Aircraft washing equipment

Abstract: The aircraft washing equipment comprises a sub-arm (15) that rotates at the tip of an ascendable and descendable arm (9) by means of a shaft (7) with a base perpendicular to the arm, and is movably controlled by a drive mechanism; a brush oscillating frame (32) rotated by a drive mechanism at the tip of the sub-arm, and which base rotates by means of a shaft (33′) perpendicular to the longitudinal direction of the sub-arm and a shaft at the tip of the arm; a brush swivelling frame (33) that is swivelled by a drive mechanism centering around the axis of the longitudinal direction of the brush oscillating frame; a brush arm (35, 36) attached to a hinge on both sides of the brush swivelling frame, disposed bendably in a plane which is parallel to the swivelling plane of the brush swivelling frame (33) and is bent by a drive mechanism; a center shaft of a rotating brush attached on brackets parallel to the brush swivelling frame and the brush arm (35, 36) mutually coupled with a universal joint, with their bases on the brush swivelling frame and the brush arm, and protruding perpendiculary to the swivelling plane of the brush swivelling frame; and a drive mechanism (34) to drive the rotating brush around the center axis.

Description: Background of the Invention This invention relates to a type of aircraft washing equipment for washing large aircraft efficiently. In the conventional method of washing an aircraft, the pressure applied to an aircraft's surface had to be maintained below a certain value. It was impossible to direct the detergent spray directly on the surfaces. In addition, because aircraft have rounded tops, sides and bellies, washing was time consuming and labor intensive, because the manual brushing of the surfaces was frequently necessary. Although it does not damage the aircraft body, this conventional method is inefficient. It is becoming increasingly difficult to handle the present volume of aircraft. GB-A-1 327 901 more specifically discloses a washing and dusting apparatus particularly for aircraft comprising an elongated boom structure pivotally mounted at its lower end on a support for pivotal movement of the boom structure about a horizontal axis and an adjustable arm having a shoulder, upper arm, elbow and wrist adjustments, pivotally mounted at its proximal end on the distal end of the elongated boom for rotation about a horizontal axis, a pair of generally cylindrical brushes being rotatably coupled to a distal tip of a telescopic member of the adjustable arm for changing the orientation of the brushes. Summary of the Invention The purpose of this invention is to provide aircraft washing equipment that can wash the outer surface of an aircraft with high efficiency, and yet can be operated by only one person. This aim is achieved by an aircraft washing equipment comprising an elongated arm which can be raised and lowered; a sub-arm pivotally mounted at the tip of the arm for rotation about a horizontal shaft perpendicular to the arm and movably controlled by a first drive mechanism; a brush pivoting frame rotatably mounted at the end of the sub-arm opposed to the horizontal shaft for rotation about a drive shaft perpendicular to the longitudinal direction of the sub-arm and to the horizontal shaft and movably controlled by a second drive mechanism; a brush swivelling frame rotatably fixed to the brush pivoting frame for rotation about a swivelling axis perpendicular to the drive shaft and swivelled by a third drive mechanism, characterized in that said brush swivelling frame is contained in a swivelling plane perpendicular to said swivelling axis and in that it further comprises two brush arms pivotally attached to hinges at opposite sides of the brush swivelling frame and pivotally movable by a fourth drive mechanism in a plane which is parallel to said swivelling plane; a plurality of center shafts for supporting a plurality of rotary brushes and arranged in parallel with said swivelling plane and said brush arms at a predetermined distance therefrom, said center shafts being rotatably mounted on brackets fixedly secured to the brush swivelling frame and the brush arms and protruding perpendicularly to the swivelling plane and to the brush ams, each of said center shafts being coupled to the adjacent one via a universal joint; and a fifth drive mechanism for rotationally driving said rotary brushes about said center shafts. Furthermore, each of the above mechanisms may be mounted on a truck with steerable and rotating wheels, and transversal wheels which are disposed perpendicularly from the fore to the back line of the truck, and protrude downward to release the steerable and rotating wheels from contact with the ground in order to move the truck transversally. Brief Description of the Drawings Figs. 1 through 8 depict one embodiment of the aircraft washing equipment according to this invention; Fig. 1 shows the entire apparatus ; Fig. 2 shows a side view of the truck; Fig. 3 shows a plan view indicating locations of the truck wheels; Fig. 4 shows a view of the mechanism that causes the transversal wheels to protrude; Fig. 5 shows a detailed side view of the boom, arm and their fore and back coupling; Fig. 6 shows a side view of the washing brush; Fig. 7 shows an expanded view of the part indicated by lines VII-VII in Fig. 6; and Fig. 8 shows an expanded view of the part indicated by lines VIII-VIII in Fig. 6. Detailed Description of Preferred Embodiments Figs. 1 through 8 are drawings of one embodiment of the aircraft washing equipment according to this invention, and Fig. 1 is an entire view of the aircraft washing equipment. Figs. 2 through 4 are drawings of a truck 1 which steerably runs on rotating wheels 51 driven by hydraulic motors. In the vicinity of each of the said rotating wheels 51 are fixed hydraulic motor driven transversal wheels 52 perpendicularly to the fore to back line of the truck 1. These transversal wheels have their bases movably fixed on the truck body 1a, and are located on the ends of the wheel arms 53 which extend to both sides of the truck body 1a. Hydraulic cylinders 54 are arranged near these transversal wheels on the wheel arms 53 and between the upper parts of the wheel arms 53 in the truck body member 1a. These hydraulic cylinders 54 downwardly protrude beyond the transversal wheels 52 to release the rotating wheels 51 from contact with the ground, and retract to return the rotating wheels 51 to the ground. A swivelling table 2 which swivels horizontally by means of a drive mechanism such as a pinion gear is fixed on the center of the width of the truck 1 in the front part. The width center section of the truck 1 forms a space 3 from front to back, excluding the part for the swivelling table 2. As shown in Fig. 2, on both sides of this space 3, a storage section 4 is present from front to back and from right to left. In front of the operator's seat 5 is the control panel for operating this equipment, as well as the driving equipment for the truck 1. The control panel is connected by means of a cord long enough for the operator to operate the equipment from the operator's seat 5 or even from outside the truck 1. The storage section 4 contains a fuel tank, an engine, a hydraulic pump, an oil tank to operate each part, washing water, a washing tank, washing liquid, a water pump, and an electronic control panel. Brackets 2a are fixed on a location corresponding to the diameter of the upper surface of the swivelling table 2. The base end of a boom 6 rotates on these brackets 2a with a horizontal shaft 7. Between the lower and intermediate section of the boom 6 and the ends of the brackets 2a on the edge of the swivelling table 2, both ends of a hydraulic cylinder 8 rotate with shafts 8a, 8b parallel to the horizontal shaft 7, as shown in detail in Fig. 5. On the tip of the boom 6, the boom 6 and an arm 9 are rotated by a shaft 10 parallel to the horizontal shaft 7, interposed by a bracket 9a installed on the base of the arm 9, so that the boom 6 and the arm 9 are parallel to each other and fixed at a specific distance from each other. Between the boom 6 and the arm 9, there is a hydraulic cylinder 13 which rotates by means of shafts 13a and 13b parallel to the horizontal shaft 7 on the brackets 11 and 12 which have both ends fixed to the upper and intermediate sections of the boom 6 and to the base of the arm 9. The arm 9 comprises an outer arm 9b and an inner arm 9c which extends telescopically, between which there is a hydraulic cylinder 14 which drives them telescopically. On the tip of the inner arm 9c, the base of the sub-arm 15 with its tip forming a "U" shaped fitting 15a rotates by means of a shaft 16 parallel to the horizontal shaft 7. The "U" shaped fitting 15a is formed so that a drive shaft 17, which extends beyond the tip, will be perpendicular to the longitudinal direction of the sub-arm 15 and the shaft 16. On the outer side of one of the legs of the "U" shaped fitting 15a, the driving hydraulic motor 18 rotates to drive the drive shaft 17. In addition, on the end of the inner arm 9c and the base of the sub-arm 15 are brackets 19 and 15b, on which a hydraulic cylinder 20 is fixed. Both ends of the cylinder are rotated by means of shafts 20a and 20b parallel to the horizontal shaft 7. The "U" shaped fitting 15a is connected to the washing brush 31 shown in Figs. 6 through 8. The washing brush 31 is structured as follows: The "U" shaped fitting 15a holds the base of a brush pivoting frame 32, with an inserted drive shaft 17. A stopper pin 17a prevents movement relative to the drive shaft 17. On the end of this brush pivoting frame 32, there is a rotatable gear 33a rotating around the longitudinal axis of the brush pivoting frame 32. A brush swivelling frame 33 is fixed on this gear 33a, in the direction of the diameter of the gear 33a. A small gear 34a, which engages the gear 33a, and a swivelling drive mechanism 34, comprising a hydraulic motor 34c rotated by reduction gears 34b, are fixed on the side of the brush pivoting frame 32. Brush arms 35 and 36 are fixed on both ends of the brush swivelling frame 33. These arms are within the plane on which the brush swivelling frame 33 swivels on hinges 35a and 36a. Parallel brush rotating shafts 33', 35', and 36' are provided at a certain distance from the brush swivelling frame 33 and the brush arms 35 and 36 respectively. These are coupled by universal joints 37. Both ends of the brush rotating shaft 33' have their bases fixed on both ends of the brush swivelling frame, rotate on the tips of the drive bracket 38 and support bracket 39, and protrude into the swivelling plane of the brush swivelling frame 33. The tips of the brush rotating shafts 35, 36 have their bases fixed on the end of the brush arms 35 and 36, and rotate on the tips of the support brackets 40 and 41 which protrude parallel to the brackets 38 and 39. Between the brackets 38 and 39 on both ends of the brush swivelling frame 33 and the intermediate section of the brush arms 35 and 36 are hydraulic cylinders 42 and 43, which rotate by means of shafts 42a and 43a, both ends of which protrude parallel to the brackets 38 and 39. In addition, on the tip of the drive bracket 38 is a sprocket 44 fixed on the brush rotating shaft 33', and a sprocket 45b of a hydraulic motor 45, which is fixed on the brush swivelling frame 33 by a fixing table 45a, is wound with a roller chain 46. Furthermore, the brush swivelling frame 33 and the brush arms 35 and 36 have jetting openings not shown, to jet out washing liquid and washing water, on brushes 33'', 35'', and 36'' on the brush rotating shafts 33', 35', and 36'. In the figure, part 47 is a sensor used to control the positions of the brushes relative to an aircraft surface. Next, explanations are given on how to use the aircraft washing equipment. When the aircraft washing equipment is not in use, the truck is housed in a garage with the arm 9 retracted by the hydraulic cylinder 14; the washing brush 31 is rotated upward to make the brush rotating shafts 33', 35', and 36' rest parallel to the arm; the swivelling table 2 with the hydraulic cylinder 8 is behind the boom 6; the hydraulic cylinder 8 and the hydraulic cylinder 13 are contracted to compact the boom 6 and the arm 9 in the space 3 extending from fore to aft of the truck 1, one lying over the other. To wash an aircraft with this equipment, an operator first confirms that the fuel, washing liquid and water tanks are filled, then drives the truck 1 on the rotating wheels 51 near to the aircraft to be washed. Next, the operator extends the steering of the wheels 51 and the hydraulic cylinder 54 to make the truck 1 ride on the transversal wheels 52, then drives it to the washing position. Then the operator uses the control panel in front of the operator's seat 5 to extend the hydraulic cylinders 8, 13, and 14 and swivels the swivelling table 2 to place the washing brush 31 close to the surface of the aircraft to be washed. Next, the operator moves the brushes 33'', 35'', and 36'' to fit the surface of the aircraft, by moving the sub-arm 15 using the extension and contraction of the hydraulic cylinder 20, pivoting the brush pivoting frame 32 using the drive hydraulic motor 18, swivelling the brush swivelling frame 33 using the swivelling drive mechanism 34, and bending the brush arms 35, 36 using the hydraulic cylinders 42 and 43. After this setting, the system is switched to automatic operation. Switching to automatic operation will rotate the brushes 33'', 35'', and 36'' and supply the washing liquid or water to the brushes. A signal from the sensor 47 automatically controls each drive mechanism for the sub-arm 15 and the washing brush section 31, causing the brushes 33'', 35'', and 36'' to follow the contour of the surface at a prescribed face pressure. The range that the parts farther from the sub-arm 15 can follow is large. In addition, because the positions of the washing brush section 31 can be altered by operating the boom 6, the arm 9 and the swivelling table 2, the ability of the washing brush section 31 to follow the contour makes it easy to wash a larger area if face fitting is conducted on the respective faces. The truck is moved if the washing brush section 31 can no longer reach a washing area even after maximum operation of the boom 6, the arm 9 and the swivelling table 2. In this case, the truck 1 with the running wheels 51 and the transversal wheels 52 can be easily moved. Thus, once the whole surface of an aircraft is divided into several blocks and face fitting is conducted on the surface of the respective blocks, the washing brush section 31 follows each face to wash the surface easily, thereby enabling one operator to wash easily the surface of a large aircraft. Further, the equipment can enlarge its washing area with only one face fitting by automatically controlling the whole system, including the drive of the boom 6, the arm 9 and the swivelling table 2. Moreover, because the truck 1 with the transversal wheels 52 and the running wheels 51 can move easily and precisely, it is possible to omit the swivelling table 2, by directly installing the base of the boom 6 so that it can rotate on the top of the truck 1.

Claims: Aircraft washing equipment comprising an elongated arm (9) which can be raised and lowered; a sub-arm (15) pivotally mounted at the tip of the arm (9) for rotation about a horizontal shaft (16) perpendicular to the arm (9) and movably controlled by a first drive mechanism (20); a brush pivoting frame (32) rotatably mounted at the end of the sub-arm (15) opposed to the horizontal shaft (16) for rotation about a drive shaft (17) perpendicular to the longitudinal direction of the sub-arm (15) and to the horizontal shaft (16) and movably controlled by a second drive mechanism (18); a brush swivelling frame (33) rotatably fixed to the brush pivoting frame (32) for rotation about a swivelling axis perpendicular to the drive shaft (17) and swivelled by a third drive mechanism (34), characterized in that said brush swivelling frame (33) is contained in a swivelling plane perpendicular to said swivelling axis and in that it further comprises two brush arms (35, 36) pivotally attached to hinges (35a, 36a) at opposite sides of the brush swivelling frame (33) and pivotally movable by a fourth drive mechanism (42, 43) in a plane which is parallel to said swivelling plane; a plurality of center shafts (33', 35', 36') for supporting a plurality of rotary brushes (33'', 35'', 36'') and arranged in parallel with said swivelling plane and said brush arms (35, 36) at a predetermined distance therefrom, said center shafts (33', 35', 36') being rotatably mounted on brackets (38, 39, 40, 41) fixedly secured to the brush swivelling frame (33) and the brush arms (35, 36) and protruding perpendicularly to the swivelling plane and to the brush ams (35, 36), each of said center shafts (33', 35', 36') being coupled to the adjacent one via a universal joint (37); and a fifth drive mechanism (45) for rotationally driving said rotary brushes (33'', 35'', 36'') about said center shafts (33', 35', 36'). Aircraft washing equipment with each mechanism as claimed in claim 1, mounted on a truck (1) with runnable and steerable wheels (51), and transversal wheels (52) which are disposed perpendicularly to the longitudinal axis of the truck, and protrude downward to release the steerable and rotating wheels (51) from contact with the ground in order to move the truck (1) transversally.

Inventors: SUZUKI TSUNEO C O SUZUKI MECHA, SUZUKI, TSUNEO, ,C/O SUZUKI MECHANICAL
Applicants: SUZUKI MECH E, SUZUKI MECHANICAL ENGINEERING CO., LTD.
Application year: 1990
Main classification: B64F5
IPC codes: B64F5