EP2010859A1 - Aufklärungssonde - Google Patents
AufklärungssondeInfo
- Publication number
- EP2010859A1 EP2010859A1 EP07723662A EP07723662A EP2010859A1 EP 2010859 A1 EP2010859 A1 EP 2010859A1 EP 07723662 A EP07723662 A EP 07723662A EP 07723662 A EP07723662 A EP 07723662A EP 2010859 A1 EP2010859 A1 EP 2010859A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- shaft
- housing
- nut
- fixing element
- shaped fixing
- 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.)
- Granted
Links
- 239000000523 sample Substances 0.000 claims description 38
- 230000006835 compression Effects 0.000 claims description 6
- 238000007906 compression Methods 0.000 claims description 6
- 239000007789 gas Substances 0.000 claims description 4
- 238000006073 displacement reaction Methods 0.000 claims description 3
- 230000001419 dependent effect Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/365—Projectiles transmitting information to a remote location using optical or electronic means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B23/00—Land mines ; Land torpedoes
- F42B23/24—Details
Definitions
- the invention relates to a reconnaissance probe which can be brought into a target area as a manually settable or ejectable by a missile load body and detects target-relevant information after placement on the ground.
- Such a probe is known for example from DE 199 06 970 C2. It comprises a housing with a plurality of distributed over the circumference arranged support legs, each about a arranged in the lower region of the housing axis of rotation by means of a pivot drive from a rest position in which they are arranged approximately parallel to the longitudinal axis of the housing, in an unfolded position at they are hinged to the outside substantially radially to the longitudinal axis of the housing, are pivotable.
- the support legs When the probe is brought into the target area, the support legs are in their rest position, and then, after the impact of the probe on the ground, are folded by the pivot drive into its deployed position.
- the reconnaissance probe is brought into the target area with a spin-stabilized carrier projectile (eg with a 155 mm artillery projectile), the probe generally still has a certain twist after it has been ejected from the carrier projectile.
- a locking device is provided, which holds the support legs to the impact of the probe on the ground in its rest position and only then the opening process of Support legs permits.
- the invention has for its object to provide a reconnaissance probe with a locking device which holds the support legs in their rest position until they are released at a defined time, for example by an electrical signal for erecting the probe.
- the invention is based essentially on the idea of holding the support legs in their rest position by a over the outer circumference of the housing extending band-shaped fixing element of the locking device in position.
- at least one end region of the fixing element is wound on a shaft rotatable about its longitudinal axis, extending in the interior of the housing or in its side wall parallel to the longitudinal axis of the housing frictionally, wherein the band-shaped fixing element is guided through a slot-shaped recess of the side wall to the shaft.
- a co-operating with the shaft controllable locking device is provided which prevents rotation of the shaft and thus unwinding of the band-shaped fixing element and thus unfolding of the support legs in the locking position of the locking device and in the unlocked position of the locking device rotation of the shaft and thus a Unfolding the support legs made possible by means of the rotary actuators.
- the pivot drives of the support legs may preferably each be a leg spring biased in the rest position of the support legs.
- both end regions of the band-shaped fixing element are wound on the shaft in a frictional engagement in the rest position of the support legs.
- the shaft has a slot extending in the axial direction for receiving the end region or regions of the band-shaped fixing element, wherein the slot width is selected such that a clamping of the End region of the band-shaped fixing element takes place in the shaft.
- the band-shaped fixing element may for example consist of plastic or a fabric.
- the locking device comprises a relative to the housing rotatable and displaceable in the direction of the longitudinal axis of the shaft against the pressure of a compression spring nut with an internal toothing, wherein for axial displacement of the nut an actuating device is provided such that in the locked position the shaft engages with a corresponding external toothing in the internal toothing of the nut and in the unlocked position the external toothing of the shaft and the internal toothing of the nut are disengaged.
- For rotationally fixed and axially displaceable arrangement of the nut may have internal teeth within the housing, which engages in an external toothing of the nut.
- the actuating device of the locking device may consist of a cylindrical housing in which a piston which can be acted upon by the gases of a pyrotechnic element is displaceably arranged, which is guided through the cylindrical housing on the front side and is supported on the end face of the shaft facing the nut.
- the cylindrical housing is supported with its side facing away from the shaft on a wall part of the mother, so that upon ignition of the pyrotechnic element, the piston presses against the end face of the shaft and thus the mother shifts so far that the internal teeth of the nut and the external teeth the shaft are disengaged.
- the mother can be designed in several parts to simplify their production and for the exact positioning of the actuator.
- a first female part is provided with the outer and the inner thread.
- a second female part connected to the first female part by a screw connection receives the actuator.
- Fig.l is a perspective view of a reconnaissance probe according to the invention shortly after hitting the ground, wherein the support legs of the probe are still held by a locking device with a band-shaped fixing in its rest position;
- FIG. 2 shows a perspective view of the reconnaissance probe shown in FIG. 1 after unfolding the support legs;
- FIG. 3 shows a section through the designated in Fig.l III-III wall portion of the housing with a shaft mounted therein, which holds the band-shaped fixing element;
- FIG. 4 shows a partially sectioned side view of the shaft shown in Figure 3 with a rotation of the shaft about its longitudinal axis inhibiting or releasing latching device and with a locking device controlling actuator, for clarity, the band-shaped fixing element is omitted.
- FIG. 5 shows a longitudinal section through the designated in Figure 4 with 16 actuator.
- Fig.l and 2 1 denotes a reconnaissance probe, for example, from a carrier projectile (not shown) spent over a target area, was dropped there and then reaches the earth by means of a parachute, not shown.
- curved support legs 2 pivoted about arranged in the lower part of the housing 3 of the reconnaissance probe 1 axes of rotation 4 by means of torsion springs 5 from its rest position to a deployed position Fig.2) to raise the reconnaissance probe 1 and then to ensure a secure state of the probe 1 on the ground.
- torsion springs 5 After unfolding the support legs 2, five evenly distributed over the outer circumference of a housing arranged sensor carrier 6 are released, which are each pivoted about a located in the upper region of the housing 3 axis of rotation to the outside.
- the locking device 7 comprises e.g. made of plastic band-shaped fixing element 8, which extends over the outer circumference of the housing 3 and the support legs 2 holds after ejection from the carrier projectile in its rest position.
- the two end portions 9, 10 of the fixing element 8 on a rotatable about its longitudinal axis 11, arranged in the interior of the side wall 12 of the housing 3 and parallel to the longitudinal axis 13 of the housing 3 extending shaft 14 frictionally wound (Figure 3), wherein the band-shaped fixing element 8 is guided through a slot-shaped recess 15 of the side wall 12 to the shaft 14.
- the shaft 14 in turn has a slot 37 through which the two end portions 9, 10 of the fixing element 8 are passed and whose width is chosen such that a clamping of the end portions 9, 10 of the band-shaped fixing element 8 in the shaft 14 takes place.
- the latching device 16 comprises a relative to the housing 3 of the reconnaissance probe first rotatably and in the direction of the longitudinal axis 11 of the shaft 14 against the pressure of a compression spring 35 displaceable multi-part nut 17.
- a shaft 14 adjacent the first female part 18 is provided with a spline having internal teeth 19, in which a provided in a portion of the shaft 14 External teeth 20 engages ( Figure 4).
- this first female part 18 also has a spline 21 provided with external teeth 21, which engages in a corresponding internal toothing 22 of the housing 3.
- second female part 24 receives a provided for the axial displacement of the nut 17, electrically controllable actuator 25.
- the second nut part 24 is closed on the bottom side by a bottom part 26 on which the compression spring 35 is supported.
- the second nut member 24 on its side facing the shaft 14 on an axial opening 27 for the passage of a piston 28 of the actuator 25 on.
- the structure of the actuator 25 can be seen in Fig.5.
- it consists of a cylindrical housing 29, in which the acted upon by the gases of an electrically ignitable pyrotechnic element 30 piston 28 is slidably disposed.
- the cylindrical housing 29 on the front side an opening 31 through which the piston 28 can be pushed.
- the cylindrical housing 29 On its side facing away from the shaft 14, the cylindrical housing 29 is supported on the inside on the bottom part 26 of the nut 17.
- the pyrotechnic element 30 of the actuator 25 is ignited after striking the reconnaissance probe 1 on the ground by means of an electrical pulse, the forming propellant gases push the piston 28 in the direction of the end face 36 of the shaft 14. Since this is mounted axially immovable, pushes the cylindrical housing 29 of the actuator 25 against the bottom part 26 of the nut 17 and moves it against the pressure of the compression spring 35 of the shaft 14 away.
- the shaft 14 is freely rotatable, and the support legs 2 are pivoted by the prestressed leg springs 5 to the outside and thereby pull the band-shaped fixing element 8 also to the outside.
- the invention is not limited to the embodiment described above. It may be sufficient, for example, if not both end portions of the band-shaped fixing element are connected to the shaft, but only one end portion and the second end portion is fixedly connected to the housing. However, this requires appropriately prestressed torsion springs or another pivot drive for opening the support legs.
- the locking device can also be realized only by a one-piece, axially displaceable nut or it can be used instead of a nut, for example, a radially displaceable locking pin or sprocket portion which engages in corresponding grooves or in a toothed ring mounted on the shaft.
- the reconnaissance probe does not necessarily have to be a probe that can be brought into the target area by a missile, but the probe can also be placed manually in the target area, for example, with the reconnaissance probe being thrown from a vehicle or from a correspondingly low-flying helicopter becomes.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Clamps And Clips (AREA)
- Telescopes (AREA)
- Dry Shavers And Clippers (AREA)
- Reverberation, Karaoke And Other Acoustics (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
- Geophysics And Detection Of Objects (AREA)
- Aerials With Secondary Devices (AREA)
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102006019212A DE102006019212A1 (de) | 2006-04-21 | 2006-04-21 | Aufklärungssonde |
| PCT/EP2007/002716 WO2007121820A1 (de) | 2006-04-21 | 2007-03-28 | Aufklärungssonde |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2010859A1 true EP2010859A1 (de) | 2009-01-07 |
| EP2010859B1 EP2010859B1 (de) | 2010-08-25 |
Family
ID=38222421
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP07723662A Not-in-force EP2010859B1 (de) | 2006-04-21 | 2007-03-28 | Aufklärungssonde |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP2010859B1 (de) |
| AT (1) | ATE479072T1 (de) |
| DE (2) | DE102006019212A1 (de) |
| ES (1) | ES2348267T3 (de) |
| WO (1) | WO2007121820A1 (de) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4105530A1 (de) * | 1990-02-23 | 1991-08-29 | Dynamit Nobel Ag | Mine mit definierter wirkrichtung |
| US5069136A (en) * | 1990-09-14 | 1991-12-03 | Honeywell Inc. | Two-stage release mechanism and method for self-righting a load |
| JP3349736B2 (ja) * | 1992-12-08 | 2002-11-25 | 防衛庁技術研究本部長 | 自動起立式弾薬 |
| DE19906970C2 (de) * | 1999-02-19 | 2003-03-27 | Rheinmetall W & M Gmbh | Aufklärungssonde |
| DE10331909A1 (de) * | 2003-07-04 | 2005-01-20 | Rheinmetall W & M Gmbh | ABC-Sensoreinrichtung |
-
2006
- 2006-04-21 DE DE102006019212A patent/DE102006019212A1/de not_active Withdrawn
-
2007
- 2007-03-28 ES ES07723662T patent/ES2348267T3/es active Active
- 2007-03-28 DE DE502007004863T patent/DE502007004863D1/de active Active
- 2007-03-28 AT AT07723662T patent/ATE479072T1/de active
- 2007-03-28 EP EP07723662A patent/EP2010859B1/de not_active Not-in-force
- 2007-03-28 WO PCT/EP2007/002716 patent/WO2007121820A1/de not_active Ceased
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2007121820A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| ES2348267T3 (es) | 2010-12-02 |
| DE102006019212A1 (de) | 2007-10-25 |
| EP2010859B1 (de) | 2010-08-25 |
| WO2007121820A1 (de) | 2007-11-01 |
| ATE479072T1 (de) | 2010-09-15 |
| DE502007004863D1 (de) | 2010-10-07 |
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