OUTER CYLINDER OF PROPULSION MACHINE SUCH AS FLYING CAR

To solve problems when a flying car of a size in such a degree of a compact car performs high speed flight in which (1) a current propulsion machine is made compact, (2) air resistance is reduced because of high speed flight, (3) a high-speed flow flowing in a radiator is decelerated, and both of a...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	MIYAUCHI SUNAO
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AEROPLANES AIRCRAFT AMPHIBIOUS OR LIKE VEHICLES ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CONVERTIBLE VEHICLES COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOWOF GASES OR LIQUIDS FLUID-PRESSURE ACTUATORS FLYING SUITS HEATING HELICOPTERS HYDRAULICS OR PNEUMATICS IN GENERAL LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING VEHICLES FOR USE BOTH ON RAIL AND ON ROAD VEHICLES IN GENERAL WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	To solve problems when a flying car of a size in such a degree of a compact car performs high speed flight in which (1) a current propulsion machine is made compact, (2) air resistance is reduced because of high speed flight, (3) a high-speed flow flowing in a radiator is decelerated, and both of a pressure loss due to air resistance in the radiator and cooling performance are optimized, and (4) a take-off/landing site is restricted in a city and the like, and therefore a short take-off/landing performance is needed.SOLUTION: A propulsion machine 2 is stored in an outer cylinder 1 having ejector principle in order to improve propulsive force of a flying car. Also, the outer cylinder 1 and its attached equipment are made into an aerodynamically-refined configuration and structure/mechanism. Also, an added value such as a radiator being built in the outer cylinder 1 or a boundary-layer control of a main wing flap are acquired.SELECTED DRAWING: Figure 6 【課題】コンパクトカー程度の大きさの空飛ぶ車が高速飛行するには、下記等の課題がある。 ▲１▼現状の推進機のコンパクト化。 ▲２▼高速飛行するので、空気抵抗を低減。 ▲３▼ラジエータ流入の高速流を減速し、ラジエータ内での空気抵抗による圧力損失と冷却性能の両方を最適化する。 ▲４▼離着陸地は、都市内等では制約があるので、短距離離着陸性能が要る。【解決手段】空飛ぶ車の推進力向上のため、エジェクタ原理を有する外筒１に推進機２を収納する。また外筒１とその付属機器を空気力学的に洗練された形態や構造・機構にする。また外筒１にラジエータ内蔵や主翼フラップの境界層制御等の付加価値をつける。【選択図】図６