METHOD OF CONTROL OF THRUST VECTOR IN ANNULAR SUPERSONIC NOZZLE AND ANNULAR SUPERSONIC NOZZLE USED FOR REALIZATION OF THIS METHOD Russian patent published in 1998 - IPC

Abstract RU 2111374 C1

FIELD: aeronautical engineering and rocketry; short takeoff and landing aeroplanes. SUBSTANCE: annular nozzle includes shroud and central body. For control of magnitude and direction of thrust, central body and/or shroud are rotated around axis of nozzle and are shifted axially; shroud and/or central body are provided with stepped cut or with combined stepped and bevel cuts. EFFECT: enhanced reliability. 3 cl, 3 dwg

Similar patents RU2111374C1

Title	Year	Author	Number
POWER PLANT FOR VERTICAL OR SHORT TAKE-OFF AND LANDING AEROPLANE	1997	Kekhvajants V.G.	RU2126904C1
METHOD TO CONTROL VECTOR OF JET ENGINE THRUST AND SUPERSONIC NOZZLE	2009	Kekhvajants Valerij Grigor'Evich	RU2412368C1
METHOD OF CREATION OF THRUST OF JET ENGINE AND DEVICE FOR REALIZATION OF THIS METHOD	1995	Kekhvajants V.G.	RU2103538C1
ADJUSTABLE FLAT NOZZLE FOR GAS TURBINE ENGINE	2001	Shkljaev I.V. Pozharinskij A.A.	RU2193680C2
NOZZLE	2022	Novikov Igor Evgenevich	RU2791932C1
THRUST GENERATION IN JET ENGINE AND JET NOZZLE TO THIS END	2012	Kekhvajants Valerij Grigor'Evich	RU2536460C2
ANNULAR JET NOZZLE OF VARIABLE GEOMETRY	1999	Bakhmutov A.A. Bukanov V.T. Klepikov I.A. Prishchepa V.I.	RU2150600C1
SILENCING NOZZLE OF AIR-JET ENGINE (VERSIONS)	2006	Zhitenev Vladimir Konstantinovich Kolesnikova Svetlana Anatol'Evna Krasheninnikov Sergej Jur'Evich Mironov Aleksej Konstantinovich Shenkin Andrej Vladimirovich	RU2313680C2
PIN NOZZLE	2022	Semenov Vasilii Vasilevich	RU2793042C1
SUPERSONIC AIRCRAFT JET ENGINE	2007	Chehjz Dzhejms D. Garzon German Andres	RU2454354C2

RU 2 111 374 C1

Authors

Kekhvajants V.G.

Dates

1998-05-20—Published

1992-09-21—Filed