METHOD FOR STABILIZATION OF AN AIRCRAFT AND APPLIAMETHOD FOR STABILIZATION OF AN AIRCRAFT AND APPLIANCE FOR ITS IMPLEMENTATION NCE FOR ITS IMPLEMENTATION

A method for stabilization of an aircraft on air part of the trajectory is in intake of the falling flow, with formation of directed jet to form side traction in the zone of the front part of the aircraft. At that, one checks the plane of the spatial attack angle by means of symmetrical V-like aerod...

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Bibliographische Detailangaben
Hauptverfasser:	PASHKOV ANATOLII VOLODYMYROVYCH PASHKOV ANATOLII VOLODYMYROVYCH, KHOROLSKYI PETRO GEORGIIOVYCH KHOROLSKYI PETRO GEORGIIOVYCH, DRON MYKOLA MYKHAILOVYCH DRON MYKOLA MYKHAILOVYCH, GRYNCHYSHYN YURII LEONIDOVYCH GRYNCHYSHYN YURII LEONIDOVYCH
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AMMUNITION AVIATION BLASTING COSMONAUTICS EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS
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Beschreibung
Zusammenfassung:	A method for stabilization of an aircraft on air part of the trajectory is in intake of the falling flow, with formation of directed jet to form side traction in the zone of the front part of the aircraft. At that, one checks the plane of the spatial attack angle by means of symmetrical V-like aerodynamical surface placed in the front part and free for rotation with respect to the long axis of the aircraft; direction of the stabilization side traction is fixed with respect to the plane of the spatial attack angle, and the value of the side traction is controlled depending on the value of that angle. Appliance for implementation of the method has placed in the front part of the aircraft connected in sequence air-intake unit, shaft-controller of the gas flow, gas flow channels and side nozzles. The front part of the aircraft is equipped with symmetrical V-like aerodynamical surface and is connected to he housing by means of rotary hinge with its axis coinciding with the long axis of the aircraft.