Rotary Damper and Manufacturing Method Thereof

Abstract

A rotary damper includes a lid (130) that closes an opening of a case (110), a protrusion (131) formed on the lid (130), and a groove (114) having an arc shape formed on the case (110). A bottom surface of the groove (114) has a gradient. The protrusion (131) moves in the groove (114) while contacting the bottom surface of the groove (114), thereby displacing the lid (130).

Claims

1. A method for manufacturing a rotary damper including a lid configured to close an opening of a case, the method comprising: placing the lid on the case so as to close the opening with the lid; measuring characteristics of the rotary damper in a state where pressure is applied to the lid in a vertical direction; fixing the lid without displacing the lid when a measurement result satisfies a set value; and displacing the lid and measuring the characteristics of the rotary damper again in a state where the pressure is applied to the lid in the vertical direction when the measurement result does not satisfy the set value.

2. The method according to claim 1, wherein when the lid is placed on the case, a protrusion formed on one of the lid and the case is brought into contact with a bottom surface having a gradient of a groove having an arc shape formed on the other of the lid and the case, and the lid is displaced by rotating the lid or the case while bringing the protrusion into contact with the bottom surface of the groove.

3. The method according to claim 2, wherein the protrusion has an arc shape, and a tip surface of the protrusion has a same gradient as the bottom surface of the groove.

4. The method according to claim 1, wherein when the lid is placed on the case, a protrusion formed on one of the lid and the case is brought into contact with a small protrusion within a recess formed on the other of the lid and the case, and the lid is displaced by applying pressure to the lid in the vertical direction such that the protrusion collapses the small protrusion.

5. The method according to claim 1, wherein a magnitude of the pressure applied to the lid during measurement is a magnitude that can resist an internal pressure during measurement.

6. The method according to claim 1, wherein the characteristics are an operating time or torque of a rotor housed in the case.

7. A rotary damper comprising: a lid configured to close an opening of a case; a protrusion configured to be formed on one of the lid and the case; and a groove having an arc shape formed on the other of the lid and the case, wherein a bottom surface of the groove has a gradient, and the protrusion can displace the lid by moving in the groove while being in contact with the bottom surface of the groove.

8. The rotary damper according to claim 7, wherein the protrusion has an arc shape, and a tip surface of the protrusion has a same gradient as the bottom surface of the groove.

9. A rotary damper comprising: a lid configured to close an opening of a case; a protrusion configured to be formed on one of the lid and the case; a recess formed on the other of the lid and the case; and a small protrusion formed in the recess, wherein the protrusion is fitted in the recess and supported by the small protrusion, and the protrusion can displace the lid by crushing the small protrusion.

Description

BRIEF DESCRIPTION OF DRAWINGS

[0012] FIG. 1 is a plan diagram of a rotary damper according to a first example.

[0013] FIG. 2 is a cross-sectional diagram taken along line A-A of FIG. 1.

[0014] FIG. 3 is a cross-sectional diagram taken along line B-B of FIG. 2.

[0015] FIG. 4 is a plan diagram of a case adopted in the first example.

[0016] FIG. 5 is an enlarged diagram of a portion C of FIG. 4.

[0017] FIG. 6 is a cross-sectional diagram of a point a of FIG. 5.

[0018] FIG. 7 is a cross-sectional diagram of a point b of FIG. 5.

[0019] FIG. 8 is a cross-sectional diagram of a point c of FIG. 5.

[0020] FIG. 9 is a bottom diagram of a lid adopted in the first example.

[0021] FIG. 10 is an enlarged diagram of a portion D of FIG. 9.

[0022] FIG. 11 is a cross-sectional diagram of a point d of FIG. 9.

[0023] FIG. 12 is a cross-sectional diagram of a point e of FIG. 9.

[0024] FIG. 13 is a cross-sectional diagram of a point f of FIG. 9.

[0025] FIG. 14 is a cross-sectional diagram illustrating a fitting state of a protrusion and a groove at the point b of FIG. 5.

[0026] FIG. 15 is a cross-sectional diagram illustrating a fitting state of a protrusion and a groove at the point b of FIG. 5.

[0027] FIG. 16 is a plan diagram of a rotary damper according to a second example.

[0028] FIG. 17 is a cross-sectional diagram taken along line E-E of FIG. 15.

[0029] FIG. 18 is a cross-sectional diagram taken along line F-F of FIG. 16.

[0030] FIG. 19 is a plan diagram of a case adopted in the first example.

[0031] FIG. 20 is a cross-sectional diagram taken along line G-G of FIG. 18.

[0032] FIG. 21 is an enlarged diagram of a portion H of FIG. 19.

[0033] FIG. 22 is a cross-sectional diagram of a lid adopted in the second example.

[0034] FIG. 23 is an enlarged diagram of a portion I of FIG. 21.

[0035] FIG. 24 is a cross-sectional diagram illustrating a fitting state of a protrusion and a recess.

[0036] FIG. 25 is a cross-sectional diagram illustrating a fitting state of a protrusion and a recess.

DESCRIPTION OF EMBODIMENTS

[0037] Hereinafter, an embodiment of the present invention will be described according to examples illustrated in the drawings.

First Example

[0038] First, a structure of a rotary damper according to the first example will be schematically described with reference to FIGS. 1 to 3. As illustrated in FIG. 1, the rotary damper according to the first example includes a case 110, a rotor 120, and a lid 130. As illustrated in FIG. 3, the case 110 has a peripheral wall 111 having a cylindrical shape. As illustrated in FIG. 2, one end of the peripheral wall 111 is closed by a bottom wall 112 integrally molded with the peripheral wall 111, and the other end of the peripheral wall 111 is closed by the lid 130. The lid 130 is fixed by swaging an end portion of the case 110. The rotor 120 is housed in the case 110 and supported by the case 110 and the lid 130. As illustrated in FIG. 3, oil chambers 140 partitioned by partition walls 113 are formed between the case 110 and the rotor 120, and the oil chambers 140 are filled with oil. The rotor 120 includes vanes 121 disposed in the oil chambers 140. As illustrated in FIG. 2, O-rings 150 for preventing oil leakage are disposed between the case 110 and the lid 130, between the lid 130 and the rotor 120, and between the rotor 120 and the case 110. The rotary damper according to the first example decelerates the rotational speed of the rotor 120 using the resistance of oil received by the vanes 121 by the rotation of the rotor 120.

[0039] Next, a feature of the case 110 adopted in the first example will be described with reference to FIGS. 4 to 8. As illustrated in FIG. 4, the case 110 adopted in the first example has grooves 114 having an arc shape. In order to horizontally support the lid 130, preferably, two or more grooves 114 are formed, and more preferably, three or more grooves 114 are formed. In the first example, four grooves 114 are formed at equal intervals. As illustrated in FIGS. 5 to 8, the grooves 114 have an L-shape in cross-section. The bottom surface of the groove 114 has a gradient that is inclined such that the depth of the groove 114 is shallowest at one end 115 of the groove 114 and deepest at the other end 116 of the groove 114. In FIG. 5, the depths of the groove 114 at a point a near the one end 115 of the groove 114, a point c near the other end 116 of the groove 114, and a point b intermediate between the points a and c are a>b>c.

[0040] Next, a feature of the lid 130 adopted in the first example will be described with reference to FIGS. 9 to 13. As illustrated in FIG. 9, the lid 130 adopted in the first example has the same number of protrusions 131 as the number of grooves 114 formed on the case 110. The shape of the protrusion 131 may be, for example, a cylinder, but is preferably the same shape as the groove 114, that is, an arc shape in order to increase the contact area between the tip surface of the protrusion 131 and the bottom surface of the groove 114. In the first example, four protrusions 131 having an arc shape are formed at equal intervals on the back surface of the lid 130. As illustrated in FIGS. 10 to 13, the tip surface of the protrusion 131 has a gradient that is inclined such that the length of the protrusion 131 is the longest at one end 132 of the protrusion 131 and the shortest at the other end 133 of the protrusion 131. In FIG. 10, the lengths of the protrusion 131 at a point d near the one end 132 of the protrusion 131, a point f near the other end 133 of the protrusion 131, and a point e intermediate between the points d and f are d>e>f. The gradient of the tip surface of the protrusion 131 is the same as the gradient of the bottom surface of the groove 114. Therefore, even when the protrusion 131 moves in the groove 114, the lid 130 is kept horizontal. Since the length of the protrusion 131 at the one end 132 of the protrusion 131 is longer than the depth of the groove 114 at the one end 115 of the groove 114, the protrusion 131 can move in the groove 114 between the one end 115 and the other end 116 of the groove 114 while bringing the tip surface into contact with the bottom surface of the groove 114.

[0041] Note that the rotary damper according to the first example has a structure including the lid 130 that closes the opening of the case 110, the protrusions 131 formed on the lid 130, and the grooves 114 having an arc shape formed on the case 110, but, alternatively, may have a structure including a lid that closes the opening of the case, protrusions formed on the case, and grooves having an arc shape formed on the lid.

[0042] Next, an example of a method for manufacturing the rotary damper according to the first example will be described. In this example, first, the rotor 120 is housed in the case 110, and oil is loaded into the oil chambers 140. Next, the lid 130 is placed on the case 110 such that the lid 130 closes the opening (the other end of the peripheral wall 111) of the case 110, and the protrusions 131 are inserted into the grooves 114 (see FIG. 14). The initial position of the one end 132 of the protrusion 131 can be arbitrarily set. In this example, the one end 132 of the protrusion 131 is positioned at the center of the groove 114 (point b in FIG. 5), but the one end 132 of the protrusion 131 may be positioned near the one end 115 of the groove 114 (point a in FIG. 5) or near the other end 116 of the groove 114 (point c in FIG. 5).

[0043] Next, the characteristics of the rotary damper are measured in a state where the pressure is applied to the lid 130 in the vertical direction. With this method, it is possible to know characteristics at the time of completion in a state where the lid 130 is not fixed, that is, in a state of not being finished as a product. In order to more accurately measure the characteristics without displacing the lid 130 in a state where the lid 130 is not fixed, the magnitude of the pressure applied to the lid 130 is preferably a magnitude that can resist the internal pressure at the time of measurement. The characteristics to be measured may be arbitrarily set, but in this example, is the operating time of the rotor 120. For the operating time of the rotor 120, for example, a shaft is coupled to a through-hole 122 formed in the rotor 120, and a certain rotational force is applied to the shaft to rotate the rotor 120. Then, the time required for the shaft to rotate a certain angle (for example, 120°) at this time is measured. Note that the characteristics to be measured may be torque. For the torque, for example, a shaft is coupled to the through-hole 122 formed in the rotor 120, and a torque for rotating the shaft is measured. In the rotary damper according to the first example, since the protrusion 131 is in contact with the bottom surface of the groove 114, the lid 130 can be stabilized in the same manner as at the time of completion by applying the pressure to the lid 130 in the vertical direction, and therefore the characteristics can be accurately measured.

[0044] The measurement value may not be uniform due to variations in dimensions of each component and/or viscosity of the oil even when the lid 130 is placed at the same position and measurement is performed. When the measurement result does not satisfy a set value, the characteristics of the rotary damper are measured again in a state where the lid 130 is displaced and the pressure is applied to the lid 130 in the vertical direction. The set value includes a tolerance that is a difference between the maximum value and the minimum value of an allowable error of the characteristics. The displacement of the lid 130 is performed by rotating the lid 130 while bringing the protrusion 131 formed on the lid 130 into contact with the bottom surface of the groove 114 formed on the case 110. In this example, by rotating the lid 130 in one direction, the protrusion 131 moves in the groove 114 toward the other end 116 of the groove 114, so that the position of the lid 130 can be lowered (see FIG. 15). In addition, by rotating the lid 130 in the reverse direction, the protrusion 131 moves in the groove 114 toward the one end 115 of the groove 114, so that the position of the lid 130 can be raised. Note that the case 110 may be rotated without rotating the lid 130. In the rotary damper according to the first example, the lid 130 can be rotated using projections 134 formed on the surface of the lid 130 (see FIGS. 1 and 2). In order to displace the lid, a structure in which a step having a staircase shape is provided at the bottom of the groove can also be adopted as a structure different from that of the first example. In this case, the lid can be displaced by the movement of the protrusion along the step, but since the position of the lid is determined in stages, it is difficult to finely adjust the position of the lid. In this respect, in the rotary damper according to the first example, the bottom surface of the groove 114 is an inclined surface, and the lid 130 is displaced by the movement of the protrusion 131 along the inclined surface, so that the position of the lid 130 can be finely adjusted. In addition, since the protrusion 131 can move in both directions in the groove 114, the position of the lid 130 can be raised as well as lowered from the initial position. With this method, even when the initial measurement result does not satisfy the set value, the characteristics can be changed so that the measurement value becomes the set value, and, therefore, even when there is a variation in the dimension of each component and/or the viscosity of the oil, more uniform characteristics can be obtained. In addition, the tolerance width of the characteristics can be made much narrower than the conventional design. For example, the tolerance width of the characteristics can be ⅓ or less of the conventional design.

[0045] When the measurement result satisfies the set value, the lid 130 is fixed without displacing the lid 130 (that is, at the position of the lid 130 at the time of measurement). In the rotary damper according to the first example, the lid 130 is fixed by swaging the end portion of the case 110, but the lid 130 may be fixed by a method such as welding.

Second Example

[0046] Next, a structure of a rotary damper according to the second example will be schematically described with reference to FIGS. 16 to 18. As illustrated in FIG. 16, the rotary damper according to the second example includes a case 210, a rotor 220, and a lid 230. As illustrated in FIG. 18, the case 210 has a peripheral wall 211 having a cylindrical shape. As illustrated in FIG. 17, one end of the peripheral wall 211 is closed by a bottom wall 212 integrally molded with the peripheral wall 211, and the other end of the peripheral wall 211 is closed by the lid 230. The lid 230 is fixed by swaging an end portion of the case 210. The rotor 220 is housed in the case 210 and supported by the case 210 and the lid 230. As illustrated in FIG. 18, oil chambers 240 partitioned by partition walls 213 are formed between the case 210 and the rotor 220, and the oil chambers 240 are filled with oil. The rotor 220 includes vanes 221 disposed in the oil chambers 240. As illustrated in FIG. 17, O-rings 250 for preventing oil leakage are disposed between the case 210 and the lid 230, between the lid 230 and the rotor 220, and between the rotor 220 and the case 210. The rotary damper according to the second example decelerates the rotational speed of the rotor 220 using the resistance of oil received by the vanes 221 by the rotation of the rotor 220.

[0047] Next, a feature of the case 210 adopted in the second example will be described with reference to FIGS. 19 to 21. As illustrated in FIG. 19, the case 210 adopted in the second example has recesses 214 having a circular shape. In order to horizontally support the lid 230, preferably, two or more recesses 214 are formed. As illustrated in FIG. 20, in the second example, two recesses 214 are formed in the partition walls 213 integrally molded with the peripheral wall 211 and the bottom wall 212. As illustrated in FIG. 21, small protrusions 215 are formed in the recesses 214.

[0048] Next, a feature of the lid 230 adopted in the second example will be described with reference to FIGS. 22 to 23. As illustrated in FIG. 22, the lid 230 adopted in the second example has the same number of protrusions 231 as the number of recesses 214 formed in the case 210. In the second example, two protrusions 231 are formed on the back surface of the lid 230. The protrusion 231 illustrated in FIG. 23 can crush the small protrusions 215.

[0049] Note that the rotary damper according to the second example has a structure including the lid 230 that closes the opening of the case 210, the protrusions 231 formed on the lid 230, the recesses 214 formed on the case 210, and the small protrusions 215 formed in the recesses 214, but, alternatively, may have a structure including a lid that closes the opening of the case, protrusions formed on the case, recesses formed on the lid, and small protrusions formed in the recesses.

[0050] Next, an example of a method for manufacturing the rotary damper according to the second example will be described. In this example, first, the rotor 220 is housed in the case 210, and oil is loaded into the oil chambers 240. Next, the lid 230 is placed on the case 210 such that the lid 230 closes the opening (the other end of the peripheral wall 211) of the case 210, and the protrusions 231 are fitted into the recesses 214 (see FIG. 24). The initial position of the tip of the protrusion 231 can be arbitrarily set. In this example, the tip of the protrusion 231 is disposed at a position where the small protrusions 215 are slightly crushed by the protrusion 231 (see FIG. 24).

[0051] Next, the characteristics of the rotary damper are measured in a state where the pressure is applied to the lid 230 in the vertical direction. With this method, it is possible to know characteristics at the time of completion in a state where the lid 230 is not fixed, that is, in a state of not being finished as a product. In order to more accurately measure the characteristics without displacing the position of the lid 230 in a state where the lid 230 is not fixed, the magnitude of the pressure applied to the lid 230 is preferably a magnitude that can resist the internal pressure at the time of measurement. The characteristics to be measured may be arbitrarily set, but in this example, is the operating time of the rotor 220. Note that the characteristics to be measured may be torque. In the rotary damper according to the second example, since the protrusion 231 is fitted to the recess 214 and supported by the small protrusions 215, the lid 230 can be stabilized in the same manner as at the time of completion by applying the pressure to the lid 230 in the vertical direction, and therefore the characteristics can be accurately measured.

[0052] The measurement value may not be uniform due to variations in dimensions of each component and/or viscosity of the oil even when the lid 230 is placed at the same position and measurement is performed. When the measurement result does not satisfy a set value, the characteristics of the rotary damper are measured again in a state where the lid 230 is displaced and the pressure is applied to the lid 230 in the vertical direction. The displacement of the lid 230 is performed by crushing the small protrusions 215 formed on the case 210 with the protrusion 231 formed on the lid 230. In this example, by applying the pressure in the vertical direction larger than that at the time of measurement to the lid 230, the protrusion 231 further crushes the small protrusions 215, so that the position of the lid 230 can be lowered (see FIG. 25). Since the position of the lid 230 is determined by the extent that the protrusion 231 crushes the small protrusions 215, the position of the lid 230 can be finely adjusted. With this method, even when the initial measurement result does not satisfy the set value, the characteristics can be changed so that the measurement value becomes the set value, and, therefore, even when there is a variation in the dimension of each component and/or the viscosity of the oil, more uniform characteristics can be obtained. In addition, the tolerance width of the characteristics can be made much narrower than the conventional design. For example, the tolerance width of the characteristics can be ⅓ or less of the conventional design.

[0053] When the measurement result satisfies the set value, the lid 230 is fixed without displacing the lid 230 (that is, at the position of the lid 230 at the time of measurement). In the rotary damper according to the second example, the lid 230 is fixed by swaging the end portion of the case 210, but the lid 230 may be fixed by a method such as welding.

REFERENCE SIGNS LIST

[0054] 110 Case

[0055] 111 Peripheral wall

[0056] 112 Bottom wall

[0057] 113 Partition wall

[0058] 114 Groove

[0059] 115 One end of groove

[0060] 116 Other end of groove

[0061] 120 Rotor

[0062] 121 Vane

[0063] 122 Through-hole

[0064] 130 Lid

[0065] 131 Protrusion

[0066] 132 One end of protrusion

[0067] 133 Other end of protrusion

[0068] 134 Projection

[0069] 140 Oil chamber

[0070] 150 O-ring

[0071] 210 Case

[0072] 211 Peripheral wall

[0073] 212 Bottom wall

[0074] 213 Partition wall

[0075] 214 Recess

[0076] 215 Small protrusion

[0077] 220 Rotor

[0078] 221 Vane

[0079] 230 Lid

[0080] 231 Protrusion

[0081] 240 Oil chamber

[0082] 250 O-ring