TWIN-ENGINED MANEUVERABLE AEROPLANE CONTROL SYSTEM Russian patent published in 1997 - IPC

Abstract RU 2099244 C1

FIELD: aeronautical engineering. SUBSTANCE: control of twin-engined maneuverable aeroplane consists in deflecting rudders and ailerons. Reaction jets of starboard and port engines deflect each in one plane; simultaneously with deflection of rudders, ailerons are deflected, as well as reaction jets of starboard and port engines which are deflected upward-outside or downward-inside. If rudders are deflected to right, reaction jet of starboard engine is deflected outside and reaction jet of port engine is deflected inside through the same angle and vice versa. Ailerons are deflected through angles determined by relationship given in Description. EFFECT: enhanced efficiency.

Similar patents RU2099244C1

Title	Year	Author	Number
METHOD TO CONTROL TWIN-ENGINE AIRCRAFT AND SYSTEM TO THIS END	2007	Anikeev Nikolaj Fedorovich Barkovskij Vladimir Ivanovich Buntin Nikolaj Nikolaevich Vlasov Pavel Nikolaevich Vorob'Ev Aleksandr Vladimirovich Dokholov Dmitrij Sergeevich Dushits-Kogan Grigorij Davydovich Mozharov Valerij Alekseevich Noskov Jurij Viktorovich Obolenskij Jurij Gennad'Evich Petrov Vjacheslav Mifodievich Sigalov Jurij Viktorovich Sinevich Grigorij Mikhajlovich Sukhanov Valerij Leonidovich Tyshkevich Vjacheslav Andreevich Fedorov Aleksej Mikhajlovich Judis Sergej Romanovich	RU2392186C2
AILERON CONTROL SYSTEM	1991	Rogozhkin Ju.M.	RU2028251C1
CONTROL SURFACES WITH AXIAL COMPENSATION	1997	Frolishchev B.N.	RU2116222C1
SHORT TAKE-OFF AND LANDING AIRCRAFT	1996	Zhulev Ju.G. Zaretskij S.A. Kazhan V.G.	RU2103199C1
AIRCRAFT IN INTEGRAL AERODYNAMIC CONFIGURATION	2010	Pogosjan Mikhail Aslanovich Davidenko Aleksandr Nikolaevich Strelets Mikhail Jur'Evich Runishev Vladimir Aleksandrovich Tarasov Aleksej Zakharovich Shokurov Aleksej Kirillovich Bibikov Sergej Jur'Evich Krylov Leonid Evgen'Evich Moskalev Pavel Borisovich	RU2440916C1
ACTIVE SYSTEM FOR CONTROL OF LIFTING FORCE	1994	Vlasov V.A. Ganich G.A. Zhulev Ju.G.	RU2086469C1
METHOD OF IMPROVEMENT OF FLIGHT SAFETY IN CASE OF ENGINE FAILURE	2014	Popov Vladimir Nikolaevich Popov Sergej Aleksandrovich Gromov Aleksandr Shekspirovich	RU2562673C1
METHOD OF CONTROL OF FLYING VEHICLE AND DEVICE FOR REALIZATION OF THIS METHOD (VERSIONS)	2005	Amir'Jants Gennadij Ashotovich	RU2299834C2
AIRCRAFT CONTROL METHOD AND COMPLEX SYSTEM METHOD IS BUILT AROUND	2006	Karasev Andrej Gennad'Evich Vorob'Ev Aleksandr Vladimirovich Dokholov Dmitrij Sergeevich Kabakov Vladimir Borisovich Kostenko Nikolaj Ivanovich Mozharov Valerij Alekseevich Noskov Jurij Viktorovich Obolenskij Jurij Gennad'Evich Petrov Vjacheslav Mefod'Evich Stepanov Valentin Aleksandrovich Shtykalo Vasilij Fedorovich Jakubovich Mark Mikhajlovich	RU2327602C1
SYSTEM OF CONTROL OF TWIN-ENGINED AEROPLANE THROUGH CONTROL OF THRUST VECTOR	1998	Simonov M.P.	RU2122963C1

RU 2 099 244 C1

Authors

Vlasov A.N.

Grigor'Ev Ju.L.

Sukhanov V.L.

Tarasov A.Z.

Dates

1997-12-20—Published

1996-08-12—Filed