000000465 moulding Methods 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 3
- 238000010137 moulding (plastic) Methods 0.000 claims description 2
- 239000000758 substrate Substances 0.000 claims 14
- 239000003380 propellant Substances 0.000 abstract description 5
- 239000004033 plastic Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 239000000969 carrier Substances 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 210000003746 feather Anatomy 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
Definitions
- the invention relates to a transverse thrust control device for influencing the trajectory of a missile, which comprises a multiple shots for corresponding correction engines containing control block, wherein in each of the shots an ignition element for the corresponding engine correction is arranged, and wherein each of the ignition elements has at least one contact element can be connected via an electrical line with an electronic control unit.
- Such lateral thrust control devices for correcting the trajectory e.g. ballistic missiles or missiles are known per se.
- the contact elements of the ignition elements are first connected to cables in the known control devices. Subsequently, the cables are then threaded through generally radial bores of the control block in a central, axially extending recess of the control block and screwed the Anzündiata in the control block.
- a disadvantage of the known transverse thrust control devices therefore, among other things, the very time-consuming installation of the ignition elements and their electrical connection to the electronic control unit.
- the lateral thrust control device comprises a large number of corrective engines (some may be as much as 180 corrective engines)
- an extremely large amount of assembly time is required due to the very limited space available inside the control block.
- it can easily by twisting the individual cables when screwing the ignition to cancel the cable z. B. come in the region of the contacts of the respective ignition element.
- a track-correctable projectile describes the EP 0 485 897 A1 This has along its circumference distributed transverse thrust drive means, each drive means having a pulse charge and a lid which is radially ejected by the pulse charge. Each pulse charge is provided with a detonator connected to an electric ignition cable
- the US 6,367,735 B1 (Basis for the preamble of claim 1) discloses a projectile, with a body, are introduced into the circumferentially shaped recesses, which open into a central, axially extending recess into which ignite ignition elements with its two pins.
- a device for steering a missile can be removed, which has a control block with arranged perpendicular to the missile surface exhaust openings corresponding nozzle body. Connected are the propellant charges with the ignition device via electrical lines.
- the invention has for its object to disclose a transverse thrust control device of the type mentioned, in which the electrical lines between the ignition elements and the electronic control unit are easily mounted safely.
- the invention is based essentially on the idea of replacing the electrical cables connected to the ignition elements by conductor tracks which are fixedly arranged on tubular, rotatably and non-displaceably arranged in the recess of the control block and the carrier only when screwing or plugging the ignition elements in the recordings of the control block are contacted by their contact elements.
- the interconnects can be applied in a conventional manner on the Kaussträgem (eg by electroplating or sticking of conductor sheets).
- the transverse thrust control device ignition elements which are provided for safety reasons, each with two contact elements and are therefore also connected via two tracks to the electronic control unit.
- two telescoping and rotatable in their end position and 29iebeêt fixable conductor carrier are provided, on each of which one of the two tracks is fixed, such that z. B. when screwing a Anzündettis a contact element contacted the conductor on the ignition element adjacent the first line carrier and the other contact element is passed through the first conductor carrier and contacted the corresponding conductor on the second conductor carrier.
- the transverse thrust control device comprises ignition elements, each having a first rod-shaped contact element and a second, cylindrically shaped contact element which surrounds the rod-shaped contact element, but has a smaller length than the latter.
- the respectively arranged on the first conductor carrier respectively first conductor track is contacted by a portion of the cylindrical contact element of the corresponding ignition element.
- the pipe-shaped pipe supports may be plastic moldings which are provided at their one end respectively with a lug-shaped head part arranged outside the receptacle of the control block, which extends perpendicularly to the longitudinal axis of the control device and at which e.g. the connections of the conductor tracks are arranged for connection to the electronic control unit.
- this head part of the cable carrier can be used for the rotation and displacement secure fixing of the cable carrier.
- the respective tab-shaped head part has at least one bore through which a pin-shaped or screw-shaped fixing element is passed, which is non-positively connected to the end face of the control block facing the cable carrier.
- a tubular molded part made of an electrically insulating material.
- FIG. 1, 1 designates a transverse thrust control device which can be used, for example, in a ballistic projectile (not shown), in which case the central longitudinal axis 2 of the control device 1 coincides with the longitudinal axis of the corresponding projectile.
- the lateral thrust control device 1 comprises a control block 3 made of metal, in which a plurality of correction engines 4 distributed over the circumference are arranged in corresponding receptacles 5.
- the receptacles 5 each have a longitudinal axis 6 which is slightly inclined relative to a radial, the longitudinal axis 2 of the control block 3 intersecting plane.
- the known correction engines 4 essentially comprise an ignition element 7 which can be screwed into the respective receptacle 5, a propellant charge 8 and a nozzle 9.
- the respective ignition element 7 has in the illustrated embodiment, two contact elements 10 and 11 ( Figure 2).
- the first contact element 10 is rod-shaped and the second contact element 11 is cylindrical and surrounds the first contact element 10.
- the first contact element 10 also has a greater length than the second contact element 11.
- the control block 3 has a central axially extending recess 12, which may be cylindrical or conical and in which the contact elements 10, 11 of the respective Anzündiatas 7 edge protrude slightly.
- the recess 12 are three nested, tubular, the longitudinal axis of the control block 3 enclosing mold parts 13-15 ( Figure 2), which are arranged on the control block 3 against rotation and secure against displacement.
- a molding 13 made of an electrically insulating material, e.g. Plastic, on.
- tubular members 14 and 15 are the other two tubular members formed as tubular members 14 and 15.
- Each of these two conductor beams 14, 15 consists of a molded part of an electrically insulating material (eg plastic) and has on the outside conductor tracks 17, 18, respectively be contacted by one of the two contact elements 10, 11 of a Anzündiatas 7.
- the cylindrical contact element 11 is pressed through the first molded part 13 when screwing the ignition element 7 into the receptacle 5 and contacts the first printed conductor 17 of the second molded part 14 assigned to this contact element 11 in a partial region 23.
- the rod-shaped contact element On the other hand, 10 of the ignition element 7 is pressed through both the first molded part 13 and the second molded part 14 and contacts the second printed conductor 18 of the third molded part 15 assigned to this contact element 10, wherein the first printed circuit 17 and the second printed conductor 18 are arranged one above the other. So that the first contact element 10 does not likewise touch the first conductor track 17, this conductor track 17 has a ring-shaped conductor region 19 which does not touch the first contact element 10 in the region in which the first contact element 10 is passed through the first conductor carrier 14.
- the three mold parts 13-15 For positioning the three mold parts 13-15 in the circumferential direction, they each have at their one end a tab-shaped head part 20 which is arranged outside the recess 12 of the control block 3 and which extends perpendicularly to the longitudinal axis 2 of the control device 1.
- the respective head part 20 is supported on an end face 21 of the control block 3 and has a bore, through which the shaft of a screw 22 is guided as a positioning element.
- the screw 22 therefore causes in addition to the positioning of the mold parts 13-15 in the circumferential direction and a fixation in the axial direction Direction.
- the invention is not limited to the embodiment described above.
- control block is made of an electrically insulating material (for example made of glass fiber reinforced plastic)
- the first shaped body can also be dispensed with, since insulation between the first conductor track and the inner surface of the control block is not required.
- the multilayer structure is preferably first prepared on a flat flexible circuit board and then then transferred to a tube.
- the multilayer board can be wrapped around a support tube and optionally also fixed to this.
- the longitudinal axes 6 of the receptacles 5 need not be inclined for the correction engines 4, but may also intersect the longitudinal axis 2 of the control block 3 at a right angle.
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- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
- Transmission Devices (AREA)
- Vehicle Body Suspensions (AREA)
- Plasma Technology (AREA)
- Elimination Of Static Electricity (AREA)
- Installation Of Indoor Wiring (AREA)
Abstract
Description
Die Erfindung betrifft eine Querschub-Steuervorrichtung zur Beeinflussung der Flugbahn eines Flugkörpers, die einen mehrere Aufnahmen für entsprechende Korrekturtriebwerke enthaltenden Steuerblock umfaßt, wobei in jeder der Aufnahmen ein Anzündelement für das entsprechende Korrekturtriebwerk angeordnet ist, und wobei jedes der Anzündelemente mindestens ein Kontaktelement aufweist, das über eine elektrische Leitung mit einer elektronischen Steuereinheit verbindbar ist.The invention relates to a transverse thrust control device for influencing the trajectory of a missile, which comprises a multiple shots for corresponding correction engines containing control block, wherein in each of the shots an ignition element for the corresponding engine correction is arranged, and wherein each of the ignition elements has at least one contact element can be connected via an electrical line with an electronic control unit.
Derartige Querschub-Steuervorrichtungen zur Korrektur der Flugbahn, z.B. ballistischer Geschosse oder Raketen, sind an sich bekannt. Dabei werden bei den bekannten Steuervorrichtungen die Kontaktelemente der Anzündelemente zunächst mit Kabeln verbunden. Anschließend werden die Kabel dann durch in der Regel radial verlaufende Bohrungen des Steuerblockes in eine zentrale, axial verlaufende Ausnehmung des Steuerblockes eingefädelt und die Anzündelemente in den Steuerblock eingeschraubt.Such lateral thrust control devices for correcting the trajectory, e.g. ballistic missiles or missiles are known per se. In this case, the contact elements of the ignition elements are first connected to cables in the known control devices. Subsequently, the cables are then threaded through generally radial bores of the control block in a central, axially extending recess of the control block and screwed the Anzündelemente in the control block.
Nachteilig ist bei den bekannten Querschub-Steuervorrichtungen daher unter anderem die sehr zeitaufwendige Montage der Anzündelemente und deren elektrische Verbindung mit der elektronischen Steuereinheit. Insbesondere wenn die Querschub-Steuervorrichtung eine große Anzahl von Korrekturtriebwerken umfaßt (z.T. kann es sich um bis zu 180 Korrekturtriebwerke handeln), wird aufgrund der sehr beschränkten Platzverhältnisse im Inneren des Steuerblockes außerordentlich viel Zeit für die Montage benötigt. Außerdem kann es durch das Verdrillen der einzelnen Kabel beim Einschrauben der Anzündelemente leicht zu einem Abbrechen der Kabel z. B. im Bereich der Kontakte des jeweiligen Anzündelementes kommen. Schließlich ist häufig eine Kontrolle der elektrischen Verbindung beim Anschluss der Kabel an der elektronischen Steuereinheit schwierig, weil nach dem Einschrauben der Anzündelemente deren Kontaktelemente nicht mehr zugänglich sind.A disadvantage of the known transverse thrust control devices, therefore, among other things, the very time-consuming installation of the ignition elements and their electrical connection to the electronic control unit. In particular, when the lateral thrust control device comprises a large number of corrective engines (some may be as much as 180 corrective engines), an extremely large amount of assembly time is required due to the very limited space available inside the control block. In addition, it can easily by twisting the individual cables when screwing the ignition to cancel the cable z. B. come in the region of the contacts of the respective ignition element. Finally, it is often difficult to control the electrical connection when connecting the cables to the electronic control unit, because after screwing in the ignition elements whose contact elements are no longer accessible.
Ein bahnkorrigierbares Projektil beschreibt die
Die
Der
Der Erfindung liegt die Aufgabe zugrunde, eine Querschub-Steuervorrichtung der eingangs erwähnten Art zu offenbaren, bei der die elektrischen Leitungen zwischen den Anzündelementen und der elektronischen Steuereinheit auf einfache Weise sicher montierbar sind.The invention has for its object to disclose a transverse thrust control device of the type mentioned, in which the electrical lines between the ignition elements and the electronic control unit are easily mounted safely.
Diese Aufgabe wird erfindungsgemäß durch die Merkmale des Anspruchs 1 gelöst. Weitere, besonders vorteilhafte Ausgestaltungen der Erfindung offenbaren die Unteransprüche.This object is achieved by the features of claim 1. Further, particularly advantageous embodiments of the invention disclose the dependent claims.
Die Erfindung beruht im wesentlichen auf dem Gedanken, die mit den Anzündelementen verbundenen elektrischen Kabel durch Leiterbahnen zu ersetzen, welche auf rohrförmigen, in der Ausnehmung des Steuerblocks dreh- und verschiebesicher angeordneten Leitungsträger fest angeordnet sind, und welche erst beim Einschrauben oder Einstecken der Anzündelemente in die Aufnahmen des Steuerblockes von deren Kontaktelementen kontaktiert werden.The invention is based essentially on the idea of replacing the electrical cables connected to the ignition elements by conductor tracks which are fixedly arranged on tubular, rotatably and non-displaceably arranged in the recess of the control block and the carrier only when screwing or plugging the ignition elements in the recordings of the control block are contacted by their contact elements.
Die Leiterbahnen können dabei in herkömmlicher Weise auf den Leitungsträgem aufgebracht werden (z.B. durch Aufgalvanisieren oder Aufkleben von Leiterbahnfolien).The interconnects can be applied in a conventional manner on the Leitungssträgem (eg by electroplating or sticking of conductor sheets).
Bei einer ersten Ausführungsform der Erfindung weist die Querschub-Steuervorrichtung Anzündelemente auf, die aus Sicherheitsgründen mit jeweils zwei Kontaktelementen versehen sind und daher auch über zwei Leiterbahnen mit der elektronischen Steuereinheit verbunden sind. Bei dieser Ausführungsform werden zwei ineinander schiebbare und in ihrer Endlage verdreh- und verschiebesicher fixierbare Leitungsträger vorgesehen, auf denen jeweils eine der beiden Leiterbahnen fest angeordnet ist, derart, dass z. B. beim Einschrauben eines Anzündelementes das eine Kontaktelement die Leiterbahn auf dem dem Anzündelement benachbarten ersten Leitungsträger kontaktiert und das jeweils andere Kontaktelement durch den ersten Leitungsträger hindurchgeführt ist und die entsprechende Leiterbahn auf dem zweiten Leitungsträger kontaktiert.In a first embodiment of the invention, the transverse thrust control device ignition elements, which are provided for safety reasons, each with two contact elements and are therefore also connected via two tracks to the electronic control unit. In this embodiment, two telescoping and rotatable in their end position and verschiebesicher fixable conductor carrier are provided, on each of which one of the two tracks is fixed, such that z. B. when screwing a Anzündelementes a contact element contacted the conductor on the ignition element adjacent the first line carrier and the other contact element is passed through the first conductor carrier and contacted the corresponding conductor on the second conductor carrier.
Für eine einfache Überprüfung der Leiterbahnen hat es sich als vorteilhaft erwiesen, wenn die beiden Leitungsträger derart innerhalb der Ausnehmung des Steuerblockes fixiert sind, daß die dem jeweiligen Anzündelement zugeordneten beiden Leiterbahnen in radialer Richtung möglichst direkt benachbart zueinander angeordnet sind.For a simple check of the strip conductors, it has proved to be advantageous if the two line carriers are fixed in such a way within the recess of the control block, that the two conductor tracks associated with the respective ignition element are arranged as directly adjacent as possible in the radial direction.
Bei einer weiteren Ausführungsform der Erfindung ist vorgesehen, daß die Querschub-Steuervorrichtung Anzündelemente umfaßt, die jeweils ein erstes stabförmiges Kontaktelement und ein zweites, zylinderförmig ausgebildetes Kontaktelement aufweisen, welches das stabförmige Kontaktelement umschließt, aber eine geringere Länge aufweist als Letzteres. Dabei wird die auf dem ersten Leitungsträger angeordnete jeweils erste Leiterbahn von einem Teilbereich des zylinderförmigen Kontaktelementes des entsprechenden Anzündelementes kontaktiert. Außerdem weist die jeweils erste Leiterbahn in dem Bereich, in dem das stabförmige Kontaktelement durch den ersten Leitungsträger hindurchgeführt ist, einen ringförmig ausgebildeten, das stabförmige Kontaktelement nicht berührenden Leiterbereich auf.In a further embodiment of the invention it is provided that the transverse thrust control device comprises ignition elements, each having a first rod-shaped contact element and a second, cylindrically shaped contact element which surrounds the rod-shaped contact element, but has a smaller length than the latter. In this case, the respectively arranged on the first conductor carrier respectively first conductor track is contacted by a portion of the cylindrical contact element of the corresponding ignition element. In addition, the respective first conductor track in the region in which the rod-shaped contact element is passed through the first conductor carrier, an annular formed, the rod-shaped contact element not touching the conductor region.
Bei den rohrförmigen Leitungsträgem kann es sich um Kunststoff-Formteile handeln, welche an ihrem einen Ende jeweils mit einem außerhalb der Aufnahme des Steuerblockes angeordneten, laschenförmig ausgebildeten Kopfteil versehen sind, das sich senkrecht zur Längsachse der Steuervorrichtung erstreckt und an dem z.B. die Anschlüsse der Leiterbahnen zur Verbindung mit der elektronischen Steuereinheit angeordnet sind. Außerdem kann dieses Kopfteil der Leitungsträger zur dreh- und verschiebesicheren Fixierung der Leitungsträger herangezogen werden. Hierzu weist das jeweilige laschenförmige Kopfteil mindestens eine Bohrung auf, durch welche ein stift- oder schraubenförmiges Fixierelement hindurchgeführt ist, welches mit der den Leitungsträger zugewandten Stirnwand des Steuerblockes kraftschlüssig verbunden ist.The pipe-shaped pipe supports may be plastic moldings which are provided at their one end respectively with a lug-shaped head part arranged outside the receptacle of the control block, which extends perpendicularly to the longitudinal axis of the control device and at which e.g. the connections of the conductor tracks are arranged for connection to the electronic control unit. In addition, this head part of the cable carrier can be used for the rotation and displacement secure fixing of the cable carrier. For this purpose, the respective tab-shaped head part has at least one bore through which a pin-shaped or screw-shaped fixing element is passed, which is non-positively connected to the end face of the control block facing the cable carrier.
Zur Isolierung des in der Regel aus Metall bestehenden Steuerblockes und den Leiterbahnen des jeweils benachbarten Leitungsträgers ist zwischen der inneren Oberfläche des Steuerblockes und dem benachbarten Leitungsträger ein rohrförmiges Formteil aus einem elektrisch isolierenden Material angeordnet.For isolating the usually made of metal control block and the interconnects of each adjacent cable carrier is arranged between the inner surface of the control block and the adjacent conductor carrier, a tubular molded part made of an electrically insulating material.
Weitere Einzelheiten und Vorteile der Erfindung ergeben sich aus dem folgenden anhand von Figuren erläuterten Ausführungsbeispiel. Es zeigen:
- Fig.1 den Längsschnitt durch eine schematisch dargestellte erfindungsgemäße Querschub-Steuervorrichtung und
- Fig.2 eine vergrößerte Ansicht des in Fig.1 mit II bezeichneten Bereiches.
- 1 shows the longitudinal section through a schematically illustrated inventive shear thrust control device and
- 2 shows an enlarged view of the area designated II in FIG.
In Fig.1 ist mit 1 eine Querschub-Steuervorrichtung bezeichnet, welche beispielsweise in ein nicht dargestelltes ballistisches Geschoß einsetzbar ist, wobei in diesem Fall dann die zentrale Längsachse 2 der Steuervorrichtung 1 mit der Längsachse des entsprechenden Geschosses zusammenfallen.In FIG. 1, 1 designates a transverse thrust control device which can be used, for example, in a ballistic projectile (not shown), in which case the central
Die Querschub-Steuervorrichtung 1 umfaßt einen aus Metall bestehenden Steuerblock 3, in dem mehrere über den Umfang verteilt angeordnete Korrekturtriebwerke 4 in entsprechenden Aufnahmen 5 angeordnet sind. Die Aufnahmen 5 weisen dabei jeweils eine Längsachse 6 auf, die gegenüber einer radialen, die Längsachse 2 des Steuerblocks 3 schneidenden Ebene leicht geneigt angeordnet ist.The lateral thrust control device 1 comprises a
Die im bekannten Korrekturtriebwerke 4 umfassen im wesentlichen ein in die jeweilige Aufnahme 5 einschraubbares Anzündelement 7, einen Treibsatz 8 und eine Düse 9.The known
Das jeweilige Anzündelement 7 besitzt bei dem dargestellten Ausführungsbeispiel zwei Kontaktelemente 10 und 11 (Fig.2). Dabei ist das erste Kontaktelement 10 stabförmig und das zweite Kontaktelement 11 zylinderförmig ausgebildet und umschließt das erste Kontaktelement 10. Das erste Kontaktelement 10 weist außerdem eine größere Länge auf als das zweite Kontaktelement 11.The
Der Steuerblock 3 besitzt eine zentrale axial verlaufende Ausnehmung 12, die zylindrisch oder konisch ausgebildet sein kann und in welcher die Kontaktelemente 10, 11 des jeweiligen Anzündelementes 7 randseitig etwas hineinragen. In der Ausnehmung 12 befinden sich drei ineinandergesteckte, rohrförmige, die Längsachse des Steuerblockes 3 umschließende Formteile 13-15 (Fig.2), die an dem Steuerblock 3 verdreh- und verschiebesicher angeordnet sind.The
Dabei schließt sich direkt an die innere Oberfläche 16 der Ausnehmung 12 des Steuerblocks 13 ein Formteil 13 aus einem elektrisch isolierenden Material, z.B. Kunststoff, an. Innerhalb dieses ersten Formteiles 13 befinden sich die beiden anderen als rohrförmige Leitungsträger ausgebildete Formteile 14 und 15. Jeder dieser beiden Leitungsträger 14, 15 besteht aus einem Formteil aus einem elektrisch isolierenden Material (z.B. Kunststoff) und weist außenseitig Leiterbahnen 17, 18 auf, die jeweils von einem der beiden Kontaktelemente 10, 11 eines Anzündelementes 7 kontaktiert werden.In this case, directly to the
Wie Fig.2 unmittelbar entnehmbar ist, wird beim Einschrauben des Anzündelementes 7 in die Aufnahme 5 das zylinderförmige Kontaktelement 11 durch das erste Formteil 13 hindurchgedrückt und kontaktiert die diesem Kontaktelement 11 zugeordnete erste Leiterbahn 17 des zweiten Formteiles 14 in einem Teilbereich 23. Das stabförmige Kontaktelement 10 des Anzündelementes 7 wird hingegen sowohl durch das erste Formteil 13 als durch das zweite Formteil 14 hindurchgedrückt und kontaktiert die diesem Kontaktelement 10 zugeordnete zweite Leiterbahn 18 des dritten Formteiles 15, wobei die erste Leiterbahn 17 und die zweite Leiterbahn 18 übereinanderliegend angeordnet sind. Damit das erste Kontaktelement 10 nicht ebenfalls die erste Leiterbahn 17 berührt, weist diese Leiterbahn 17 in dem Bereich, in dem das erste Kontaktelement 10 durch den ersten Leitungsträger 14 hindurchgeführt ist, einen ringförmig ausgebildeten, das erste Kontaktelement 10 nicht berührenden Leiterbereich 19 auf.2, the
Zur Positionierung der drei Formteile 13-15 in Umfangsrichtung weisen diese jeweils an ihrem einen Ende ein außerhalb der Ausnehmung 12 des Steuerblockes 3 angeordnetes laschenförmiges Kopfteil 20 auf, welches sich senkrecht zur Längsachse 2 der Steuervorrichtung 1 erstreckt. Das jeweilige Kopfteil 20 stützt sich an einer Stirnfläche 21 des Steuerblockes 3 ab und weist eine Bohrung auf, durch welche als Positionierungselement der Schaft einer Schraube 22 hindurchgeführt ist. Die Schraube 22 bewirkt daher zusätzlich zur Positionierung der Formteile 13-15 in Umfangsrichtung auch eine Fixierung in axialer Richtung.For positioning the three mold parts 13-15 in the circumferential direction, they each have at their one end a tab-
Die Erfindung ist selbstverständlich nicht auf das vorstehend beschriebene Ausführungsbeispiel beschränkt. So kann beispielsweise auf einen der beiden Leitungsträger verzichtet werden, wenn die Anzündelemente jeweils nur ein nach außen geführtes Kontaktelement aufweisen (die jeweils zweite elektrische Verbindung kann dann über Masse erfolgen).Of course, the invention is not limited to the embodiment described above. For example, it is possible to dispense with one of the two conductor carriers if the ignition elements each have only one outwardly guided contact element (the second electrical connection can then be made via ground).
Sofern der Steuerblock aus einem elektrisch isolierenden Material besteht (z.B. aus glasfaserverstärktem Kunststoff), kann auch der erste Formkörper entfallen, da eine Isolierung zwischen der ersten Leiterbahn und der inneren Oberfläche des Steuerblockes nicht erforderlich ist.If the control block is made of an electrically insulating material (for example made of glass fiber reinforced plastic), the first shaped body can also be dispensed with, since insulation between the first conductor track and the inner surface of the control block is not required.
Außerdem ist es auch möglich, bei Verwendung von Anzündelementen mit mehreren Kontaktelementen diese mit benachbarten Leiterbahnen des gleichen Leitungsträgers zu verbinden.Moreover, it is also possible, when using ignition elements with a plurality of contact elements, to connect them to adjacent conductor tracks of the same conductor carrier.
Es ist aber auch möglich, statt einzelner rohrförmiger, konzentrisch angeordneter Isolier- und Kontaktträger eine vorgefertigte Multilayer-Platine zu verwenden. Hierzu wird der Multilayeraufbau vorzugsweise zunächst auf einer planen flexiblen Platine hergestellt und anschließend dann zu einem Rohr umgelegt. Dabei kann die Multilayer-Platine um ein Stützrohr herumgelegt und gegebenenfalls auch an diesem fixiert werden.But it is also possible to use a prefabricated multilayer board instead of individual tubular, concentrically arranged insulating and contact carrier. For this purpose, the multilayer structure is preferably first prepared on a flat flexible circuit board and then then transferred to a tube. In this case, the multilayer board can be wrapped around a support tube and optionally also fixed to this.
Ferner müssen die Längsachsen 6 der Aufnahmen 5 für die Korrekturtriebwerke 4 nicht geneigt ausgebildet sein, sondern können die Längsachse 2 des Steuerblockes 3 auch unter einem rechten Winkel schneiden.Furthermore, the longitudinal axes 6 of the
Zur Lagepositionierung der Leiterbahnen in Umfangsrichtung in bezug auf die Aufnahmen der Anzündelemente des Steuerblockes kann statt der Einbringung von Bohrlöchern in die einzelnen Formteile und den Steuerblock, durch welche anschließend eine Schraube oder ein Stift geführt wird, z.B. auch eine Einfräsung in alle Teile mit einer Paßfeder vorgesehen werden.For positional positioning of the traces in the circumferential direction with respect to the recordings of the ignition of the control block instead of the introduction of boreholes in the individual moldings and the control block through which a screw or pin is then performed, for example, a milled into all parts with a feather key be provided.
Da in Axialrichtung keine großen Kräfte auftreten, kann nach der Positionierung der Formteile in Umfangsrichtung eine einfache Klebung der Formteile an dem Steuerblock ausreichen. Denkbar wäre allerdings auch, z.B. bei dem äußersten Formteil das entsprechende Bohrloch durch einen angespritzten Kunststoffbolzen zu ersetzen, der dann als Preßsitz in dem Bohrloch des Steuerblockes sitzt.Since no large forces occur in the axial direction, a simple adhesion of the molded parts to the control block can be sufficient after the positioning of the molded parts in the circumferential direction. It would also be conceivable, however, for example, to replace the corresponding borehole with a molded-on plastic bolt in the outermost molded part, which then sits as a press fit in the borehole of the control block.
- 11
- (Querschub-) Steuervorrichtung(Transverse thrust) control device
- 22
- (zentrale) Längsachse(central) longitudinal axis
- 33
- Steuerblockcontrol block
- 44
- KorrekturtriebwerkThruster
- 55
- Aufnahmeadmission
- 66
- Längsachselongitudinal axis
- 77
- Anzündelementignition
- 88th
- Treibsatzpropellant
- 99
- Düsejet
- 1010
- (erstes, stabförmiges) Kontaktelement(first, rod-shaped) contact element
- 1111
- (zweites, zylinderförmiges) Kontaktelement(second, cylindrical) contact element
- 1212
- Ausnehmungrecess
- 1313
- (erstes) Formteil(first) molding
- 1414
- (zweites) Formteil, (erster) Leitungsträger(second) molded part, (first) conductor carrier
- 1515
- (drittes) Formteil, (zweiter) Leitungsträger(third) molded part, (second) conductor carrier
- 1616
- innere Oberflächeinner surface
- 1717
- (erste) Leiterbahn, elektrische Leitung(first) trace, electrical line
- 1818
- (zweite) Leiterbahn, elektrische Leitung(second) trace, electrical line
- 1919
- LeiterbereichHead of
- 2020
- Kopfteilheadboard
- 2121
- Stirnflächeface
- 2222
- Schraube, PositionierungselementScrew, positioning element
- 2323
- Teilbereichsubregion
Claims (8)
- Lateral-thrust control apparatus for influencing the flight path of a missile, which has a control block (3) which contains a plurality of holders (5) for corresponding correction motors (4), with an ignition element (7) for the corresponding correction motor (4) being arranged in each of the holders (5), and with each of the ignition elements (7) having at least one contact element (10, 11) which can be connected via an electrical line (17, 18) to an electronic control unit, and with the control block (3) having a central, axially running recess (12) into which the contact element (10, 11) of the respective ignition element (7) which is located in the holder (5) projects, characterized in that at least one tubular line substrate (14, 15) composed of an electrically insulating material is arranged such that it cannot rotate and cannot move laterally in the recess (12) of the control block (3), on which line substrate (14, 15) at least some of the electrical lines (17, 18) are arranged fixed as conductor tracks, in such a manner that the contact element (10, 11) of the respective ignition element (7) makes contact with the conductor track (17, 18) associated with this contact element (10, 11).
- Lateral-thrust control apparatus according to Claim 1, characterized in that, in the case of a control apparatus (1) with ignition elements (7) which each have two contact elements (10, 11) and can be connected via two conductor tracks (17, 18) to an electronic control unit, two line substrates (14, 15) are provided which can be pushed one inside the other and can be fixed in their final position such that they cannot rotate and cannot move laterally on each of which one of the two conductor tracks (17, 18) is arranged firmly such that that respective one contact element (10) of the ignition element (7) makes contact with the first conductor track (17) on the first line substrate (14) adjacent to the ignition element (7), and the respective other contact element (11) of the ignition element (7) is passed through the first line substrate (14) and makes contact with the conductor track (18) on the second line substrate (15).
- Lateral-thrust control apparatus according to Claim 2, characterized in that the two line substrates (14, 15) are fixed within the recess (12) of the control block (3) such that the two conductor tracks (17, 18) which are associated with the respective ignition element (7) are arranged radially adjacent to one another.
- Lateral-thrust control apparatus according to Claim 3, characterized in that the control apparatus (1) has ignition elements (7) which each have a first contact element (10) in the form of a rod and a second, cylindrical contact element (11), which surrounds the contact element (10) in the form of a rod but has a shorter length than the contact element in the form of a rod, in that the respective first conductor track (17), which is adjacent to the inner surface (16) of the recess (12) of the control block (3) and is arranged on the first line substrate (14) of an ignition element (7) makes contact with a subarea of the cylindrical contact element (11) and in that the respective first conductor track (17) has an annular conductor area (19), which does not touch the contact element (10) which is in the form of a rod in the area in which the contact element (10) which is in the form of a rod passes through the first line substrate (14).
- Lateral-thrust control apparatus according to one of Claims 1 to 3, characterized in that the line substrates (14, 15) are plastic mouldings which are each provided at at least one end with a head part (20) which is arranged outside the recess (12) of the control block (3) and becomes broader.
- Lateral-thrust control apparatus according to one of Claims 1 to 5, characterized in that a tubular moulding (13) composed of an electrically insulating material is arranged between the inner surface (16) of the control block (3) and the first line substrate (14), in order to insulate the control block (3) which is composed of metal, and the conductor tracks (17) on the adjacent first line substrate (14).
- Lateral-thrust control apparatus according to one of Claims 1 to 6, characterized in that the line substrates (14, 15) are each parts of a tubular multilayer board.
- Lateral-thrust control apparatus according to Claim 5, characterized in that in order to position the tubular line substrates (14, 15) in the circumferential direction, their head parts (20) each have at least one drilled hole through which at least one positioning element (22), which is in the form of a pin or screw, can be passed, and can be connected to that end surface (21) of the control block (3) which faces the head parts (20).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10354098 | 2003-11-19 | ||
| DE10354098A DE10354098A1 (en) | 2003-11-19 | 2003-11-19 | Lateral-thrust control apparatus |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1533589A1 EP1533589A1 (en) | 2005-05-25 |
| EP1533589B1 true EP1533589B1 (en) | 2007-09-19 |
Family
ID=34428805
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP04023729A Expired - Lifetime EP1533589B1 (en) | 2003-11-19 | 2004-10-05 | Control system using a transversal jet |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US7118065B1 (en) |
| EP (1) | EP1533589B1 (en) |
| AT (1) | ATE373808T1 (en) |
| DE (2) | DE10354098A1 (en) |
| ES (1) | ES2290601T3 (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7416154B2 (en) * | 2005-09-16 | 2008-08-26 | The United States Of America As Represented By The Secretary Of The Army | Trajectory correction kit |
| US7875838B1 (en) * | 2007-04-04 | 2011-01-25 | The United States Of America As Represented By The Secretary Of The Navy | Post boost control power assembly |
| US8362408B2 (en) * | 2009-10-22 | 2013-01-29 | Honeywell International Inc. | Steerable projectile charging system |
| US20140137539A1 (en) * | 2012-11-19 | 2014-05-22 | Raytheon Company | Thrust-producing device with detonation motor |
| US9068808B2 (en) * | 2013-01-17 | 2015-06-30 | Raytheon Company | Air vehicle with bilateral steering thrusters |
| US10914559B1 (en) * | 2016-11-21 | 2021-02-09 | Lockheed Martin Corporation | Missile, slot thrust attitude controller system, and method |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3034434A (en) * | 1960-03-08 | 1962-05-15 | Frank H Swaim | Thrust vector control system |
| US3868883A (en) * | 1964-02-20 | 1975-03-04 | Mc Donnell Douglas Corp | Guidance system |
| US3860199A (en) * | 1972-01-03 | 1975-01-14 | Ship Systems Inc | Laser-guided projectile system |
| DE4036166A1 (en) * | 1990-11-14 | 1992-05-21 | Diehl Gmbh & Co | RAILWAY CORRECTABLE PROJECT |
| DE4408085C2 (en) * | 1994-03-10 | 1999-08-12 | Rheinmetall W & M Gmbh | Device for guiding a missile not rotating about its longitudinal axis |
| DE4410326C2 (en) * | 1994-03-25 | 1998-07-02 | Rheinmetall Ind Ag | Projectile with a device for trajectory correction |
| US6367735B1 (en) * | 2000-02-10 | 2002-04-09 | Quantic Industries, Inc. | Projectile diverter |
| DE10141169A1 (en) * | 2001-08-22 | 2003-03-13 | Diehl Munitionssysteme Gmbh | artillery rocket |
-
2003
- 2003-11-19 DE DE10354098A patent/DE10354098A1/en not_active Withdrawn
-
2004
- 2004-10-05 DE DE502004005009T patent/DE502004005009D1/en not_active Expired - Lifetime
- 2004-10-05 AT AT04023729T patent/ATE373808T1/en active
- 2004-10-05 EP EP04023729A patent/EP1533589B1/en not_active Expired - Lifetime
- 2004-10-05 ES ES04023729T patent/ES2290601T3/en not_active Expired - Lifetime
- 2004-11-18 US US10/990,970 patent/US7118065B1/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| DE10354098A1 (en) | 2005-06-23 |
| EP1533589A1 (en) | 2005-05-25 |
| DE502004005009D1 (en) | 2007-10-31 |
| ES2290601T3 (en) | 2008-02-16 |
| US7118065B1 (en) | 2006-10-10 |
| ATE373808T1 (en) | 2007-10-15 |
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