Damper device
US-2022056982-A1 · Feb 24, 2022 · US
US11965576B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11965576-B2 |
| Application number | US-202117380274-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 20, 2021 |
| Priority date | Aug 20, 2020 |
| Publication date | Apr 23, 2024 |
| Grant date | Apr 23, 2024 |
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A damper device includes a first rotor, a second rotor, an elastic coupling part elastically coupling the first and second rotors in a rotational direction, and a hysteresis generating mechanism. The hysteresis generating mechanism generates a hysteresis torque and includes a friction member. The friction member is configured to make frictional contact with the first or second rotor. The friction member does not make frictional contact with the first and second rotors in a first torsion angular range where torsion is caused from a neutral condition to a first side and a second side in the rotational direction. The friction member makes frictional contact with the first or second rotor so as to generate a hysteresis torque in a second torsion angular range exceeding the first torsion angular range. The friction member is set in a neutral position by actuation of the elastic coupling part in the neutral condition.
Opening claim text (preview).
What is claimed is: 1. A damper device, comprising: a first rotor by which torque is input into the damper device and arranged to be rotated about a rotational axis; a second rotor by which torque is output from the damper device and arranged to be rotated about the rotational axis, the second rotor disposed to be rotatable relative to the first rotor in a first rotational direction and in a second rotational direction that is opposite to the first rotational direction; an elastic coupling part including a first elastic member and a second elastic member, the elastic coupling part configured to elastically couple the first and second rotors in said first and second rotational directions; and a hysteresis generating mechanism configured to generate a hysteresis torque when torsion is caused by rotation of the second rotor relative to the first rotor, the hysteresis generating mechanism including a friction member configured to cause friction by sliding relative to the first or the second rotor, wherein the friction member of the hysteresis generating mechanism does not cause friction by sliding relative to either the first rotor or the second rotor in a first torsion angular range extending from a neutral condition where there is no torsion between the first and second rotors to a first angular amount of relative rotation in the first rotational direction and to the first angular amount of relative rotation in the second rotational direction, the friction member causes friction by sliding relative to the first or second rotor so as to generate the hysteresis torque in a second torsion angular range exceeding the first torsion angular range in the first rotational direction or the second rotational direction, the friction member is further configured to be held in a neutral position by contact with and compression of the first and second elastic members when the first and second rotors are in the neutral condition, the first rotor includes a first support portion with a width in the circumferential direction of the first rotor and a second support portion with a width in the circumferential direction of the first rotor, and the second rotor includes a first accommodation portion with a width in the circumferential direction of the second rotor and a second accommodation portion with a width in the circumferential direction of the second rotor, the width of the first accommodation portion being the same as the width of the first support portion and the width of the second accommodation portion being the same as the width of the second support portion, the first accommodation portion is disposed to overlap in part the first support portion and to be angularly offset from the first support portion in the first rotational direction when the first and second rotors are in the neutral condition, and the second accommodation portion is disposed to overlap in part the second support portion and to be angularly offset from the second support portion in the second rotational direction when the first and second rotors are in the neutral condition, and the first elastic member is compressed in the first support portion and the first accommodation portion when the first and second rotors are in the neutral condition, and the second elastic member is compressed in the second support portion and the second accommodation portion when the first and second rotors are in the neutral condition, the second elastic member actuated in parallel with the first elastic member and expansionary forces within the first and second elastic members counteracting each other when the first and second rotors are in the neutral condition to hold the first and second rotors in the neutral condition and the friction member in the neutral position. 2. The damper device according to claim 1 , wherein the amount of angular offset in the first rotational direction of the first accommodation portion relative to the first support portion is equal to the amount of angular offset in the second rotational direction of the second accommodation portion relative to the second support portion, the friction member does not cause friction by sliding relative to either the first rotor or the second rotor when the first and second rotors are rotated relative to each other from the neutral condition by an amount that is equal to the amount of angular offset between the first accommodation portion and the first support portion and between the second accommodation portion and the second support portion, and the friction member causes friction by sliding relative to either the first or the second rotor when the first and second rotors are rotated relative to each other by an amount that is greater than the amount of angular offset between the first accommodation portion and the first support portion and between the second accommodation portion and the second support portion. 3. The damper device according to claim 1 , wherein the friction member includes first and second contact surfaces that face in opposite rotational directions, with an end surface of one of the first and second elastic members being arranged to make contact with one of the first and second contact surfaces and an end surface of the other of the first and second elastic members being arranged to make contact with the other of the first and second contact surfaces. 4. The damper device according to claim 1 , wherein when in an uncompressed free state, the length of the first elastic member is the same as the widths of the first support portion and the first accommodation portion in the circumferential directions of the first and second rotors, respectively, and when in an uncompressed free state, the length of the second elastic member is the same as the widths of the second support portion and the second accommodation portion in the circumferential directions of the first and second rotors, respectively, the angular offset of the first accommodation portion relative to the first support portion causes 1) the first elastic member to transition from an initial compressed state thereof to its uncompressed free state and then to be recompressed as the first rotor rotates from the neutral condition in the first rotational direction with respect to the second rotor, and 2) the first elastic member to be further compressed from the initial compressed state thereof as the first rotor rotates from the neutral condition in the second rotational direction with respect to the second rotor, and the angular offset of the second accommodation portion relative to the second support portion causes 1) the second elastic member to transition from an initial compressed state thereof to its uncompressed free state and then to be recompressed as the first rotor rotates from the neutral condition in the second rotational direction with respect to the second rotor, and 2) the second elastic member to be further compressed from the initial compressed state thereof as the first rotor rotates from the neutral condition in the second rotational direction with respect to the second rotor. 5. The damper device according to claim 4 , wherein the first and second support portions each include a first support surface at a first-rotational-direction end thereof, and the first and second support portions each include a second support surface at a second-rotational-direction end thereof, the first and second accommodation portions each include a first accommodation surface at a first-rotational-direction end thereof, and the first and second accommodation portions each include a second accommodation surface at a second-rotational-direction end thereof, when compressed, the first elastic member is disposed between the first support surface and the second accommodation surface, and when compressed, the second elastic member is disposed be
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