EP1102023A2 - Dispositif de refoulement pour canon d'artillerie - Google Patents

Dispositif de refoulement pour canon d'artillerie Download PDF

Info

Publication number
EP1102023A2
EP1102023A2 EP00123207A EP00123207A EP1102023A2 EP 1102023 A2 EP1102023 A2 EP 1102023A2 EP 00123207 A EP00123207 A EP 00123207A EP 00123207 A EP00123207 A EP 00123207A EP 1102023 A2 EP1102023 A2 EP 1102023A2
Authority
EP
European Patent Office
Prior art keywords
projectile
linear motor
carriage
gun barrel
projectile according
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
Application number
EP00123207A
Other languages
German (de)
English (en)
Other versions
EP1102023B1 (fr
EP1102023A3 (fr
Inventor
Rüdiger Dipl.-Ing. Baus
Thomas Dr. Kneisel
Karl Ing. Grad Lieberum
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
KNDS Deutschland GmbH and Co KG
Original Assignee
Krauss Maffei Wegmann GmbH and Co KG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP1102023A2 publication Critical patent/EP1102023A2/fr
Publication of EP1102023A3 publication Critical patent/EP1102023A3/fr
Application granted granted Critical
Publication of EP1102023B1 publication Critical patent/EP1102023B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/38—Loading arrangements, i.e. for bringing the ammunition into the firing position
    • F41A9/39—Ramming arrangements
    • F41A9/42—Rammers separate from breech-block

Definitions

  • the invention relates to a projectile rifle for artillery with the features from the preamble of claim 1.
  • Such a projectile projector also referred to as a "free-flight projector” is described for example in EP 0 352 584 A2.
  • the principle of the free flight pawn is that one outside the Armory located floor so high speed is that this is due to leaving the acceleration system the kinetic energy caused by the acceleration outdoors Flight moves on and the attachment process is realized in this way.
  • the in the abovementioned publication, such as, for example, also in CH 664 627 described free flight attachments have a sled system for acceleration, where the projectile, including the Sled is accelerated and when the required preparation speed is reached the sled is braked. The projectile then flies through the bottom piece in the cargo space of the weapon and is in the trains of the Gun barrel attached.
  • Free-flight attachments are also known which have spring-loaded actuators, for example, coil springs that are preloaded by an electric motor or use gas springs that are triggered mechanically during the attachment process and the stored energy via downstream machine components (Chains, racks) on the projectile or the attachment slide transfer.
  • spring-loaded actuators for example, coil springs that are preloaded by an electric motor or use gas springs that are triggered mechanically during the attachment process and the stored energy via downstream machine components (Chains, racks) on the projectile or the attachment slide transfer.
  • the invention has for its object a projectile for artillery with the input and specified in the preamble of claim 1
  • a projectile for artillery with the input and specified in the preamble of claim 1
  • the invention is based on the knowledge that the implementation of such Drive device by driven by conventional electric motors Systems to implement the necessary for the moment of the start-up process high electrical energy in the translatory carriage movement fails.
  • As a result of the implementation of the rotary motion of a conventional Electric motor in the translatory carriage movement push the for this Machine elements known in mechanical engineering (chains, spindles, gears, Racks) due to the inertial forces occurring during acceleration and the high application speeds to the limits of their resilience.
  • mechanical engineering chains, spindles, gears, Racks
  • the basic idea of the invention is therefore, instead of the known, designed as a piston-cylinder drive device electric linear motor to use.
  • Linear motors allow direct Generation of linear movements without the interposition of gears.
  • the drive device designed as a linear motor is that in the opposite approach to the piston-cylinder drive, its Thrust developed to the end of the acceleration stroke, the acceleration process and a possible braking process with the linear motor is very precisely controllable.
  • the linear motor can therefore develop an additional braking force, which are taken into account when designing the means for braking the sled can be.
  • the electrical supply of the linear motor can be done in one Combat vehicle arranged gun from a powered by the electrical system Battery buffers take place.
  • Short-term storage can be used to have high electrical power available whose capacity is designed for a piecing process. It is also possible to use one attached to the attachment slide electrical measuring system to monitor the course of the preparation process and Via a control system, the delivery of the electrical power to the linear motor to control.
  • Fig. 1 shows the rear end of the gun barrel 1 not otherwise shown artillery gun, on which the bottom piece 1.1 is arranged.
  • a pivotable about the shield pin axis S is Storey transfer arm 2 arranged, a carrier at its outer end 3 carries, on which a projectile is arranged.
  • a guideway 4.3 is attached, on which a roller guide 4.1 Carriage 4 is guided in the direction parallel to the tube core axis R.
  • a shell-like engagement element 4.2 as a driver for the lying on the sled in a receiving trough 4.4 Floor G.
  • the stop 7.1 in the end position of the carriage 4 shown in Fig. 2 at the rear end of Gun barrel is applied.
  • the carriage 4 thus moves during the attachment process from the rest position shown in FIG. 1 to the end position shown in FIG. 2, in Fig. 2 the beginning of the end position with solid lines and the after retraction of the shock absorber 7 final end position shown in dashed lines is.
  • the projectile moves during and after braking of the carriage 4 G in free flight into gun barrel 1.
  • the drive device for accelerating the carriage 4 has in the in 1 to 3 embodiment shown an electric linear motor on with an elongated flat, between the carrier 3 and the Carriage 4 fixed primary part 5, which in one in Figs. 1 and 2 not shown way connected to the electrical supply device is.
  • the movable secondary part 6 of the linear motor is an elongated flat Component formed and consists of ferromagnetic material, for example made of iron with a magnetic track 6.1.
  • the secondary part 6 runs over the flat lying primary part 5. With this arrangement, a pulling force occurs twice the maximum feed force between the primary and secondary part on, which must be transmitted by the slide guide 4.1-4.3.
  • the Space for the shock absorber, not shown, is designated in Fig. 3 with 7.2.
  • Fig. 4 shows a drive device equipped with two linear motors is. 4, which correspond to corresponding components from FIG. 3, are identified by the same reference number and an apostrophe.
  • the slide 4 ' is via a linear guide 4.1' in a central guide rail 4.3 'out.
  • the primary parts 5.1 'and 5.2'der Linear motors are fixed on both sides of the slide 4 'in the carrier 3'.
  • the primary parts 5.1 'and 5.2' are opposite to the two Sides of the slide, which are designed as outward-pointing components, Secondary parts 6.1 'and 6.2' made of ferromagnetic material arranged, each carrying a magnetic track 6.1 'or 6.1 ".
  • Primary and Secondaries are here in the vertical direction and opposite each other aligned. With this arrangement, the tightening forces compensate each other by arranging the primary and secondary parts in pairs. However, you are still present within the structure of the carriage 4 'so that a very rigid sled structure must be realized. It also arises due to the arrangement in pairs a somewhat increased construction effort.
  • the slide length can be shortened to the length of the secondary part be, which results in a weight reduction.
  • the charging cradle 4.4 or 4.4 'arranged on the slide 4 or 4' can be achieved that the front end of the charging cradle when braking of the carriage into the cargo space of the weapon (Fig. 2 dashed Presentation). Through this measure, the exit behavior of the floor G noticeably at the moment of the "departure" from the attachment slide 4 improved.
  • An electrical supply device for those shown in FIGS. 1 to 4 Fig. 5 shows the drive devices of the projectile attachment.
  • the supply device owns one, for example, of the combat vehicle's electrical system connected battery buffer 9.
  • battery buffer 9 For as synchronous machines trained linear motors must the existing DC voltage on the for the operation of the linear motor or the linear motors required AC voltage be reshaped. This is done by means of a to the battery buffer 9 connected inverters 8.
  • the converter 8 contains high electrical power a short-term memory 8.1, the capacity of which is designed for a preparation process is.
  • An electrical measuring system 10 attached to the attachment slide 4 or 4 ′ monitors the course of the preparation process and controls it via a control system 11 targeted the delivery of electrical power from the short-term storage 8.1 to the primary part 5 of the linear motor.
  • the regulation can be carried out according to any predefinable control characteristic which the sled accelerates in the various movement phases or is slowed down.
  • FIG. 6 shows the path-time profile of the attachment slide in an exemplary manner during the application process with an acceleration phase, a braking phase, a rest phase and a rewind phase.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Linear Motors (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Manufacturing Of Micro-Capsules (AREA)
  • Control Of Electric Motors In General (AREA)
  • Hard Magnetic Materials (AREA)
EP00123207A 1999-11-17 2000-10-26 Dispositif de refoulement pour canon d'artillerie Expired - Lifetime EP1102023B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19955234 1999-11-17
DE19955234A DE19955234A1 (de) 1999-11-17 1999-11-17 Geschoßansetzer für Artillerie

Publications (3)

Publication Number Publication Date
EP1102023A2 true EP1102023A2 (fr) 2001-05-23
EP1102023A3 EP1102023A3 (fr) 2002-02-06
EP1102023B1 EP1102023B1 (fr) 2005-11-16

Family

ID=7929307

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00123207A Expired - Lifetime EP1102023B1 (fr) 1999-11-17 2000-10-26 Dispositif de refoulement pour canon d'artillerie

Country Status (6)

Country Link
US (1) US6467389B1 (fr)
EP (1) EP1102023B1 (fr)
AT (1) ATE310223T1 (fr)
DE (2) DE19955234A1 (fr)
ES (1) ES2251340T3 (fr)
PL (1) PL193246B1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103776296A (zh) * 2014-01-17 2014-05-07 中国船舶重工集团公司第七一〇研究所 多功能手动装退弹推杆
FR3123977A1 (fr) * 2021-06-15 2022-12-16 Nexter Systems Dispositif de mise a poste d'un projectile

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005003672A1 (fr) * 2003-07-02 2005-01-13 Denel (Pty) Ltd Ensemble de chargement de munitions
FR2945616B1 (fr) * 2009-05-13 2011-07-29 Nexter Systems Dispositif de chargement d'une munition
DE102014017554B4 (de) * 2014-11-28 2021-12-23 Thyssenkrupp Ag Vorrichtung zum Ausstoßen eines Objekts aus einem Waffenrohr mit einem Linearmotor
DE102019203071B4 (de) * 2019-03-06 2022-04-28 Thyssenkrupp Ag Brückenlose Waffenmulde
DE102019211285B3 (de) * 2019-07-30 2020-09-24 Thyssenkrupp Ag Waffenbrücke
US12173981B2 (en) 2021-10-13 2024-12-24 Moab Ventures Llc Launching system for an air gun

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH664627A5 (de) 1986-11-20 1988-03-15 Sig Schweiz Industrieges Beschleunigungseinrichtung fuer eine ladevorrichtung eines geschuetzes.
EP0352584A2 (fr) 1988-07-28 1990-01-31 Wegmann & Co. GmbH Refouloir de projectiles pour artillerie

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1595414A (fr) * 1968-12-19 1970-06-08
DE2455994C3 (de) * 1974-11-27 1980-01-10 Mak Maschinenbau Gmbh, 2300 Kiel Vorrichtung zum Ausstoßen bzw. Ablaufen von Tauch- und Schwimmkörpern aus Rohren
DE2460507C3 (de) * 1974-12-20 1979-12-06 Walter 6600 Saarbruecken Landsrath Schießgerät für in einem Rohr zu beschleunigende Geschosse
DE3208941C2 (de) * 1982-03-12 1985-10-10 Rheinmetall GmbH, 4000 Düsseldorf Vorrichtung zum Übertragen von Energie auf den Verschlußkörper eines Geradzugverschlusses einer automatischen Rohrwaffe
US4555972A (en) * 1982-12-20 1985-12-03 Westinghouse Electric Corp. Electromagnetic launcher with powder driven projectile insertion
US4791850A (en) * 1986-01-23 1988-12-20 Minovitch Michael Andrew Electromagnetic launching system for long-range guided munitions
DE3644513C1 (de) * 1986-12-24 1992-08-27 Dornier Gmbh Munitionszufuehrung
DE3940421A1 (de) * 1989-12-07 1991-06-13 Wegmann & Co Vorrichtung zur zufuehrung von treibladungen fuer rohrwaffen groesseren kalibers

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH664627A5 (de) 1986-11-20 1988-03-15 Sig Schweiz Industrieges Beschleunigungseinrichtung fuer eine ladevorrichtung eines geschuetzes.
EP0352584A2 (fr) 1988-07-28 1990-01-31 Wegmann & Co. GmbH Refouloir de projectiles pour artillerie

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103776296A (zh) * 2014-01-17 2014-05-07 中国船舶重工集团公司第七一〇研究所 多功能手动装退弹推杆
CN103776296B (zh) * 2014-01-17 2015-06-10 中国船舶重工集团公司第七一〇研究所 多功能手动装退弹推杆
FR3123977A1 (fr) * 2021-06-15 2022-12-16 Nexter Systems Dispositif de mise a poste d'un projectile
EP4105591A1 (fr) * 2021-06-15 2022-12-21 NEXTER Systems Dispositif de mise à poste d'un projectile

Also Published As

Publication number Publication date
ES2251340T3 (es) 2006-05-01
EP1102023B1 (fr) 2005-11-16
US6467389B1 (en) 2002-10-22
PL193246B1 (pl) 2007-01-31
DE19955234A1 (de) 2001-05-23
EP1102023A3 (fr) 2002-02-06
DE50011622D1 (de) 2005-12-22
PL343880A1 (en) 2001-05-21
ATE310223T1 (de) 2005-12-15

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