WO2015022982A1 - 樹脂トルクロッド - Google Patents
樹脂トルクロッド Download PDFInfo
- Publication number
- WO2015022982A1 WO2015022982A1 PCT/JP2014/071412 JP2014071412W WO2015022982A1 WO 2015022982 A1 WO2015022982 A1 WO 2015022982A1 JP 2014071412 W JP2014071412 W JP 2014071412W WO 2015022982 A1 WO2015022982 A1 WO 2015022982A1
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- WIPO (PCT)
- Prior art keywords
- ribs
- rib
- central axis
- torque rod
- ring
- Prior art date
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K5/00—Arrangement or mounting of internal-combustion or jet-propulsion units
- B60K5/12—Arrangement of engine supports
- B60K5/1208—Resilient supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K5/00—Arrangement or mounting of internal-combustion or jet-propulsion units
- B60K5/12—Arrangement of engine supports
- B60K5/1241—Link-type support
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
- F16F1/3842—Method of assembly, production or treatment; Mounting thereof
- F16F1/3849—Mounting brackets therefor, e.g. stamped steel brackets; Restraining links
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
- F16F15/08—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with rubber springs ; with springs made of rubber and metal
Definitions
- the present invention relates to a torque rod, and particularly relates to a torque rod provided with a plurality of ribs.
- a torque rod as a vibration isolator used when an engine is attached to a vehicle body is known.
- a resin torque rod made of resin is also known.
- JP 2010-19323 A Japanese Patent No. 5095577
- the resin torque rod becomes relatively large when required strength and durability are increased, it is required to make the resin torque rod as compact as possible to improve attachment to the vehicle body.
- rigidity must not be lost for compactness. Therefore, it is desired to be highly rigid and compact. The present application aims to realize such a request.
- the invention described in claim 1 is a resin torque rod in which ring portions are integrally provided at both ends in the length direction of the rod portion (12).
- a plurality of lateral ribs (50, 44, 54A, 54B) projecting in a direction orthogonal to the direction of the central axis (C2) are provided on the outer peripheral surface of at least one ring portion (16), and the protruding height of each lateral rib
- the protruding height of each lateral rib is highest at the central portion in the central axis (C2) direction, and gradually decreases toward both sides in the central axial line (C2) direction.
- the protruding height of the lateral ribs (54A, 54B) in the central axis (C2) direction is the depth of the groove between the adjacent lateral ribs (54A, 54B). It is characterized in that it changes non-uniformly due to the change in height.
- each of the lateral ribs formed at intervals in the direction of the central axis (C2) has a longitudinal length formed in the direction of the central axis (C2). It is connected and integrated by a rib (52).
- the vertical rib (52) is inclined so that a middle portion in the central axis (C2) direction protrudes outward most. It is characterized by.
- predetermined rigidity is ensured by the plurality of lateral ribs (50, 44, 54A, 54B), and the protruding height of the lateral rib is gradually lowered in the direction of the central axis (C2). Since the contour in the direction of the central axis (C2) is inclined so that the protrusion height decreases toward the axial end direction of the central axial line (C2), the axial direction of the central axial line (C2) It becomes compact in. Moreover, since only the protrusion height is changed without reducing the number of the lateral ribs, the necessary rigidity can be ensured at the same time.
- the protrusion height protrudes most outward in the central portion in the central axis (C2) direction, and gradually decreases on either side toward both axial ends in the central axis (C2) direction.
- both axial directions of the central axis (C2) can be made compact.
- the necessary rigidity on both axial sides of the central axis (C2) can be ensured at the same time.
- the lateral ribs (54 ⁇ / b> A, 54 ⁇ / b> B) have the protrusion height changed non-uniformly by changing the depth of the groove between the adjacent lateral ribs (54 ⁇ / b> A, 54 ⁇ / b> B). Therefore, the cooling property can be improved and the generation of voids can be prevented.
- the horizontal ribs are connected and integrated by the vertical ribs that are long in the direction of the central axis (C2), the overall rigidity of the horizontal ribs can be increased.
- the vertical rib (52) is inclined inward toward both sides in the central axis (C2) direction so that the central portion in the central axis (C2) direction protrudes most outward.
- the vertical rib (52) portion can be prevented from protruding more than necessary.
- the torque rod 10 includes a rod-shaped rod portion 12 and a main body portion 18 in which a first ring portion 14 and a second ring portion 16 are integrally formed with a known appropriate resin such as FRP at both longitudinal ends thereof.
- the first ring portion 14 includes a ring hole 15 (see FIG. 4), and is connected to the first inner member 22 via a first elastic body 20 disposed on the inner side.
- the first elastic body 20 is made of an appropriate elastic material such as rubber, and the first ring portion 14 and the first inner member 22 are elastically coupled by appropriate means such as vulcanization adhesion.
- the first inner member 22 is a pipe member made of metal or the like, and is attached to an engine (not shown) by a bolt (not shown) passed through the first inner member 22.
- the second ring portion 16 includes a ring hole 17 (see FIG. 4), and is coupled to the second inner member 32 via a second elastic body 30 disposed on the inner side.
- the second elastic body 30 is made of an appropriate elastic material such as rubber, and elastically couples the second ring portion 16 and the second inner member 32 by appropriate means such as vulcanization adhesion.
- the second inner member 32 is a pipe member made of metal or the like, and is attached to a vehicle body (not shown) by a bolt (not shown) passed through the second inner member 32.
- the center of the first ring portion 14 is O1
- the center of the second ring portion 16 is O2
- a straight line connecting them is a center line C0.
- the central axis of the first ring portion 14 is C1
- the width is W1 (FIG. 2)
- the central axis of the second ring portion 16 is C2
- the width is W2 (FIG. 1).
- the center axis C1 is also the axis of the first inner member 22, and the center O1 is in the middle of the width W1 on the center axis C1.
- the center axis C2 is also the axis of the second inner member 32
- the center O2 is the middle of the width W2 on the center axis C2.
- the central axes C1 and C2 are orthogonally twisted by 90 °.
- the torque rod that is the subject of the present invention is not limited to such a torsion type, and the center axes C1 and C2 may be parallel.
- the center line C0 is orthogonal to these center axes C1 and C2.
- the rod portion 12 is provided symmetrically with respect to the center line C0 (see FIG. 2), and the center line C0 is also the center line of the rod portion 12.
- the direction of the center line C0 is the front-rear direction
- the direction of the center axis C2 is the up-down direction
- the left side in FIG. In FIG. 2 the direction of the central axis C1 is the left-right direction
- the upper side of the figure is the right side.
- the second elastic body 30 has an arm portion 34 that extends from the second inner member 32 to the left and right, and forms a vibration-proof main portion.
- the arm portion 34 has a substantially V-shape convex forward in plan view and expands rearward, and the second inner member 32 faces the stopper 38 through a piercing hole 36 penetrating in the vertical direction. .
- a straight hole 39 penetrating in the vertical direction is also formed on the front side of the arm portion 34.
- the columnar portion 42 extends rearward along the center line C ⁇ b> 0 and continues to the cylindrical portion 47 of the second ring portion 16.
- the cylindrical portion 47 surrounds the ring hole 17 and has a relatively thin ring shape surrounded by the central groove 45 and the deep groove 56B. Using this as a base, each horizontal rib and vertical rib 52 (described later) are in the radial direction. It protrudes outward.
- a connecting portion between the cylindrical portion 47 and the columnar portion 42 forms a substantially triangular thick portion 48, and a substantially triangular hollow hole 49 is opened downward (see FIG. 4).
- the second ring portion 16 is formed larger than the first ring portion 14 and has a substantially rectangular shape in plan view.
- This shape is a shape of a lateral rib composed of the first rib 50 and the second ribs 54A and 54B.
- a plurality of lateral ribs of the second ring portion 16 are provided.
- the ribs in the front half of the second ring portion 16 form the first rib 50 on the top and bottom, and the first rib 50 is continuous with the top and bottom ribs 40 on the front rod portion 12.
- the rear portions of the first ribs 50 are connected by vertical vertical ribs 52 on the side of the second inner member 32, and are continuous with the second ribs 54 ⁇ / b> A via the vertical ribs 52.
- the upper surface (lower surface) is an integral one in which the first rib 50 and the second rib 54A are continuous.
- the rear portion of the intermediate rib 44 is a portion that continuously extends rearward from the rod portion 12, and each rear end portion is continuous with the vertical rib 52.
- An upper and lower groove 41 is formed between the intermediate rib 44 and the upper and lower ribs 40 in the longitudinal direction along the intermediate rib 44.
- Each rear end portion 41 b of the upper and lower grooves 41 extends rearward in parallel with the center line C 0 so as to engrave the outer peripheral surface of the second ring portion 16 and is connected to the vertical rib 52.
- the central groove 45 extends rearward along the center line C0, and further extends rearward across the vertical rib 52.
- a plurality of second ribs 54 ⁇ / b> A and 54 ⁇ / b> B are formed in parallel on the outer peripheral surface of the second ring portion 16 behind the vertical rib 52.
- a total of four second ribs 54A are formed in parallel, two above and below across the extension (groove 56B) of the central groove 45, and the protrusion height is relatively low.
- Two second ribs 54B are provided, are parallel to each other with the center line C0 interposed therebetween, and have a relatively high protruding height.
- the rear end positions of the second ribs 54A and 54B are the same. Therefore, the change in the protruding height is formed by the depth of the groove formed between the second ribs 54A and 54B. That is, only the groove 56B between the pair of second ribs 54B having a high protruding height is deep, and the other grooves 56A are relatively shallow.
- each groove 56A is connected to the left and right vertical ribs 52.
- the deep groove 56B is formed on the center line C0, and the left and right end portions are continuous with the central groove 45 that crosses the left and right vertical ribs 52.
- FIG. 6 is a side view showing the second ring portion 16 from the rear.
- the left and right end portions of the second ribs 54A and 54B are inclined along the straight lines L1 and L2.
- the straight line L1 is inclined so as to converge gradually toward the central axis C2, and the left and right protruding ends of the second ribs 54A and 54B above the groove 56B are along the straight line L1.
- the height of the second ribs 54A and 54B which are horizontal ribs, projecting in the left-right direction becomes lower toward the upper side, and the height of each rib in the left-right direction gradually changes upward. Is uneven.
- the inclination of the straight line L1 is also the inclination of the vertical rib 52.
- the vertical ribs 52 are inclined along the straight lines L1 and L2.
- the protruding left and right ends of the second ribs 54A and 54B below the groove 56B are along a straight line L2 that is opposite to the straight line L1.
- the angle formed with the central axis C2 of the straight line L2 is the same as that of the straight line L1.
- the second ribs 54A and 54B, which are lateral ribs below the groove 56B also have uneven projection heights in the left-right direction.
- FIG. 7 is a reverse side view showing the first ring portion 14 and the second ring portion 16 from the front.
- the second ring portion 16 extends along the vertical rib 52 where the left and right protruding end portions of the upper and lower ribs 40 and the intermediate rib 44 are inclined along the straight lines L1 and L2 even when viewed from the front. Have changed. Therefore, the protruding height in the left-right direction of each horizontal rib is also uneven on the first half side of the second ring portion 16.
- the horizontal ribs before and after the second ring portion 16 do not necessarily need to have the same vertical inclination, and may be different.
- the inclination can be made different on the left and right.
- the inclination angles of the straight lines L1 and L2 can be freely adjusted.
- the 2nd ring part 16 changes the number of horizontal ribs before and behind the vertical rib 52 as a boundary, decreases the front side, and increases the back side.
- the front side having a relatively low required rigidity can be lightened by increasing the thickness.
- the rear side having a relatively high required rigidity increases the rigidity by providing a larger number of lateral ribs.
- the vertical ribs 52 connect the upper and lower first ribs 50 and the intermediate ribs 44 as the front side ribs and the second ribs 54A and 54B as the rear side ribs, whereby the rigidity of the entire horizontal ribs is increased. Is higher.
- each horizontal rib itself is also increased by widening the protruding width of the horizontal rib.
- the projecting heights of the horizontal ribs in the left-right direction are inclined so as to be lower in the upper and lower directions, the vertical protrusion in the left-right direction can be reduced.
- the left and right direction can be made relatively compact while ensuring the required high rigidity.
- the vertical space in the left and right direction of the second ring portion 16 between the peripheral member 60 and the peripheral member 60 Even in a case where the width becomes narrower, it can be easily arranged.
- the protrusion height of each horizontal rib was made non-uniform
- the rear end portions of the respective horizontal ribs have the same height in the vertical direction.
- the protrusions of the respective horizontal ribs can be made uneven by inclining the front end side of each horizontal rib protruding in the left-right direction.
- channel of the up-down direction intermediate part forms the center groove
- 10 torque rod
- 12 rod part
- 14 first ring part
- 16 second ring part
- 44 intermediate rib
- 45 central groove
- 50 first rib
- 52 vertical rib
- 54A second rib
- 54B second rib
- 56A groove
- 56B groove
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
- Vibration Prevention Devices (AREA)
- Springs (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
Description
また、リブを湾曲させたものもある(特許文献2参照)。
したがって、高剛性でかつコンパクトにすることが望まれる。本願はこのような要請の実現を目的とする。
少なくとも一方のリング部(16)の外周面に、その中心軸線(C2)の方向と直交する方向へ張り出す横リブ(50、44、54A、54B)を複数設けるとともに、各横リブの突出高さが中心軸線(C2)方向へ直線状に傾斜していることを特徴とする樹脂トルクロッド。
しかも、横リブの数は減らさず突出高さのみ変化させるだけなので、必要な剛性を同時に確保することができる。
第2内側部材32は金属製等のパイプ部材であり、ここに通した図示しないボルト等により図示しない車体へ取付けられている。
各中心軸線C1とC2は直交して互いに90°ねじれている。但し、本願発明の対象となるトルクロッドはこのようなねじれタイプだけでなく、各中心軸線C1及びC2が平行するものでもよい。
腕部34は平面視で前方へ凸の略V字状をなし、後方へ向かって拡開し、第2内側部材32は上下方向へ貫通するすぐり穴36を介してストッパ38と対向している。
腕部34の前方側にも上下方向に貫通するすぐり穴39が形成されている。
円筒部47と柱状部42の連結部は略三角形状の肉厚部48をなし、ここに略三角形状の肉抜き穴49が下方へ開放されて形成されている(図4参照)。
このうち、第2リング部16の前半部におけるリブは、上下が第1リブ50をなし、この第1リブ50は前方のロッド部12における上下リブ40と連続している。
第1リブ50の後部は第2内側部材32の側方にて、上下方向の縦リブ52で連結され、縦リブ52を介して第2リブ54Aに連続している。上面(下面)は第1リブ50と第2リブ54Aが連続する一体のものになっている。
上下部溝41の各後端部41bは、第2リング部16の外周面を彫り込むようにして中心線C0と平行に後方へ延びて縦リブ52に接続している。
中央溝45は中心線C0に沿って後方へ延び、縦リブ52を横切ってさらに後方へ延びている。
なお、各溝56Aの左右端部は左右の縦リブ52に接続している。一方、深い溝56Bは中心線C0上に形成され、左右端部は左右の縦リブ52を横切る中央溝45に連続している。
また、各直線L1及びL2の傾斜角は自由に調整できる。
また、前方側の横リブである上下の第1リブ50及び中間リブ44と、後部側の横リブである第2リブ54A及び54Bとを縦リブ52で連結することにより、横リブ全体の剛性をより高めている。
44:中間リブ、45:中央溝、50:第1リブ、52:縦リブ、54A:第2リブ、54B:第2リブ、56A:溝、56B:溝
Claims (5)
- ロッド部(12)の長さ方向両端にリング部を一体に設けた樹脂製のトルクロッドにおいて、
少なくとも一方のリング部(16)の外周面に、その中心軸線(C2)の方向と直交する方向へ張り出す横リブ(50、44、54A、54B)を複数設けるとともに、各横リブの突出高さが中心軸線(C2)方向へ直線状に傾斜していることを特徴とする樹脂トルクロッド。 - 各横リブの突出高さは、中心軸線(C2)方向中央部が最も高く、中心軸線(C2)方向両側へ向かって次第に低くなることを特徴とする請求項1のトルクロッド。
- 中心軸線(C2)方向における横リブ(54A、54B)の突出高さは、隣り合う横リブ(54A、54B)間の溝の深さが変化することにより、不均一に変化することを特徴とする請求項1又は2に記載した樹脂トルクロッド。
- 中心軸線(C2)方向に間隔をもって形成された各横リブは、中心軸線(C2)方向に長く形成された縦リブ(52)により連結一体化されていることを特徴とする請求項1~3のいずれか1項に記載した樹脂トルクロッド。
- 縦リブ(52)は、中心軸線(C2)方向中間部が最も外方へ突出するように傾斜していることを特徴とする請求項1~4のいずれか1項に記載した樹脂トルクロッド。
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE112014003740.0T DE112014003740T5 (de) | 2013-08-14 | 2014-08-13 | Kunststoff-Drehmomentstab |
CN201480041499.9A CN105408659B (zh) | 2013-08-14 | 2014-08-13 | 树脂转矩杆 |
US14/902,718 US9796255B2 (en) | 2013-08-14 | 2014-08-13 | Resin torque rod |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2013168737A JP6189673B2 (ja) | 2013-08-14 | 2013-08-14 | 樹脂トルクロッド |
JP2013-168737 | 2013-08-14 |
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WO2015022982A1 true WO2015022982A1 (ja) | 2015-02-19 |
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PCT/JP2014/071412 WO2015022982A1 (ja) | 2013-08-14 | 2014-08-13 | 樹脂トルクロッド |
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US (1) | US9796255B2 (ja) |
JP (1) | JP6189673B2 (ja) |
CN (1) | CN105408659B (ja) |
DE (1) | DE112014003740T5 (ja) |
WO (1) | WO2015022982A1 (ja) |
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US20170167559A1 (en) * | 2015-12-11 | 2017-06-15 | Hyundai Motor Company | Structure of mounting bracket |
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ES2706414T3 (es) * | 2013-10-02 | 2019-03-28 | Nhk Spring Co Ltd | Miembro de brazo de suspensión |
US9815361B2 (en) * | 2015-07-29 | 2017-11-14 | Fca Us Llc | Split bushing torque strut isolator assembly |
JP6570967B2 (ja) * | 2015-10-28 | 2019-09-04 | 株式会社ブリヂストン | トルクロッド |
JP6855189B2 (ja) * | 2016-08-25 | 2021-04-07 | 株式会社ブリヂストン | トルクロッド |
FR3057541B1 (fr) * | 2016-10-14 | 2019-03-29 | Airbus Helicopters | Amortisseur de trainee integre a l'interieur d'une pale d'un rotor |
KR102479485B1 (ko) * | 2016-12-13 | 2022-12-19 | 현대자동차주식회사 | 분산된 스토퍼들을 가지는 자동차의 트랜스미션 마운트 |
JP6824771B2 (ja) * | 2017-02-16 | 2021-02-03 | Toyo Tire株式会社 | トルクロッド及びその製造方法 |
JP6424299B1 (ja) * | 2017-04-25 | 2018-11-14 | 住友理工株式会社 | トルクロッド |
KR20210153256A (ko) * | 2020-06-10 | 2021-12-17 | 현대자동차주식회사 | 자동차용 트랜스미션 마운트 |
JP2022090754A (ja) * | 2020-12-08 | 2022-06-20 | 山下ゴム株式会社 | トルクロッド |
FR3119654B1 (fr) * | 2021-02-09 | 2023-05-26 | Hutchinson | Support antivibratoire et véhicule comportant un tel support antivibratoire. |
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JP2009115109A (ja) * | 2007-11-01 | 2009-05-28 | Toyo Tire & Rubber Co Ltd | 防振連結ロッド |
JP2010019323A (ja) * | 2008-07-09 | 2010-01-28 | Bridgestone Corp | トルクロッド |
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JP4589612B2 (ja) * | 2003-09-05 | 2010-12-01 | 株式会社ブリヂストン | 防振装置 |
JP4694815B2 (ja) * | 2004-10-15 | 2011-06-08 | 株式会社ブリヂストン | トルクロッド及びその製造方法 |
JP4722883B2 (ja) * | 2007-06-20 | 2011-07-13 | 山下ゴム株式会社 | トルクロッド |
JP5913848B2 (ja) * | 2011-07-13 | 2016-04-27 | 日産自動車株式会社 | トルクロッド |
DE102011052398B4 (de) * | 2011-08-04 | 2016-11-17 | Benteler Automobiltechnik Gmbh | Lageranordnung |
DE112013004015T5 (de) * | 2012-08-11 | 2015-05-07 | Yamashita Rubber Kabushiki Kaisha | Schwingungsisoliervorrichtung |
-
2013
- 2013-08-14 JP JP2013168737A patent/JP6189673B2/ja active Active
-
2014
- 2014-08-13 DE DE112014003740.0T patent/DE112014003740T5/de not_active Withdrawn
- 2014-08-13 CN CN201480041499.9A patent/CN105408659B/zh active Active
- 2014-08-13 US US14/902,718 patent/US9796255B2/en active Active
- 2014-08-13 WO PCT/JP2014/071412 patent/WO2015022982A1/ja active Application Filing
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009115109A (ja) * | 2007-11-01 | 2009-05-28 | Toyo Tire & Rubber Co Ltd | 防振連結ロッド |
JP2010019323A (ja) * | 2008-07-09 | 2010-01-28 | Bridgestone Corp | トルクロッド |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20170167559A1 (en) * | 2015-12-11 | 2017-06-15 | Hyundai Motor Company | Structure of mounting bracket |
Also Published As
Publication number | Publication date |
---|---|
DE112014003740T5 (de) | 2016-05-19 |
CN105408659A (zh) | 2016-03-16 |
CN105408659B (zh) | 2017-10-24 |
JP6189673B2 (ja) | 2017-08-30 |
JP2015036577A (ja) | 2015-02-23 |
US9796255B2 (en) | 2017-10-24 |
US20160176279A1 (en) | 2016-06-23 |
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