Show metadata Hide metadata

(19)

(11)

2 575 301

(13)

(51)

IPC

B64D39/00(2006-01-01)

(21) (22)

Application

2014133924/11, 2014-08-18

(24)

Start date

2014-08-18

(22)

Actual filing date

2014-08-18

(45)

Published

2016-02-20

(72)

Inventor

Vorontsov Vladimir Petrovich

(73)

Holder

Publichnoe Aktsionernoe Obshchestvo Aviatsionnyj Nauchno-Tekhnicheskij Kompleks Im. G.M. Berieva" Im. G.M. Berieva")

METHOD TO ENSURE SAFETY OF IN-FLIGHT REFUELLING AND APPARATUS THEREFOR Russian patent published in 2016 - IPC B64D39/00

Abstract RU 2575301 C1

FIELD: aviation.

SUBSTANCE: invention relates to aviation, in particular to in-flight refuelling. To ensure the safety of in-flight refuelling, before the fuel supply through the flight refuelling probe with a cone, vortex generators on the plane shall be extended for intensive mixing of air flow and fuel in the event of its leak. The safety device contains vortex generators with the height entering beyond the boundary layer to the height not exceeding one third of the distance between the surface of the aircraft and the lower edge of the engine air intake, the vortex generators are installed in the peak speed area in the way of design fuel spill.

EFFECT: improved safety of operation at in-flight refuelling.

4 cl, 6 dwg

Similar patents RU2575301C1

Title	Year	Author	Number
METHOD FOR DISPLAYING CURRENT AND PROGNOSTIC INFORMATION DURING AIR REFUELING OF AIRCRAFTS	2017	Ajvazyan Sergej Albertovich Moiseev Anatolij Georgievich	RU2676594C2
TANKER AEROPLANE	1994	Egorshev Anatolij Viktorovich Rafeenkov Vladimir Mikhajlovich Lomakin Vladimir Vladimirovich Komarov Vladimir Aleksandrovich	RU2100257C1
TANKER AEROPLANE	1994	Egorshev Anatolij Viktorovich Komarov Vladimir Aleksandrovich Lomakin Vladimir Vladimirovich Rafeenkov Vladimir Mikhajlovich	RU2142897C1
AIR REFUELING SYSTEM WITH AUTOMATIC CONTROL AND AUTO-STABILIZED REFUELING DEVICE	2023	Sadrtdinov Vladislav Diyasovich Inyachkina Yana Olegovna Khrapov Dmitrij Alekseevich	RU2809164C1
METHOD OF INVESTIGATING INGRESS OF ICE FRAGMENTS INTO ENGINE AIR INTAKES AND DEVICE FOR ITS IMPLEMENTATION	2018	Vorontsov Vladimir Petrovich Zajtsev Valerij Yurevich Chemezov Vladimir Leonidovich	RU2692835C1
GROUND MOVABLE BENCH AND METHOD OF ITS APPLICATION FOR TESTING OF AUTOMATIC CONTROL SYSTEM OF REFUELLING IN AIR	2023	Sadrtdinov Vladislav Diyasovich Solomatin Yurij Aleksandrovich Lukashov Igor Valerevich Badretdinova Ajgul Bulatovna Vinogradova Alla Konstantinovna Bespalova Lyudmila Vasilevna	RU2819151C1
MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS	1996	Simonov M.P. Knyshev A.I. Barkovskij A.F. Korchagin V.M. Blinov A.I. Galushko V.G. Emel'Janov I.V. Grigorenko A.I. Kalibabchuk O.G. Shenfinkel' Ju.I. Dubovskij Eh.A. Sopin V.P. Petrov V.M. Dzhandzhgava G.I. Bekirbaev T.O. Pogosjan M.A. Chepkin V.M.	RU2207968C2
FUEL SYSTEM OF SUSPENSION UNIT FOR FUELING IN FLIGHT	1984	Gnenkov V.P. Danilin R.S. Mirnyj R.N. Naumov Ju.G. Stepanenko V.A. Sukhov I.I.	RU1262865C
DEVICE FOR CHECK OF AIRCRAFT IN-FLIGHT REFUELLING PROCESS	1997	Bublik Viktor Aleksandrovich Kapkin Aleksandr Pavlovich	RU2111154C1
METHOD FOR DETERMINING THE OVERLAP OF A TOWED TWO-WIRE AIRCRAFT ANTENNA AND THE DEVICE FOR ITS IMPLEMENTATION	2017	Vorontsov Vladimir Petrovich Shapovalov Aleksandr Georgievich	RU2658549C1

RU 2 575 301 C1

Authors

Vorontsov Vladimir Petrovich

Dates

2016-02-20—Published

2014-08-18—Filed