WO2016122430A1 - Unité d'interface d'arme à feu - Google Patents

Unité d'interface d'arme à feu Download PDF

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Publication number
WO2016122430A1
WO2016122430A1 PCT/TR2016/050023 TR2016050023W WO2016122430A1 WO 2016122430 A1 WO2016122430 A1 WO 2016122430A1 TR 2016050023 W TR2016050023 W TR 2016050023W WO 2016122430 A1 WO2016122430 A1 WO 2016122430A1
Authority
WO
WIPO (PCT)
Prior art keywords
interface
gun
unit
power
data
Prior art date
Application number
PCT/TR2016/050023
Other languages
English (en)
Inventor
Yuksel SERDAR
Rafet EROGLU
Sait SARI
Ahmet MERT
Ahmet Coban
Original Assignee
Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi
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 Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi filed Critical Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi
Priority to UAU201707414U priority Critical patent/UA123684U/uk
Publication of WO2016122430A1 publication Critical patent/WO2016122430A1/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G5/00—Elevating or traversing control systems for guns
    • F41G5/14—Elevating or traversing control systems for guns for vehicle-borne guns
    • F41G5/18—Tracking systems for guns on aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B64D7/02—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms
    • B64D7/06—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms movably mounted
    • 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
    • F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/28—Electrically-operated systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G5/00—Elevating or traversing control systems for guns
    • F41G5/06—Elevating or traversing control systems for guns using electric means for remote control

Definitions

  • the present invention relates to a gun weapon interface unit developed to fire and control the gun unit (e.g. M-197 gun unit) of aircrafts (e.g. AH-1S Cobra helicopter). More specifically, the present invention relates to a gun weapon interface unit which communicates with a mission computer, thus enables all commands and status information to be digitally transmitted to the mission computer, and which, when the mission computer fails, can be controlled by means of the discrete control signals coming from the pilot mission grips.
  • a gun weapon interface unit developed to fire and control the gun unit (e.g. M-197 gun unit) of aircrafts (e.g. AH-1S Cobra helicopter). More specifically, the present invention relates to a gun weapon interface unit which communicates with a mission computer, thus enables all commands and status information to be digitally transmitted to the mission computer, and which, when the mission computer fails, can be controlled by means of the discrete control signals coming from the pilot mission grips.
  • the objective of the present invention is to provide a gun weapon interface unit which enables to fire and control the gun weapon unit of the aircrafts.
  • all of the peripheral equipment and relays used for controlling and firing the gun system are collected in the gun weapon interface unit. This way, cable lengths and weights are reduced.
  • the gun weapon interface unit communicates with a mission computer via MIL-STD-1760D data bus and transmits all of the commands and status information digitally to the mission computer and thus control of the gun unit is facilitated.
  • the gun weapon interface unit of the present invention is designed in compliance with the environmental requirements determined by military standards (MIL- HDBK-5400, MIL-STD-810, MIL-STD-704 and MIL-STD-461).
  • a gun weapon interface unit developed to fulfill the objectives of the present invention is illustrated in the accompanying figures, in which:
  • Figure 1 is a schematic view of the gun weapon interface unit.
  • Figure 2 is a schematic view of the interface card.
  • Gun unit A gun weapon interface unit (1) which enables to control and fire the gun units (T) of the aircrafts (H), basically comprises
  • At least one interface card (2) which is adapted to generate control signals according to the discrete control and condition signals coming to it and to transmit these signals to the gun unit (T) that will be controlled; and to generate position information from the data coming from the gun unit (T) position sensors and to transmit these information to the gun unit (T) that will be directed; and to establish data communication with a mission computer (G),
  • At least one power card (3) which is adapted to supply the required power, - at least one main board (3) on which the interface card (2) and the power card (4) are mounted, at least one filter circuit (5) which is adapted to avoid electromagnetic interference from power lines,
  • At least one data interface (6) which provides a connection interface for receiving data from the pilot mission grip (K), aircraft (H) and/or gun unit (T) and sending data to the gun unit (T),
  • At least one power interface (7) which provides power inlet to supply power to the power card (3)
  • At least one communication interface (8) which provides a connection interface for communication with a mission computer (G),
  • test interface 9 which provides a connection interface for testing the unit via an external computer (B).
  • the gun weapon interface unit (1) of the present invention is comprised of a box shaped body, interface connections and three electronic cards. These cards are the interface card (2), the power card (4) and the main board (3) on which the former cards are mounted ( Figure 1).
  • the interface card (2) includes thereon a control circuit (2.1), a signal conditioning circuit (2.2), a resolver interface circuit (2.3), a communication circuit (2.4) and a test circuit (2.5) ( Figure 2).
  • the signal conditioning circuit (2.2) located in the interface card (2) converts the discrete control and condition signals coming from the pilot mission grip (K), aircraft (H) and/or gun unit (T) via a data interface (6) into digital data and sends them to the control circuit (2.1) comprising a controller. Similarly, it converts the digital data output from the control circuit (2.1) to discrete control signals and sends them to the gun unit (T) that will be controlled.
  • the resolver interface circuit (2.3) converts the position information coming from the azimuth and elevation resolver sensors (i.e. angle sensors) located in the gun unit (T) via the data interface (6) into digital data and sends them to the control circuit (2.1). Furthermore, it converts the digital position error data, which comes from the control circuit (2.1) and is required to direct the gun unit (T), to resolver information and transmits it to the gun unit (T).
  • the communication circuit (2.4) enables the gun weapon interface unit (1) and the mission computer (G) to communicate with each other via the communication interface (8) (preferably via the MIL-STD-1760D data bus).
  • the test circuit (2.5) enables the gun weapon interface unit (1) to be tested or software to be loaded thereon by means of an external computer (B) via a test interface (9).
  • an external computer B

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

La présente invention concerne une unité d'interface d'arme à feu (1) qui permet de commander des unités de canon (T) d'aéronefs (H), et de déclencher le tir de ces dernières, et qui comprend dans l'ensemble au moins une carte d'interface (2), qui est conçue pour générer des signaux de commande en fonction des signaux discrets de commande et d'état venant à cette dernière et pour transmettre ces signaux à l'unité de canon (T) qui sera commandée et pour établir une communication de données avec un ordinateur de mission (G); au moins une carte de puissance (3) qui est conçue pour fournir la puissance nécessaire; au moins une planche principale (4) sur laquelle sont montées la carte d'interface (2) et la carte de puissance (3); au moins un circuit filtrant (5) qui est conçu pour éviter les interférences électromagnétiques des lignes d'alimentation; au moins une interface de données (6) qui fournit une interface de connexion pour recevoir des données de la poignée de contrôle du pilote (K), de l'aéronef (H) et/ou de l'unité de canon (T) et envoyer des données à l'unité de canon (T); au moins une interface de puissance (7) qui fournit une entrée de puissance afin de fournir de la puissance à la carte de puissance (3); au moins une interface de communication (8) qui fournit une interface de connexion pour permettre une communication avec un ordinateur de mission (G); au moins une interface de test (9) qui fournit une interface de connexion pour tester l'unité par le biais d'un ordinateur externe (B).
PCT/TR2016/050023 2015-01-29 2016-01-29 Unité d'interface d'arme à feu WO2016122430A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201707414U UA123684U (uk) 2015-01-29 2016-01-29 Блок сполучення з гарматним або кулеметним озброєнням

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TR201501013 2015-01-29
TR2015/01013 2015-01-29

Publications (1)

Publication Number Publication Date
WO2016122430A1 true WO2016122430A1 (fr) 2016-08-04

Family

ID=55629086

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/TR2016/050023 WO2016122430A1 (fr) 2015-01-29 2016-01-29 Unité d'interface d'arme à feu

Country Status (2)

Country Link
UA (1) UA123684U (fr)
WO (1) WO2016122430A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109398716A (zh) * 2018-12-03 2019-03-01 中航技进出口有限责任公司 外置式机载控制系统
RU2748133C1 (ru) * 2020-10-02 2021-05-19 Василий Васильевич Ефанов Способ управления вооружением многофункциональных самолетов тактического назначения и система для его осуществления

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060219094A1 (en) * 2002-11-06 2006-10-05 Nir Padan Real time dynamically controled elevation and azimuth gun pod mounted on a fixed wing aerial combat vehicle
US7137599B1 (en) * 2004-04-26 2006-11-21 Raytheon Company Launcher with dual mode electronics
US20100070674A1 (en) * 2008-09-15 2010-03-18 Raytheon Company Smart translator box for agm-65 aircraft "maverick" analog interface to mil-std-1760 store digital interface
US20130218372A1 (en) * 2012-02-22 2013-08-22 Sikorsky Aircraft Corporation Weapons Stores Processor Panel For Aircraft

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060219094A1 (en) * 2002-11-06 2006-10-05 Nir Padan Real time dynamically controled elevation and azimuth gun pod mounted on a fixed wing aerial combat vehicle
US7137599B1 (en) * 2004-04-26 2006-11-21 Raytheon Company Launcher with dual mode electronics
US20100070674A1 (en) * 2008-09-15 2010-03-18 Raytheon Company Smart translator box for agm-65 aircraft "maverick" analog interface to mil-std-1760 store digital interface
US20130218372A1 (en) * 2012-02-22 2013-08-22 Sikorsky Aircraft Corporation Weapons Stores Processor Panel For Aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109398716A (zh) * 2018-12-03 2019-03-01 中航技进出口有限责任公司 外置式机载控制系统
CN109398716B (zh) * 2018-12-03 2023-11-28 中航技进出口有限责任公司 外置式机载控制系统
RU2748133C1 (ru) * 2020-10-02 2021-05-19 Василий Васильевич Ефанов Способ управления вооружением многофункциональных самолетов тактического назначения и система для его осуществления

Also Published As

Publication number Publication date
UA123684U (uk) 2018-03-12

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