SPRAY SYSTEM AND SPRAY METHOD

• Main Authors: MINATOGAWA RYO, OZAKI TERUTAKA
• Format: Patent
• Language: English; Japanese
• Published: 05.12.2019
• Subjects: AEROPLANES; AIRCRAFT; APPLYING LIQUIDS OR OTHER FLUENT MATERIALS TO SURFACES, IN GENERAL; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; ATOMISING APPARATUS; AVIATION; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; HELICOPTERS; NOZZLES; PARACHUTES; PERFORMING OPERATIONS; SPRAYING APPARATUS; SPRAYING OR ATOMISING IN GENERAL; TRANSPORTING

To reduce a size of an air thrust device to reduce influence of airflow on jet flow in a spray system which can utilize the air thrust device to move an injector to any work position easily.SOLUTION: A spray system 1 includes a first self-propulsion machine 10 and a second self-propulsion machine 20. The first self-propulsion machine 10 includes a first air thrust device 11 and an injector 12 capable of spraying a fluid to a working surface W. The second self-propulsion machine 20 includes a second air thrust device 21 and a first supply pipe 22 which supplies the fluid to the first self-propulsion machine 10.SELECTED DRAWING: Figure 1 【課題】空気推力装置を用いることによって噴射装置を任意の作業位置に容易に移動させることが可能な吹付システムにおいて、空気推力装置の大きさを抑制して噴射流への気流の影響を低減する。【解決手段】吹付システム１は、第１の自己推進機１０と、第２の自己推進機２０とを含む。第１の自己推進機１０は、第１の空気推力装置１１と、作業面Ｗに流体を吹き付けること可能な噴射装置１２とを備える。第２の自己推進機２０は、第２の空気推力装置２１と、第１の自己推進機１０に流体を供給する第１の供給管２２とを備える。【選択図】図１