EP0184564A1 - Practice target - Google Patents
Practice target Download PDFInfo
- 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- Withdrawn
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
- F41J9/00—Moving targets, i.e. moving when fired at
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
- F41J9/00—Moving targets, i.e. moving when fired at
- F41J9/08—Airborne targets, e.g. drones, kites, balloons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
- F41J5/00—Target indicating systems; Target-hit or score detecting systems
- F41J5/12—Target 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)
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)
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20020007677A (ko) * | 2000-07-18 | 2002-01-29 | 김명일 | 대공사격 훈련 시스템 |
Citations (3)
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 |
-
1984
- 1984-10-09 SE SE8405033A patent/SE468366B/sv not_active IP Right Cessation
-
1985
- 1985-09-12 EP EP85850282A patent/EP0184564A1/en not_active Withdrawn
- 1985-10-04 FI FI853865A patent/FI853865L/fi not_active IP Right Cessation
- 1985-10-05 KR KR1019850007341A patent/KR860003491A/ko not_active Application Discontinuation
- 1985-10-08 NO NO853985A patent/NO853985L/no unknown
- 1985-10-08 JP JP60224620A patent/JPS61165599A/ja active Pending
- 1985-10-09 DK DK462485A patent/DK462485A/da not_active Application Discontinuation
Patent Citations (3)
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)
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 |