WO2010149307A2 - Verfahren und vorrichtung zur messung der mündungsgeschwindigkeit eines projektils oder dergleichen - Google Patents

Verfahren und vorrichtung zur messung der mündungsgeschwindigkeit eines projektils oder dergleichen Download PDF

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Publication number
WO2010149307A2
WO2010149307A2 PCT/EP2010/003637 EP2010003637W WO2010149307A2 WO 2010149307 A2 WO2010149307 A2 WO 2010149307A2 EP 2010003637 W EP2010003637 W EP 2010003637W WO 2010149307 A2 WO2010149307 A2 WO 2010149307A2
Authority
WO
WIPO (PCT)
Prior art keywords
projectile
muzzle
launching tube
weapon
coupler
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.)
Ceased
Application number
PCT/EP2010/003637
Other languages
German (de)
English (en)
French (fr)
Other versions
WO2010149307A3 (de
Inventor
Henry Roger Frick
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.)
Rheinmetall Air Defence AG
Original Assignee
Rheinmetall Air Defence AG
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
Priority to CN201080026710.1A priority Critical patent/CN102460060B/zh
Priority to PL10739846T priority patent/PL2446215T3/pl
Priority to DK10739846.3T priority patent/DK2446215T3/da
Priority to EP10739846.3A priority patent/EP2446215B1/de
Priority to JP2012516558A priority patent/JP5654585B2/ja
Priority to ES10739846.3T priority patent/ES2487622T3/es
Priority to CA2764525A priority patent/CA2764525C/en
Application filed by Rheinmetall Air Defence AG filed Critical Rheinmetall Air Defence AG
Publication of WO2010149307A2 publication Critical patent/WO2010149307A2/de
Publication of WO2010149307A3 publication Critical patent/WO2010149307A3/de
Priority to ZA2011/08923A priority patent/ZA201108923B/en
Priority to IL217171A priority patent/IL217171A0/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S11/00Systems for determining distance or velocity not using reflection or reradiation
    • G01S11/02Systems for determining distance or velocity not using reflection or reradiation using radio waves
    • G01S11/023Systems for determining distance or velocity not using reflection or reradiation using radio waves using impedance elements varying with distance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/32Muzzle attachments or glands
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P3/00Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • G01P3/64Devices characterised by the determination of the time taken to traverse a fixed distance
    • G01P3/66Devices characterised by the determination of the time taken to traverse a fixed distance using electric or magnetic means
    • G01P3/665Devices characterised by the determination of the time taken to traverse a fixed distance using electric or magnetic means for projectile velocity measurements

Definitions

  • the invention is concerned with the subject of the construction length reduction of a particular operated as a waveguide weapon nrohres.
  • a waveguide is a tube with a characteristic cross-sectional shape, which has a very good electrically conductive wall. Above all, rectangular and round waveguides are widely used in technology.
  • a method of operating the tube as a circular waveguide and measuring the Doppler velocity of the projectile in the tube can be read in EP 0 023 365 A2.
  • the frequency of the signal is above the cutoff frequency for the respective waveguide mode.
  • the resulting electromagnetic wave propagates in the tube and is reflected by the projectile.
  • a double frequency shift dependent on the instantaneous speed results. From this then a muzzle velocity of the projectile is determined.
  • DE 10 2006 058 375 A1 proposes to use the weapon barrel or the launching tube and / or parts of the muzzle brake as waveguides. However, this waveguide is operated below the cutoff frequency of the respective waveguide mode.
  • the signal generator (eg oscillator) supplies a signal with a constant center frequency, which is below the smallest limit frequency of the waveguide Waveguide is operated.
  • the signal generator generates either a carrier in continuous wave mode (CW mode) or a modulated signal.
  • the invention provides the task to reduce the length of the waveguide or the weapon nrohres can.
  • the invention is based on the idea of shortening the measurement setup by reducing the distance between receiving and transmitting coupler to preferably 0 mm to realize.
  • the implementation of this idea is made more difficult by the fact that, if the coupler falls below a certain distance, individual terms can no longer be determined, but so-called sum fields. This makes it necessary to split these sum fields in order to determine the muzzle velocity V 0 .
  • the source field caused by the transmitting coupler is first measured, that is to say when no projectile is in the waveguide.
  • a characteristic, reflected sum signal results, which is scanned in time in an evaluation device.
  • the information about the speed v 0 of the projectile is included ( ⁇ z (t)), but can not be read directly. Therefore, for the realization of the inventive concept, the induced voltage is measured and subtracted from this the source field. The remaining reflected (electromagnetic) sum field is then divided by software into individual terms, so that several speeds are determined over time. From these, an extremely accurate projectile velocity is then determined by averaging.
  • the oscillator frequency may preferably be in the range between 40 MHz and 80 MHz, but is not set to a specific value itself. For other calibres, other frequency ranges may be provided. This frequency range (40 MHz and 80 MHz) makes it easy to procure components for this frequency range, especially since component tolerances have no influence on the measurement process. In addition, only low electromagnetic emissions are emitted.
  • Fig. 2 shows a measuring device for measuring the projectile speed behind the
  • 3 shows a representation of the sequence of the signal processing of both measuring methods.
  • FIGS. 1 and 2 1 denotes a waveguide or a weapon or launching tube and / or parts of the muzzle brake in which a transmitter coupler 2 is integrated.
  • Fig. 2 is a receiving coupler 4 in the direction of the mouth of the transmitter coupler 2.
  • the transmitting coupler 2 is electrically connected to an oscillator 5.
  • the two receiving couplers 3, 4 are in turn connected to an evaluation device 6.
  • a combination of the arrangement of the two receiving couplers 3, 4 in a measuring arrangement 10 is preferred, but is not required.
  • Shot through the waveguide 1 / gun barrel is a projectile 7 whose velocity is to be measured v 0 . This arrangement is already known from DE 10 2008 024 574.7, to which reference is made here.
  • the terms of the above expression are constant in time, with the individual terms decaying at different speeds in space. If the projectile 7 is removed or approaches the receiving coupler 3, 4, as described in more detail in FIG. 3, an induced voltage U IND is measured.
  • the first term "A" of this formula is constant in time and can be used for calibration, and is preferably measured continuously, but especially shortly before the shot, that is to say when no projectile 7 is still in the waveguide 1. These values are stored continuously, preferably By means of such a calibration, all changes in the constants, which result, for example, from temperature effects in the weapon, are eliminated If, in the case of a shot, the course of the signal U
  • the proposed method allows the distance reduction of transmission 2 and receiving coupler 3, 4 of z k to 0 mm, so that the waveguide can be shortened at least in this area.
  • the transmitting coupler 2 should be able to assume the task of the (r) receiving coupler 3, 4, so that the induced voltage is measured directly at the transmitting coupler 2.
  • the shift register should be sufficiently large. be dimensioned so that, for example, values in measurement intervals of "per second" recorded and thus can be used for the evaluation of all data calibration.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
PCT/EP2010/003637 2009-06-26 2010-06-17 Verfahren und vorrichtung zur messung der mündungsgeschwindigkeit eines projektils oder dergleichen Ceased WO2010149307A2 (de)

Priority Applications (9)

Application Number Priority Date Filing Date Title
PL10739846T PL2446215T3 (pl) 2009-06-26 2010-06-17 Sposób oraz urządzenie do pomiaru prędkości wylotowej pocisku lub tym podobnych
DK10739846.3T DK2446215T3 (da) 2009-06-26 2010-06-17 Fremgangsmåde og indretning til måling af mundingshastigheden af et projektil eller lignende
EP10739846.3A EP2446215B1 (de) 2009-06-26 2010-06-17 Verfahren und vorrichtung zur messung der mündungsgeschwindigkeit eines projektils oder dergleichen
JP2012516558A JP5654585B2 (ja) 2009-06-26 2010-06-17 弾丸などの初速を測定する方法および装置
ES10739846.3T ES2487622T3 (es) 2009-06-26 2010-06-17 Procedimiento y dispositivo para la medición de la velocidad en la boca de un proyectil o similares
CN201080026710.1A CN102460060B (zh) 2009-06-26 2010-06-17 用于测量射弹或类似物的出口速度的方法和设备
CA2764525A CA2764525C (en) 2009-06-26 2010-06-17 Method and device for measuring the muzzle velocity of a projectile or the like
ZA2011/08923A ZA201108923B (en) 2009-06-26 2011-12-05 Method and device for measuring the muzzle velocity of a projectile or the like
IL217171A IL217171A0 (en) 2009-06-26 2011-12-22 Method and device for measuring the muzzle velocity of a projectile or the like

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102009030862A DE102009030862B3 (de) 2009-06-26 2009-06-26 Verfahren und Vorrichtung zur Messung der Mündungsgeschwindigkeit eines Projektils oder dergleichen
DE102009030862.8 2009-06-26

Publications (2)

Publication Number Publication Date
WO2010149307A2 true WO2010149307A2 (de) 2010-12-29
WO2010149307A3 WO2010149307A3 (de) 2011-03-03

Family

ID=42993812

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2010/003637 Ceased WO2010149307A2 (de) 2009-06-26 2010-06-17 Verfahren und vorrichtung zur messung der mündungsgeschwindigkeit eines projektils oder dergleichen

Country Status (11)

Country Link
EP (1) EP2446215B1 (OSRAM)
JP (1) JP5654585B2 (OSRAM)
CN (1) CN102460060B (OSRAM)
CA (1) CA2764525C (OSRAM)
DE (1) DE102009030862B3 (OSRAM)
DK (1) DK2446215T3 (OSRAM)
ES (1) ES2487622T3 (OSRAM)
IL (1) IL217171A0 (OSRAM)
PL (1) PL2446215T3 (OSRAM)
WO (1) WO2010149307A2 (OSRAM)
ZA (1) ZA201108923B (OSRAM)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106526221B (zh) * 2016-11-30 2022-09-23 江苏科技大学 一种次口径子弹的速度测量装置
US10948253B2 (en) * 2017-01-13 2021-03-16 Wilcox Industries Corp. Sensor system for advanced smart weapons barrels
CN109596855B (zh) * 2018-12-27 2020-12-01 西安奇维科技有限公司 一种测试弹体出口初速和加速度的方法
CN112113462B (zh) * 2020-04-24 2023-04-07 南京钧和瑞至电子科技有限公司 直瞄武器射击效果检测方法、系统及虚拟靶标射击系统

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0023365A2 (en) 1979-07-31 1981-02-04 ARES, Inc. Doppler-type projectile velocity measurement apparatus and method
DE102006058375A1 (de) 2006-12-08 2008-06-12 Oerlikon Contraves Ag Verfahren zur Messung der Mündungsgeschwindigkeit eines Projektils oder dergleichen
DE102008024574A1 (de) 2008-05-21 2010-06-17 Rheinmetall Air Defence Ag Vorrichtung und Verfahren zur Messung der Mündungsgeschwindigkeit eines Projektils oder dergleichen

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT389764B (de) * 1988-03-04 1990-01-25 Avl Verbrennungskraft Messtech Verfahren und einrichtung zur bestimmung innenballistischer kenngroessen in rohrwaffen
AT393038B (de) * 1989-08-28 1991-07-25 Avl Verbrennungskraft Messtech Verfahren und einrichtung zur bestimmung von bewegungskenngroessen
US5827958A (en) * 1996-01-05 1998-10-27 Primex Technologies, Inc. Passive velocity data system
US6644111B2 (en) * 2002-02-15 2003-11-11 The United States Of America As Represented By The Secretary Of The Army Apparatus and method for measuring exit velocity of a gun round

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0023365A2 (en) 1979-07-31 1981-02-04 ARES, Inc. Doppler-type projectile velocity measurement apparatus and method
DE102006058375A1 (de) 2006-12-08 2008-06-12 Oerlikon Contraves Ag Verfahren zur Messung der Mündungsgeschwindigkeit eines Projektils oder dergleichen
DE102008024574A1 (de) 2008-05-21 2010-06-17 Rheinmetall Air Defence Ag Vorrichtung und Verfahren zur Messung der Mündungsgeschwindigkeit eines Projektils oder dergleichen

Also Published As

Publication number Publication date
CA2764525A1 (en) 2010-12-29
JP2012530910A (ja) 2012-12-06
ES2487622T3 (es) 2014-08-22
DE102009030862B3 (de) 2010-11-25
JP5654585B2 (ja) 2015-01-14
CN102460060B (zh) 2014-11-05
WO2010149307A3 (de) 2011-03-03
PL2446215T3 (pl) 2015-04-30
EP2446215B1 (de) 2014-06-18
DK2446215T3 (da) 2014-09-01
EP2446215A2 (de) 2012-05-02
CN102460060A (zh) 2012-05-16
CA2764525C (en) 2014-04-22
IL217171A0 (en) 2012-02-29
ZA201108923B (en) 2012-11-28

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