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2003133223/11, 2003-11-14

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Start date

2003-11-14

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Actual filing date

2003-11-14

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Published

2004-06-27

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Inventor

Belyj Ju.I.Bregman B.D.Gorb V.S.Gurulev A.M.Demin I.M.Dzhandzhgava G.I.Ivanov Ju.L.Kavinskij V.V.Knyshev A.I.Mamonov A.I.Merkulov V.I.Negrikov V.V.Orekhov M.I.Pekarsh A.I.Pogosjan M.A.Poljakov V.B.Simonov M.P.Sopin V.P.Tagantsev V.A.

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Holder

Otkrytoe Aktsionernoe Obshchestvo Sukhogo"Otkrytoe Aktsionernoe Obshchestvo Aviatsionnoe Proizvodstvennoe Ob"Edinenie"Otkrytoe Aktsionernoe Obshchestvo Priborostroitel'Noe Konstruktorskoe Bjuro"

MULTI-MISSION AIRCRAFT Russian patent published in 2004 - IPC

Abstract RU 2231478 C1

FIELD: aircraft instrumentation engineering.

SUBSTANCE: proposed multi-mission aircraft is used for detection and destruction of air, surface and ground targets at simultaneous performance of reconnaissance and training measures in combat version and combat trainer version. Airframe, aircraft equipment, power plant and high-lift devices, as well as indication and control, complex of destruction and counter-measure appliances, parameter monitoring and recording system inter-aircraft communication system, system for connection with control points, radar sighting system, pilotage navigational system, infra-red imaging sighting system, laser optical sighting system, counter-measures system, destruction and passive counter-measure aids control system, tele-command guidance system, navigational and guidance satellite system, display processor, reprogrammed storage unit, "n" multi-functional indicators, TV signal converter and on-board digital computer are interconnected by information exchange channel. Digital computer has computer-logic modules for planning flight missions, taking decisions pertaining to elimination of failures, connection and disconnection of information exchange system, complex target allocation and target designation, selection and application of destruction and counter-measures appliances which are interconnected by internal information exchange channel. Aircraft is additionally provided with parameter meter of motion of antenna of radar sighting system and computer logic modules for prompt analysis of results of operational reconnaissance and application of destruction, ground preparation and training units, combined target designation by aeronautical chart, forming parameters for emergency escape of crew from aircraft, forming parameters of motion of antenna of radar sighting system extend functional capabilities and enhances efficiency.

EFFECT: extended functional capabilities; enhanced efficiency both in single-seat and two-seat versions.

1 dwg

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RU 2 231 478 C1

Authors

Belyj Ju.I.

Bregman B.D.

Gorb V.S.

Gurulev A.M.

Demin I.M.

Dzhandzhgava G.I.

Ivanov Ju.L.

Kavinskij V.V.

Knyshev A.I.

Mamonov A.I.

Merkulov V.I.

Negrikov V.V.

Orekhov M.I.

Pekarsh A.I.

Pogosjan M.A.

Poljakov V.B.

Simonov M.P.

Sopin V.P.

Tagantsev V.A.

Dates

2004-06-27—Published

2003-11-14—Filed

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