EP1798513A1 - Anti-Rückschlag Verriegelungsvorrichtung für Geschoss mit entrollbare Flossen - Google Patents
Anti-Rückschlag Verriegelungsvorrichtung für Geschoss mit entrollbare Flossen Download PDFInfo
- Publication number
- EP1798513A1 EP1798513A1 EP06291898A EP06291898A EP1798513A1 EP 1798513 A1 EP1798513 A1 EP 1798513A1 EP 06291898 A EP06291898 A EP 06291898A EP 06291898 A EP06291898 A EP 06291898A EP 1798513 A1 EP1798513 A1 EP 1798513A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- groove
- tongue
- fin
- projectile
- support
- 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
- 239000000463 material Substances 0.000 claims abstract description 9
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 4
- 239000010959 steel Substances 0.000 claims abstract description 4
- 238000013016 damping Methods 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 abstract description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 3
- 230000000087 stabilizing effect Effects 0.000 description 3
- 238000010304 firing Methods 0.000 description 2
- 241000272517 Anseriformes Species 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Images
Classifications
-
- 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
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- F42B10/16—Wrap-around fins
-
- 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
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
Definitions
- the technical field of the invention is that of devices for locking the deployable surfaces of projectiles, such as wings, control surfaces or fins.
- stabilization fins projectiles fired by a smooth-bore gun.
- the fins are during firing supported along an outer surface of the projectile or they fit into radial housings. They deploy at the exit of the barrel of the weapon to ensure their stabilizing function.
- the patent FR-2860577 thus describes a device for deploying such fins.
- the fins Once deployed the fins must occupy a reliable position and remain in this position. The absence of rebounds is also sought because the existence of a rebound delays the moment when the fin starts to be aerodynamically efficient.
- the locking of the fins is an essential function to ensure at the end of opening. Note that in the case of ducks, non-locking is a catastrophic event.
- FR-2860577 proposes an opening made in a block relative to which pivots the fin, opening which receives an end of a rod carrying the fin.
- the invention aims to provide a simple and reliable device that prevents rebound of the fin and which also ensures its locking end of the race.
- the efficiency and reliability of the device are all the more important that the kinetic energy of the blade is high and in particular the speed of opening.
- the device does not affect the deployment movement itself, which guarantees the final position of the fin and notably avoids the risk (encountered with certain known devices) of stopping the fin before it is fully deployed.
- the subject of the invention is a device for locking a deployable surface or wing of a projectile, a wing mounted pivoting and positioned in a deployed position in a radial groove of the projectile, characterized in that it comprises at least one flexible tongue whose one end is projecting into the groove, a lateral clearance to the groove allowing a flexion of the tongue in a first direction to allow the entry of the fin in the groove.
- the width of the groove and the length of the tongue will be chosen so that the tongue plates by buttressing the fin on one face of the groove.
- the groove may be carried by a support, the tongue being held by a block partially delimiting the lateral clearance, the tongue being clamped between the block and the support.
- the tongue may be constituted by a steel sheet.
- the bottom of the groove may carry a damping material.
- the support may comprise at least two elements arranged on either side of the groove, one of the two elements being made of a plastic material and having an extension constituting the bottom of the groove.
- a projectile 1 has at its rear a plurality of wings 2 deployable of which only one is shown here.
- the fin is in the folded position resting flat along the body of the projectile 1 and is oriented substantially along the axis 3 of the projectile. It pivots during firing through a deployment mechanism 4 which is not described in detail because it is not the subject of the present invention.
- This deployment mechanism may be similar to that described in the patent FR2860577 which can be referred to for more details.
- a rear part 5 thereof When the fin is deployed, a rear part 5 thereof enters a radial groove 6 arranged on a support 7 integral with the body of the projectile 1.
- the support 7 is more particularly visible in FIG.
- the support 7 comprises two elements 8 and 9 which are arranged on either side of the groove 6. These elements will be secured to the body of the projectile 1, for example by screws (not shown).
- One of the two elements (the element 8) is made of a plastic material and it comprises an extension 10 which constitutes the bottom of the groove 6.
- the element 9 is made of metal (for example aluminum). It has a clearance 11 at its upper part.
- a tongue 12 is fixed to the element 9.
- This tongue is constituted for example by a steel sheet of a few tenths of a millimeter thick with sharp edges.
- the tongue 12 is pinched between the element 9 and a block 13 made for example of aluminum.
- connection between the tongue 12, the element 9 and the block 13 can be likened to a perfect embedding that allows no sliding or pivoting of the tongue 12.
- the tongue 12 Because of its material and its thickness the tongue 12 has a certain flexibility. It can flex at the passage of the fin in the direction of the opening without opposing resistance and remaining in a field of elastic deformation.
- the clearance 11, lateral to the groove 6, allows a flexion of the tongue 12 in the direction I which allows to create the bracing of the mechanism, which prohibits the rise of the fin in a direction E inverse in the first sense I.
- FIG. 3 shows the fin 2 engaged in the groove 6.
- the fin 2 When entering the groove 6, the fin 2 pushes easily the tongue 12 which flexes without effort and freely deforms in the clearance 11 and thus passes the fin 2.
- the adhesion force of the fin 2 on the face 6a is greater than the external forces that tend to raise the fin.
- the fin 2 is thus firmly locked by the adhesive force at the face 6a, and following the principle of bracing.
- the device is all the more effective as the external forces are important.
- the rebound of the fin is therefore impossible, any return back being prohibited by the tongue 12.
- the locking of the fin 2 is immediate, reliable and play-free, and the fin can not leave its groove.
- a damping material for example a rubber layer
- stabilizing fins have here been taken as an example to describe the invention. It is understood that the invention can be applied to other types of deployable surfaces (control surfaces, wings ).
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Vibration Dampers (AREA)
- Lock And Its Accessories (AREA)
- Optical Couplings Of Light Guides (AREA)
- Braking Arrangements (AREA)
- Railway Tracks (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0513202A FR2895071B1 (fr) | 2005-12-19 | 2005-12-19 | Dispositif de verrouillage anti-rebond d'une ailette deployable d'un projectile. |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1798513A1 true EP1798513A1 (de) | 2007-06-20 |
EP1798513B1 EP1798513B1 (de) | 2008-07-23 |
Family
ID=36950391
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06291898A Active EP1798513B1 (de) | 2005-12-19 | 2006-12-11 | Anti-Rückschlag Verriegelungsvorrichtung für Geschoss mit entrollbarer Flosse |
Country Status (5)
Country | Link |
---|---|
US (1) | US7919739B2 (de) |
EP (1) | EP1798513B1 (de) |
AT (1) | ATE402390T1 (de) |
DE (1) | DE602006001927D1 (de) |
FR (1) | FR2895071B1 (de) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7829830B1 (en) * | 2007-10-19 | 2010-11-09 | Woodward Hrt, Inc. | Techniques for controlling access through a slot on a projectile |
FR3041744B1 (fr) * | 2015-09-29 | 2018-08-17 | Nexter Munitions | Projectile d'artillerie ayant une phase pilotee. |
FR3071917B1 (fr) | 2017-10-04 | 2021-11-19 | Nexter Munitions | Dispositif de blocage d'ailette et projectile comportant un tel dispositif |
KR102088240B1 (ko) * | 2018-11-14 | 2020-03-12 | 주식회사 경인테크 | 수납 및 분리가 용이한 유도 포탄용 조종날개 구동장치 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1563271A (de) * | 1967-07-11 | 1969-04-11 | ||
US4709878A (en) * | 1984-04-17 | 1987-12-01 | British Aerospace Plc | Fin assembly deployment spring |
DE4017504A1 (de) * | 1989-06-02 | 1993-07-15 | British Aerospace | Entfaltungssystem fuer stromlinienfluegel |
DE19941557C1 (de) | 1999-09-01 | 2001-04-26 | Rheinmetall W & M Gmbh | Flugkörper |
DE19941555C1 (de) | 1999-09-01 | 2001-05-03 | Rheinmetall W & M Gmbh | Flugkörper |
FR2860577A1 (fr) | 2003-10-06 | 2005-04-08 | Giat Ind Sa | Dispositif de deploiement d'une ailette d'un projectile |
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-
2005
- 2005-12-19 FR FR0513202A patent/FR2895071B1/fr not_active Expired - Fee Related
-
2006
- 2006-12-11 EP EP06291898A patent/EP1798513B1/de active Active
- 2006-12-11 AT AT06291898T patent/ATE402390T1/de not_active IP Right Cessation
- 2006-12-11 DE DE602006001927T patent/DE602006001927D1/de active Active
- 2006-12-18 US US11/640,171 patent/US7919739B2/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1563271A (de) * | 1967-07-11 | 1969-04-11 | ||
US4709878A (en) * | 1984-04-17 | 1987-12-01 | British Aerospace Plc | Fin assembly deployment spring |
DE4017504A1 (de) * | 1989-06-02 | 1993-07-15 | British Aerospace | Entfaltungssystem fuer stromlinienfluegel |
DE19941557C1 (de) | 1999-09-01 | 2001-04-26 | Rheinmetall W & M Gmbh | Flugkörper |
DE19941555C1 (de) | 1999-09-01 | 2001-05-03 | Rheinmetall W & M Gmbh | Flugkörper |
FR2860577A1 (fr) | 2003-10-06 | 2005-04-08 | Giat Ind Sa | Dispositif de deploiement d'une ailette d'un projectile |
Also Published As
Publication number | Publication date |
---|---|
EP1798513B1 (de) | 2008-07-23 |
FR2895071B1 (fr) | 2008-01-18 |
DE602006001927D1 (de) | 2008-09-04 |
FR2895071A1 (fr) | 2007-06-22 |
US7919739B2 (en) | 2011-04-05 |
ATE402390T1 (de) | 2008-08-15 |
US20070138335A1 (en) | 2007-06-21 |
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