METHOD OF COMPLEX IMPROVEMENT OF AERODYNAMIC AND TRANSPORT CHARACTERISTICS, RAM WING MACHINE FOR IMPLEMENTATION OF NAMED METHOD (VERSIONS) AND FLIGHT METHOD Russian patent published in 2015 - IPC B60V1/11 B60V1/08 

Abstract RU 2539443 C2

FIELD: transport.

SUBSTANCE: group of inventions relates to aircraft and vehicles with air (static and dynamic) unloading, in particular self-stabilised ram wing machines of A, B and C types. The ram wing machine (RWM) contains a hull, a propulsor, a bearing plane of small lengthening (PSL) with end floating washers, retractable front and back protections of a static airbag, stabilisation and control devices. The bearing PSL is implemented in the form of a centre wing of small lengthening (CW) which is made in the longitudinal direction at least of two PSLs - the front PSL with a nose guard and flaperons and the back PSL with flaperons. Under the centre wing within the boundaries of its projection to the horizontal plane a cavity of static AB (StAB), under the front PSL - a cavity of dynamic AB (DAB), under the back PSL - a cavity of static and dynamic AB (SDAB) are made. At the complex increase of aerodynamic and transport characteristics of RWM including the creation of the necessary carrying power (CP) by means of the elevated pressure zone between the bearing PSL and the bearing surface the natural character of dependences of CP value and the positions of focuses of the bearing PSL from the angle of attack and height of flight is changed by the creation in the longitudinal direction of at least two local zones of formation of CP - front and back, with points of their application on a longitudinal axis respectively in front of and behind the centre of mass.

EFFECT: improvement of the safety of flight and manoeuvres, increase in the bearing ability and height of flight in the mode of the screen effect, reduction of sizes, improvement of runway characteristics, water tightness, expansion of functionality and range of operational centring, improvement of convenience of operation and maintenance is achieved.

38 cl, 37 dwg

Similar patents RU2539443C2

Title Year Author Number
WING-IN-GROUND-EFFECT CRAFT 2003
  • Sergeev Viktor Georgievich
  • Zhukov Vladimir Grigor'Evich
  • Novikov Aleksandr Viktorovich
RU2286268C2
GROUND-EFFECT CRAFT 2002
  • Martirosov R.G.
RU2254250C2
"TAILLESS" FLARECRAFT 2022
  • Pavlov Gennadij Alekseevich
RU2776632C1
HOVERCARFT 2012
  • Jakovlev Vladimir Vasil'Evich
  • Jakovlev Aleksandr Vasil'Evich
RU2550568C2
TAKEOFF-AND-LANDING COMPLEX FOR GROUND-EFFECT CRAFT AND METHOD OF PERFORMING TAKEOFF AND LANDING OF SUCH CRAFT 2002
  • Martirosov R.G.
RU2254251C2
HOVERCRAFT WITH WATER-JET PROPULSOR 2015
  • Garafutdinov Askhat Abrarovich
RU2582505C1
EKRANOPLAN OF INTEGRATED AEROGYDRODYNAMIC COMPOUND 2016
  • Kolganov Vyacheslav Vasilevich
RU2629463C1
SELF-STABILISING WINGED SURFACE EFFECT VEHICLE 2007
  • Surzhik Vitalij Vital'Evich
  • Mukhopad Jurij Fedorovich
  • Velichko Igor' Ivanovich
RU2368522C2
WING-IN-GROUND EFFECT CRAFT AND METHOD OF LONGITUDINAL CONTROL 1993
  • Navolotskij Leonid Nikolaevich
RU2097229C1
WING IN GROUND 2019
  • Krutov Aleksandr Aleksandrovich
  • Pigusov Evgenij Aleksandrovich
  • Chernousov Vladimir Ivanovich
RU2729114C1

RU 2 539 443 C2

Authors

Novikov-Kopp Ivan

Dates

2015-01-20Published

2010-01-05Filed