Compressed air tool

Abstract

A turning device (11) for compressed air tools (10). which is operated by a compressed fluid, is provided with a housing (16) and with a rotor (12), which is rotatably arranged in a front housing part (17) and into whose turbine element the fluid, which is under pressure, can flow, has a braking arrangement (14) and a switch (36) for the compressed fluid, which is in operative connection with the braking arrangement (14) and is arranged on a rear housing part (21) in line with a compressed fluid supply conduit (26). So that such a turning device (11) requires fewer components and can be stopped in a simpler and faster way by means of a fluid switch (36), a sliding switch (36) is provided, which encloses the rear housing part (21) in the area of the supply conduit (26) and is provided with axially oriented control pins (41), which are connected, fixed against relative displacement, with a brake disk (44) of the braking arrangement (14).

Description

DESCRIPTION

[0001] The invention relates to a turning device operated by compressed air, for example for compressed air tools as described in the preamble to claim 1.

[0002] With such a turning device known from U.S. Pat. No. 5,186,603, the switch constitutes at least partially the rear housing part and can be rotated in a screw thread in relation to the front housing part and a housing cover which receives it. The supply with compressed fluid is opened or closed by means of this rotation. The braking arrangement is spring-loaded and is pressed on the rotor in the course of closing the compressed fluid supply conduit when the switch is turned.

[0003] The construction of this known turning device is comparatively elaborate and requires a multitude of components. Moreover, opening and closing the compressed fluid supply conduit cannot be performed with one hand and is therefore impractical and furthermore time-consuming because of the multitude of required revolutions.

[0004] It is the object of the present invention to create a turning device of the type mentioned at the outset which requires fewer components and which can be brought to a stop in a simpler and faster way by means of a fluid switch.

[0005] The characteristics recited in claim 1 are provided for attaining this object in a turning device of the type mentioned.

[0006] By means of the steps of the invention it is achieved that the switch is embodied as a simple sliding switch which cannot only be operated with one hand, but also in a very rapid manner. The direct opening and closing of the braking arrangement by means of the sliding switch is possible because of the slide-proof connection of the brake disk and the sliding switch without requiring further components.

[0007] A slide-proof guide for the control pins is achieved by means of the characteristics of claim 2. With the characteristics of claim 3, venting can take place simultaneously with the shutoff and braking of the rotor.

[0008] Advantageous embodiments in respect to opening and closing the compressed fluid supply conduit with the aid of the sliding switch ensue from the characteristics of one or several of claims 4 to 6.

[0009] Further details of the invention can be taken from the following description, in which the invention is described in greater detail and explained by means of the exemplary embodiment represented in the drawings.

[0010] FIG. 1 represents a compressed air tool provided with a turning device in accordance with a preferred exemplary embodiment of the invention in the switched off and braked position in longitudinal section and truncated form, and

[0011] FIG. 2 a truncated representation corresponding to FIG. 1, but in the operating position.

[0012] The compressed air tool 10 represented in the drawings has a turning device 11, which h as a rotor 12, for example in the form of a turbine, which can be charged with compressed air and in this way caused to rotate. The supply of compressed air can be turned on or off by means of a sliding switch 13, wherein a braking arrangement 14 acts on the rotor 12 simultaneously with the shutoff of compressed air by means of the sliding switch 13.

[0013] The compressed air tool 10 has an elongated housing 16 surrounding a drive shaft 18, which is connected, fixed against relative rotation, with the rotor 12 and is provided with a clamping chuck 19 on its end projecting out of the housing 16. The drive shaft 18 is rotatably seated in the housing 16 in the area close to the rotor 12, as well as in the area remote from the rotor 12 and close to the clamping chuck 19.

[0014] The front housing part 17, which faces the rear housing part 21 and can be connected with it, is embodied in a cup shape on one end 22. The cup-shaped end 22 is closed by a cover element 23 of the rear housing part 21. A tube element 24 of the rear housing part 21 passes through the cover element 23, which tube element 24 has an axially centered, axial supply conduit 26 for the compressed air. Here, the cover element 23 and the tube element 24 are one piece. The supply conduit 26 terminates in the turbine rotor 12. The supply conduit 26 is interrupted in the tube element 24 outside of the cover element 23. Several radial bypass conduits 31, or 32, which extend from the outer circumference of the tube element 24 and are respectively arranged evenly distributed over the circumference, terminate in the closed ends 27 and 28 of the supply conduit 26 which are facing each other. A sleeve-shaped slide 36 is axially movable on the tube element 24 provided with a smooth cylindrical exterior circumference 29 and provided with a connecting end 33 for a compressed air connection. The sleeve-shaped slide 36 is used as a switch for supplying and blocking compressed air supplied via the supply conduit 26 and used for driving the turning device 11. The slide 36 has an interior annular groove 37 which can connect the radial bypass conduits 31 and 32 of the two closed supply conduit ends 27 and 28 with each other. In accordance with FIG. 2, the annular groove 37 has a width corresponding to the radial bypass conduits 31 and 32, so that in the connected position of the sliding switch 36 the outlet openings of the radial bypass conduits 31 and 32 are covered by the annular groove 37 and are connected. An O-ring 33, or two O-rings 39 and 40, are arranged on both sides of the annular groove 37 and prevent leaks to the outside in the connected state and, in the state of the sliding switch 36 in which it interrupts the compressed air supply, the center O-ring 40 of which is arranged at a place between the two radial bypass conduits 31 and 32 (FIG. 1). In this position the bypass conduits 31 are not connected with the bypass conduits 32, so that the compressed air supply is interrupted.

[0015] The sleeve-shaped slide 36 has several, for example three, control pins 41, which are arranged evenly distributed over the circumference and extend in the axial direction. The control pins 41 are maintained with one end in blind bores 42 of the sleeve-shaped slide 36, pass through guide bores 43 in the cover element 23 in an axially movable manner and on their end located inside the cup-shaped end 22 of the front housing part 17 are connected, fixed against relative displacement, with a brake disk 44 of the braking arrangement 14. The brake disk 44, which is equipped with a ring-shaped brake lining 46, is axially movable on the inner end of the tube element 24 facing the rotor 12.

[0016] A connection, fixed against relative displacement, of the slide 36 with the brake disk 44 is provided with the aid of the axial control pins 41 so that, when the sliding switch 36 is in a position where it interrupts the supply of compressed air (FIG. 1), the brake disk 44 presses with its brake lining 46 against an annular front 47 of the rotor 12. In accordance with FIG. 2, when the compressed air supply is open, the brake disk 44 is at an axial distance from the rotor 12. The cover element 23 is furthermore provided with axial vent openings 48 for venting during operation.

[0017] Even though the turning device 11 has been described in connection with a compressed air tool 10, it is understood that the turning device 11 can also be employed with a tool operated by means of a different compressed fluid.

Claims

1. A turning device (11) operated by compressed air, for example for compressed air tools (10), having a housing (16) and a rotor (12), which is rotatably arranged in a front housing part (17) and into whose turbine element the fluid under pressure can flow, having a braking arrangement (14) and a switch (36) for the compressed fluid, which is in operative connection with the braking arrangement (14) and is arranged on a rear housing part (21) in line with a compressed fluid supply conduit (26), characterized in that a sliding switch (36) is provided, which encloses the rear housing part (21) in the area of the supply conduit (26) and is provided with axially oriented control pins (41), which are connected, fixed against relative displacement, with a brake disk (44) of the braking arrangement (14).

2. The turning device in accordance with claim 1, characterized in that the control pins (41) are guided in and through a cover (23) of the housing (16).

3. The turning device in accordance with claim 2, characterized in that the housing cover (23) is supplied with vent openings (48).

4. The turning device in accordance with at least one of claims 1 to 3, characterized in that the supply conduit (26) is interrupted in the rear housing part (21), and each end (27, 28) of the supply conduit (26) is connected with radial bypass conduits (31, 32) arranged in the rear housing part (21), whose outlet openings can be covered by the sliding switch (36).

5. The turning device in accordance with claim 4, characterized in that the sliding switch (36) has an interior annular compressed fluid groove (37), whose width corresponds to the axial distance of the bypass conduits (31, 32) from both ends (27, 28) of the supply conduit (26).

6. The turning device in accordance with claim 5, characterized in that seal rings (38, 39, 40) are provided in the sliding switch (36) at both sides of the annular groove (37), the center seal ring (40) of which separates the two bypass conduits (31, 32).