EP0184564A1 - Practice target - Google Patents

Practice target Download PDF

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Publication number
EP0184564A1
EP0184564A1 EP85850282A EP85850282A EP0184564A1 EP 0184564 A1 EP0184564 A1 EP 0184564A1 EP 85850282 A EP85850282 A EP 85850282A EP 85850282 A EP85850282 A EP 85850282A EP 0184564 A1 EP0184564 A1 EP 0184564A1
Authority
EP
European Patent Office
Prior art keywords
signal
practice target
target according
processing unit
sensing member
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.)
Withdrawn
Application number
EP85850282A
Other languages
German (de)
English (en)
French (fr)
Inventor
Hakan Arbrandt
Jan Brunstedt
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.)
Norabel AB
Original Assignee
Norabel AB
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 Norabel AB filed Critical Norabel AB
Publication of EP0184564A1 publication Critical patent/EP0184564A1/en
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J9/00Moving targets, i.e. moving when fired at
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J9/00Moving targets, i.e. moving when fired at
    • F41J9/08Airborne targets, e.g. drones, kites, balloons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J5/00Target indicating systems; Target-hit or score detecting systems
    • F41J5/12Target indicating systems; Target-hit or score detecting systems for indicating the distance by which a bullet misses the target

Definitions

  • Sausage-shaped practice targets towed by aircraft are currently used but these targets are unable to simulate realistic flight behaviour, evasive tactics, etc.
  • These targets can be provided with a hit indicator (in reality a device measuring the miss distance), which records the number of shots within various zones from the indicator.
  • the present invention designated the Ripan system, solves the above problems.
  • Condition 1-3 led to the choice of radio-controlled miniature aircraft as a preferred carrier for sensing and indicating members with signal-processor between.
  • Condition 4 is fulfilled by means of pyrotechnical visual indication, flash, fitted on the aircraft. An electric flash or radio-transmission to a "display" on the ground is also feasible.
  • condition 5 enables fulfilment of condition 6.
  • the target size can be varied by giving the sensor unit a variable sensitivity threshold.
  • a microphone is selected which senses the pressure surge from a projectile passing at supersonic speed. The amplitude of this pressure surge is proportional to the distance and different thresholds can therefore be selected for this.
  • the miniature aircraft may thus constitute a "virtual" target differing in size from one time to another. The target is "virtual" since the visible target the soldier aims at is always the miniature aircraft.
  • a buffer for the number of registrations is also included in the signal processor, thus enabling the number of hits for achieving destruction to be varied. Varying degrees of difficulty are thus possible.
  • “Ripan” comprises the following main components:
  • the sensor 1 may be electromagnetic in order to avoid this limitation.
  • the signal processor is a unit 2 in which the sensitivity threshold for the microphone and the number of recorded "hits" required for destruction are set.
  • the processor 2 When the pre-set number of recorded "hits" has been reached, the processor 2 emits a signal which trips an indication.
  • the indicator unit 3 may consist of a number of pyrotechnical cartridges giving a powerful reddish flash to ensure good visibility.
  • the cartridges are disposed of after use, and are replaced by new ones.
  • the miniature aircraft is radio-controlled and can be guided from the ground both with respect to direction and speed.
  • the plane needs no special start ramp, but is thrown into the air by the "pilot's" assistant.
  • the equipment consists of five units:
  • the signal-processor, decoder/detonator unit and battery unit are combined to form a hit indicator.
  • the measuring microphone and pyro-unit are connected to the hit indicator by cabling provided with a contact device.
  • the hit indicator is based on the principle that a pressure wave (supersonic bang) is generated around a projectile travelling at supersonic speed.
  • the amplitude of the pressure wave decreases as the distance from the passing projectile increases.
  • the pressure wave is picked up by a measuring microphone and its signal is transmitted to the signal processor.
  • the in-coming signal is detected and processed in the signal-processor.
  • the analog signal is then converted to digital form. (8 bits parallel.)
  • the digital information is then transmitted to the decoder/detonator.
  • the digital information which is proportional to the amplitude from the supersonic bang, is converted in the decoder to a new digital form corresponding to 15 distance zones around the microphone.
  • a pre-set zone is then selected and passed on to a programmable counter which counts the number of detected hits within the selected zone.
  • the counter is adjustable between 1 and 15. When the correct number of hits is reached a firing pulse will be generated to a pyrotechnical charge.
  • the pyro-unit consists at present of 10 pyrotechnical charges. These are triggered electrically. Selection is performed and the requisite firing pulse generated in the detonator which forms an integral part with the decoder.
  • All units are supplied with current in any suitable manner, such as from a separate battery unit.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Oscillators With Electromechanical Resonators (AREA)
  • Treatment And Processing Of Natural Fur Or Leather (AREA)
  • Micro-Organisms Or Cultivation Processes Thereof (AREA)
  • Lubricants (AREA)
EP85850282A 1984-10-09 1985-09-12 Practice target Withdrawn EP0184564A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE8405033A SE468366B (sv) 1984-10-09 1984-10-09 Oevningsmaal
SE8405033 1984-10-09

Publications (1)

Publication Number Publication Date
EP0184564A1 true EP0184564A1 (en) 1986-06-11

Family

ID=20357276

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85850282A Withdrawn EP0184564A1 (en) 1984-10-09 1985-09-12 Practice target

Country Status (7)

Country Link
EP (1) EP0184564A1 (da)
JP (1) JPS61165599A (da)
KR (1) KR860003491A (da)
DK (1) DK462485A (da)
FI (1) FI853865L (da)
NO (1) NO853985L (da)
SE (1) SE468366B (da)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007015282A1 (en) * 2005-08-03 2007-02-08 D Adamo Mario Equipment for target shooting without using live targets
KR101140448B1 (ko) * 2008-03-24 2012-04-30 콸콤 인코포레이티드 다수의 다이버시티 소스로부터 신호들을 합성하기 위한 방법들 및 장치들

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20020007677A (ko) * 2000-07-18 2002-01-29 김명일 대공사격 훈련 시스템

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1578241A1 (de) * 1965-06-18 1971-08-12 Fisfeld Kurt Dipl Ing Signalgeber fuer die Schussablage von vom Flugzeug geschleppten Zielen
DE1703447A1 (de) * 1968-05-22 1972-01-13 Flygmaal Air Target Ltd Ab Akustisch wirkender Trefferanzeiger fuer geschleppte Flugzeugzielscheiben
FR2365773A1 (fr) * 1976-09-27 1978-04-21 United Kingdom Government Indicateur de but manque pour cibles aeriennes

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1578241A1 (de) * 1965-06-18 1971-08-12 Fisfeld Kurt Dipl Ing Signalgeber fuer die Schussablage von vom Flugzeug geschleppten Zielen
DE1703447A1 (de) * 1968-05-22 1972-01-13 Flygmaal Air Target Ltd Ab Akustisch wirkender Trefferanzeiger fuer geschleppte Flugzeugzielscheiben
FR2365773A1 (fr) * 1976-09-27 1978-04-21 United Kingdom Government Indicateur de but manque pour cibles aeriennes

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007015282A1 (en) * 2005-08-03 2007-02-08 D Adamo Mario Equipment for target shooting without using live targets
KR101140448B1 (ko) * 2008-03-24 2012-04-30 콸콤 인코포레이티드 다수의 다이버시티 소스로부터 신호들을 합성하기 위한 방법들 및 장치들

Also Published As

Publication number Publication date
FI853865L (fi) 1986-04-10
FI853865A0 (fi) 1985-10-04
NO853985L (no) 1986-04-10
SE8405033D0 (sv) 1984-10-09
DK462485A (da) 1986-04-10
SE468366B (sv) 1992-12-21
SE8405033L (sv) 1986-04-10
DK462485D0 (da) 1985-10-09
JPS61165599A (ja) 1986-07-26
KR860003491A (ko) 1986-05-26

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Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19850917

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE FR GB IT LI LU NL SE

17Q First examination report despatched

Effective date: 19870318

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19870729

RIN1 Information on inventor provided before grant (corrected)

Inventor name: ARBRANDT, HAKAN

Inventor name: BRUNSTEDT, JAN