PL422879A1 - Central avionic control computer - Google Patents

Central avionic control computer

Info

Publication number
PL422879A1
PL422879A1 PL422879A PL42287916A PL422879A1 PL 422879 A1 PL422879 A1 PL 422879A1 PL 422879 A PL422879 A PL 422879A PL 42287916 A PL42287916 A PL 42287916A PL 422879 A1 PL422879 A1 PL 422879A1
Authority
PL
Poland
Prior art keywords
card
avionic
discrete
interface
management
Prior art date
Application number
PL422879A
Other languages
Polish (pl)
Inventor
Yuksel Serdar
Huseyin Dincer Calislar
Umur Akinci
Mehmet Unal Durmus
Sefa Akyurek
Serkan Dortkardesler
Mahmut Celal Ademoglu
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
Publication of PL422879A1 publication Critical patent/PL422879A1/en

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F1/00—Details not covered by groups G06F3/00 - G06F13/00 and G06F21/00
    • G06F1/16—Constructional details or arrangements
    • G06F1/18—Packaging or power distribution
    • G06F1/181—Enclosures
    • G06F1/182—Enclosures with special features, e.g. for use in industrial environments; grounding or shielding against radio frequency interference [RFI] or electromagnetical interference [EMI]
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F1/00—Details not covered by groups G06F3/00 - G06F13/00 and G06F21/00
    • G06F1/16—Constructional details or arrangements
    • G06F1/18—Packaging or power distribution
    • G06F1/183—Internal mounting support structures, e.g. for printed circuit boards, internal connecting means
    • G06F1/185—Mounting of expansion boards
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F1/00—Details not covered by groups G06F3/00 - G06F13/00 and G06F21/00
    • G06F1/16—Constructional details or arrangements
    • G06F1/18—Packaging or power distribution
    • G06F1/183—Internal mounting support structures, e.g. for printed circuit boards, internal connecting means
    • G06F1/188—Mounting of power supply units
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00—Constructional details common to different types of electric apparatus
    • H05K7/14—Mounting supporting structure in casing or on frame or rack
    • H05K7/1401—Mounting supporting structure in casing or on frame or rack comprising clamping or extracting means
    • H05K7/1411—Mounting supporting structure in casing or on frame or rack comprising clamping or extracting means for securing or extracting box-type drawers
    • H05K7/1412—Mounting supporting structure in casing or on frame or rack comprising clamping or extracting means for securing or extracting box-type drawers hold down mechanisms, e.g. avionic racks

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Human Computer Interaction (AREA)
  • Power Engineering (AREA)
  • Computer Hardware Design (AREA)
  • General Physics & Mathematics (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Electromagnetism (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Processing Or Creating Images (AREA)
  • User Interface Of Digital Computer (AREA)

Abstract

Niniejszy wynalazek dotyczy awionicznego centralnego komputera sterującego (1), umożliwiającego sterowanie wykrywaniem celu i bronią, walką elektroniczną, nawigacją, systemami transmisji danych taktycznych i komunikacji zintegrowanymi w statku powietrznym, realizację zarządzania misją i lotem, zarządzanie prezentacją wyświetlania i nadzorowanie wymiany wszystkich informacji w statku powietrznym z pojedynczego centrum i zasadniczo zawiera on ramę montażową (2), która zapewnia interfejs montażowy dla zlokalizowanych w niej kart elektronicznych, co najmniej jedną kartę (3) procesora awionicznego, która jest przystosowana do realizowania nawigacji, komunikacji, nadzoru, zarządzania awaryjnego i procesów planowania zadań, płytkę typu mezzanine interfejsu MIL-STD-1553, płytkę typu mezzanine interfejsu ARINC-429, co najmniej jedną kartę przetwarzania graficznego, która jest przystosowana do generowania grafiki, która ma być wyświetlana na ekranach dla interfejsu użytkownika, co najmniej jedną kartę (7) przetwarzania wideo, która jest przystosowana do wykonywania procesu przełączania sygnałów wideo i zmiany postaci wideo, co najmniej jedną kartę (8) dyskretnego interfejsu, która zapewnia dyskretny interfejs wejścia i wyjścia dla dyskretnych markerów, co najmniej jedną kartę (9) magazynowania energii i co najmniej jedną płytkę zasilania, która dostarcza energię elektryczną, wymaganą przez karty elektroniczne wykorzystywane w jednostce.The present invention relates to an avionic central control computer (1) enabling control of target detection and weapons, electronic warfare, navigation, tactical data transmission systems and communications integrated in the aircraft, the implementation of mission and flight management, display presentation management and supervising the exchange of all information in the ship air from a single center and essentially includes a mounting frame (2) that provides a mounting interface for the electronic cards located in it, at least one card (3) of an avionic processor, which is adapted to provide navigation, communication, supervision, emergency management and processes task scheduling, MIL-STD-1553 mezzanine board, ARINC-429 mezzanine board, at least one graphics processing card that is adapted to generate graphics to be displayed on screens for interfe jsu user, at least one video processing card (7) that is adapted to perform the process of switching video signals and changing video form, at least one card (8) of a discrete interface that provides a discrete input and output interface for discrete markers, at least one energy storage card (9) and at least one power board that supplies the electricity required by the electronic cards used in the unit.

PL422879A 2015-03-02 2016-03-02 Central avionic control computer PL422879A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TR201502422 2015-03-02
PCT/TR2016/050052 WO2016140637A1 (en) 2015-03-02 2016-03-02 An avionic central control computer

Publications (1)

Publication Number Publication Date
PL422879A1 true PL422879A1 (en) 2018-03-26

Family

ID=55750425

Family Applications (1)

Application Number Title Priority Date Filing Date
PL422879A PL422879A1 (en) 2015-03-02 2016-03-02 Central avionic control computer

Country Status (3)

Country Link
PL (1) PL422879A1 (en)
WO (1) WO2016140637A1 (en)
ZA (1) ZA201706134B (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6865690B2 (en) * 2001-06-21 2005-03-08 Northrop Grumman Corporation Voltage conditioner with embedded battery backup

Also Published As

Publication number Publication date
WO2016140637A1 (en) 2016-09-09
ZA201706134B (en) 2019-01-30

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