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JPH0253651B2 - - Google Patents
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JPH0253651B2 - - Google Patents

Info

Publication number
JPH0253651B2
JPH0253651B2 JP59171272A JP17127284A JPH0253651B2 JP H0253651 B2 JPH0253651 B2 JP H0253651B2 JP 59171272 A JP59171272 A JP 59171272A JP 17127284 A JP17127284 A JP 17127284A JP H0253651 B2 JPH0253651 B2 JP H0253651B2
Authority
JP
Japan
Prior art keywords
cylinder
residual
inertia force
deviation
angle
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP59171272A
Other languages
Japanese (ja)
Other versions
JPS6148628A (en
Inventor
Tetsuzo Fujikawa
Makizo Hirata
Shinichi Tanba
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kawasaki Heavy Industries Ltd
Original Assignee
Kawasaki Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kawasaki Heavy Industries Ltd filed Critical Kawasaki Heavy Industries Ltd
Priority to JP17127284A priority Critical patent/JPS6148628A/en
Publication of JPS6148628A publication Critical patent/JPS6148628A/en
Publication of JPH0253651B2 publication Critical patent/JPH0253651B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/22Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/22Compensation of inertia forces
    • F16F15/24Compensation of inertia forces of crankshaft systems by particular disposition of cranks, pistons, or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明はV形内燃機関の改良に係り、特に高次
の残存不平衡慣性力を最小値にするようにしたも
のに関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an improvement of a V-type internal combustion engine, and particularly to one in which higher-order residual unbalanced inertia force is minimized.

(従来技術) 従来からV形内燃機関のクランクピンに所定の
偏角を設けて1次残存不平衡慣性力を0にする所
謂位相クランク(特開昭58−113646号)が開発さ
れている。
(Prior Art) A so-called phase crank (Japanese Unexamined Patent Publication No. 113646/1983) has been developed in which the crank pin of a V-type internal combustion engine is provided with a predetermined deflection angle to reduce the primary residual unbalanced inertia force to zero.

この先行技術では第6図に示すようにクランク
軸のオーバーバランス率δおよびクランクピン相
対角βを β=2α+180゜ δ=0.5 とした時に1次残存不平衡慣性力が0になるが、
高次の残存不平衡慣性力は必ずしも最小値になる
とは限らないという問題がある。
In this prior art, as shown in Fig. 6, the primary residual unbalanced inertia force becomes 0 when the crankshaft overbalance ratio δ and the crank pin relative angle β are β = 2α + 180° δ = 0.5.
There is a problem in that the higher-order residual unbalanced inertial force does not necessarily reach its minimum value.

(発明の目的) 本発明は高次の残存不平衡慣性力をも含んで残
存不平衡慣性力を最小値に近ずけることができる
V形内燃機関を提供することを目的としている。
(Objective of the Invention) An object of the present invention is to provide a V-type internal combustion engine that can bring the residual unbalanced inertia close to a minimum value, even including higher-order residual unbalanced inertia.

(発明の構成) 本発明は往復系質量と回転系質量が共に等しい
一方のシリンダ列と他方のシリンダ列との挟み角
αが60度未満の40度近辺で、1次不平衡慣性力の
みが0の場合に対するクランク軸のオーバーバラ
ンス率の偏差分を△δ、クランクピン相対角βの
偏差率を△β、前記挟み角をαとしたときに β=2α+180゜+△β δ=0.5+△δ(△β>0、△δ>0) と表示されるオーバーバランス率δおよびクラン
クピン相対角βを、△δおよび△βを0を越える
値に調整することによつて1次に高次を含めた残
存不平衡慣性力を最小にしたことを特徴とするV
形内燃機関である。
(Structure of the Invention) The present invention is characterized in that when the included angle α between one cylinder row and the other cylinder row, where both the reciprocating system mass and the rotating system mass are equal, is less than 60 degrees, around 40 degrees, only the first-order unbalanced inertia force is applied. When the deviation of the crankshaft overbalance rate relative to the case of 0 is △δ, the deviation rate of the crank pin relative angle β is △β, and the included angle is α, β = 2α + 180° + △β δ = 0.5 + △ By adjusting the overbalance ratio δ and the crank pin relative angle β expressed as δ (△β>0, △δ>0) to values exceeding 0, the first order higher order V characterized by minimizing the residual unbalanced inertia including
It is an internal combustion engine.

(実施例) 本発明を適用した場合を示す第1図において、
2を前シリンダとし、4を後シリンダとする。r
はクランクアーム長さ、Lはコンロツド長さを
夫々示している。
(Example) In FIG. 1 showing the case where the present invention is applied,
2 is the front cylinder and 4 is the rear cylinder. r
indicates the crank arm length, and L indicates the connecting rod length.

オーバーバランス率δはピストン、ピストンピ
ン等の往復系質量をm、カウンタバランサ6、ク
ランクピン8等の回転系質量をnとしたとき δ=n/m で表示される。なお回転系質量nはクランク軸中
心Oを挟んで対向した位置にあり遠心力が互いに
打消す方向に作用するカウンタバランサ6、クラ
ンクピン8の質量を相殺したものになる。
The overbalance rate δ is expressed as δ=n/m, where m is the mass of the reciprocating system such as the piston and piston pin, and n is the mass of the rotating system such as the counter balancer 6 and the crank pin 8. The rotating system mass n is the mass of the counter balancer 6 and the crank pin 8, which are located at opposing positions with the crankshaft center O in between and whose centrifugal forces act in directions that cancel each other out.

1次不平衝慣性力のみが0となる場合に対す
る、高次のものを含んで残存不平衝慣性力が最小
値となる場合のオーバーバランス率の偏差分を△
δとするとオーバーバランス率δは δ=0.5+△δ ……(1) となる。
The deviation of the overbalance rate when only the first-order unimpinged inertia force is 0 and when the residual unimpeded inertial force including higher-order ones is the minimum value is △
If δ, the overbalance rate δ is δ=0.5+△δ...(1).

同様に前シリンダ2と後シリンダ4との相対角
βは偏差分を△β、シリンダ挟み角をαとする
と、 β=2α+180゜+△β ……(2) となる。
Similarly, the relative angle β between the front cylinder 2 and the rear cylinder 4 is β=2α+180°+Δβ (2) where the deviation is Δβ and the cylinder angle is α.

第1図においてクランク回転角θの時の合成不
平衝慣性力Fは、x方向の不平衝慣性力成分を
Fx、y軸方向の不平衝慣性力成分をFyとすると F=√22 ……(3) で表示される。このときFx、Fyは往復系質量を
m、クランクアーム長さをr、クランク軸角速度
をωとすると Fx=(Fr1+Fr2)cosα−δmrω2
(cosθ+cos(β−θ))……(4) Fy=(Fr1−Fr2)sinα−δmrω2
(sinθ−sin(β−θ))……(5) で表示される。(4)式、(5)式中のFr1、Fr2はコンロ
ツド長さをL、シリンダオフセツト量をεとする
と Fr1=mrω2〔cos(θ−α/2)+λcos2(θ−α/2
)+sin(θ−α/2)・(λsin(θ−α/2)−ξ)
3 +ξsin(θ−α/2)/(1−(λsin(θ−
α/2)−ξ)23/2〕……(6) Fr2=mrω2〔cos(θ+α/2−β)+λcos2(θ+α
/2−β)+sin(θ+α/2−β)・(λsin(θ +α/2−β)+ξ)3−ξsin(θ+α/2−
β)/(1−(λsin(θ+α/2−β)−ξ)23/2
〕……(7) ただし λ=r/L、ξ=ε/L となる。
In Fig. 1, the resultant unimpulsive inertial force F when the crank rotation angle is θ is the unimpulsive inertial force component in the x direction.
If the unimpinged inertial force component in the Fx and y-axis directions is Fy, it is expressed as F=√ 2 + 2 ...(3). At this time, Fx and Fy are reciprocating system mass m, crank arm length r, and crankshaft angular velocity ω, then Fx = (Fr 1 + Fr 2 ) cosα−δmrω 2
(cosθ+cos(β−θ))……(4) Fy=(Fr 1 −Fr 2 )sinα−δmrω 2
(sinθ−sin(β−θ))……(5) Fr 1 and Fr 2 in equations (4) and (5) are Fr 1 = mrω 2 [cos (θ-α/2) + λcos2 (θ-α /2
)+sin(θ−α/2)・(λsin(θ−α/2)−ξ)
3 +ξsin(θ−α/2)/(1−(λsin(θ−
α/2)-ξ) 2 ) 3/2 ]...(6) Fr 2 = mrω 2 [cos(θ+α/2-β)+λcos2(θ+α
/2-β)+sin(θ+α/2-β)・(λsin(θ+α/2-β)+ξ) 3 −ξsin(θ+α/2-
β)/(1-(λsin(θ+α/2-β)-ξ) 2 ) 3/2
]...(7) However, λ=r/L, ξ=ε/L.

このときr=36mm、L=124mm、ε=0として
計算により合成慣性力Fの最大値が最小となる前
記偏差分△β、△δの挟み角αに対する特性を求
めると第2図に示すグラフを得る。したがつて任
意の挟み角αに対して最適な△β、△δを選択し
て残存不平衝慣性力Fを算出すると、α<60゜の
範囲で1次不平衝慣性力のみが0となる場合の残
存不平衝慣性力を100%とした時に、△βおよび
△δの最適値を選択することにより残存不平衝慣
性力Fが減少していることが分かる。
At this time, the characteristics of the deviations △β and △δ with respect to the included angle α at which the maximum value of the resultant inertial force F becomes the minimum are calculated by setting r = 36 mm, L = 124 mm, and ε = 0, and the graph shown in Fig. 2 is obtained. get. Therefore, if the residual unimpingement inertia force F is calculated by selecting the optimal △β and △δ for any included angle α, only the first-order unimpingement inertia force becomes 0 in the range α < 60°. It can be seen that when the residual unimpeded inertia force in this case is taken as 100%, the residual unimpeded inertial force F is reduced by selecting the optimal values of Δβ and Δδ.

次にα=45゜、r=36mm、L=124mm、ε=0と
した時にクランクピン相対角βを変化させて計算
により得たオーバーバランス率δと係数K=
mrω2の関係を第3図に示す。第3図および第2
図から挟み角αが45゜の場合、δ=0.53、β=280゜
とした時に係数Kが最小となることが分る。
Next, when α = 45°, r = 36 mm, L = 124 mm, and ε = 0, the overbalance rate δ and coefficient K = calculated by changing the crank pin relative angle β
The relationship of mrω 2 is shown in Figure 3. Figures 3 and 2
From the figure, it can be seen that when the included angle α is 45°, the coefficient K becomes the minimum when δ=0.53 and β=280°.

(発明の効果) 以上説明したように本発明によれば、1次不平
衝慣性力のみが0となる場合に対するクランク軸
のオーバーバランス率δの偏差分を△δ、クラン
クピン相対角βの偏差分を△βとして、高次の残
存不平衝慣性力Fの最大値が最小となるように△
δ、△βを選択したので、残存不平衝慣性力Fを
減少させることができる。しかもV形エンジンの
構造を変更することを要せず、偏差分△δ、△β
の選択のみで残存不平衝慣性力Fが減少するの
で、極めて実施が容易である。すなわち本発明に
おいては、等式β=2α+180゜とは別の位置に最小
振動が得られる位置、バランス比があるという事
実を見出し、しかもその最大振動がシリンダー相
対角(シリンダー挟み角α)60度未満でしか得ら
れないこと、更にシリンダ相対角40度近辺で最も
その効果が大きいという解析結果に基づき、オー
バーバランス率δの偏差分△δ及びクランクピン
相対角βの偏差分△βを0とは異なる、0を越え
る値に定めることを特徴としており、これにより
1次不平衝慣性力は0とはならないが、1次に高
次を含めた残存不平衝慣性力を最小にすることが
できるのである。
(Effects of the Invention) As explained above, according to the present invention, the deviation of the overbalance rate δ of the crankshaft relative to the case where only the first-order unimpingement inertia force is 0 is calculated as △δ, and the deviation of the crankpin relative angle β is calculated as Δδ. △
Since δ and Δβ are selected, the residual unimpulsive inertial force F can be reduced. Moreover, it is not necessary to change the structure of the V-type engine, and the deviations △δ, △β
Since the residual unimpingement inertia force F is reduced only by selecting , it is extremely easy to implement. In other words, in the present invention, we have discovered that there is a position and balance ratio where the minimum vibration is obtained at a position different from the equation β = 2α + 180°, and that the maximum vibration is at a cylinder relative angle (cylinder included angle α) of 60 degrees. Based on the analysis result that the effect is greatest when the cylinder relative angle is less than 40 degrees, the deviation △δ of the overbalance ratio δ and the deviation △β of the crankpin relative angle β are set to 0. is set to a value that is different and exceeds 0, and as a result, the first-order unimpulsive inertia force does not become zero, but the residual unimpulsive inertia force including the first-order higher order can be minimized. It is.

(別の実施例) (1) 第4図に示すように前シリンダ2、後シリン
ダ4を外方にオフセツト量εだけオフセツト配
置した場合には、第5図に示すようにオフセツ
ト量ε=0の第1図の場合より更に残存不平衝
慣性力Fの最大値の最小値を小さくすることが
できる。
(Another embodiment) (1) When the front cylinder 2 and the rear cylinder 4 are arranged outward by an offset amount ε as shown in FIG. 4, the offset amount ε=0 as shown in FIG. The minimum value of the maximum value of the residual unimpingement inertia force F can be made smaller than the case of FIG.

(2) 本発明は一方のシリンダ列と他方のシリンダ
列の気筒数が等しい偶数気筒V形エンジンに限
らず、両シリンダ列の往復系質量および回転系
質量が互いに等しければ、例えば前シリンダ列
が2気筒、後シリンダ列が1気筒の奇数気筒V
形エンジンにも適用できる。
(2) The present invention is not limited to even-numbered V-type engines in which the number of cylinders in one cylinder row and the other cylinder row are equal; if the reciprocating system mass and the rotating system mass of both cylinder rows are equal to each other, for example, Odd number cylinder V with 2 cylinders and 1 cylinder in the rear cylinder row
It can also be applied to shaped engines.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明を適用したV形2気筒エンジン
の構造略図、第2図は第1図のエンジンにおける
シリンダ挟み角−残存不平衝慣性力、オーバーバ
ランス率の偏差分、クランクピン相対角の偏差分
特性を示すグラフ、第3図はオーバーバランス率
−係数の特性を示すグラフ、第4図は本発明の別
の実施例を示す構造略図、第5図は第4図の場合
のオフセツト量−残存不平衝慣性力Fの最大値の
最小値、オーバーバランス率、クランクピン相対
角特性を示すグラフ、第6図は従来例を示す構造
略図である。2……前シリンダ、4……後シリン
ダ、6……カウンタバランサ、8……クランクピ
ン。
Fig. 1 is a structural diagram of a V-type two-cylinder engine to which the present invention is applied, and Fig. 2 shows the cylinder angle of the engine shown in Fig. 1, the residual unimpingement inertia force, the deviation of the overbalance ratio, and the relative angle of the crankpin. Graph showing the deviation characteristic, FIG. 3 is a graph showing the overbalance rate-coefficient characteristic, FIG. 4 is a structural diagram showing another embodiment of the present invention, and FIG. 5 is the offset amount in the case of FIG. 4. - A graph showing the minimum value of the maximum value of the residual unimpulsive inertia force F, the overbalance ratio, and the crank pin relative angle characteristics. FIG. 6 is a structural diagram showing a conventional example. 2...Front cylinder, 4...Rear cylinder, 6...Counter balancer, 8...Crank pin.

Claims (1)

【特許請求の範囲】 1 往復系質量と回転系質量が共に等しい一方の
シリンダ列と他方のシリンダ列との挟み角αが60
度未満の40度近辺で、1次不平衡慣性力のみが0
の場合に対するクランク軸のオーバーバランス率
の偏差分を△δ、クランクピン相対角βの偏差分
を△β、前記挟み角をαとしたときに β=2α+180゜+△β δ=0.5+△δ(△β>0、△δ>0) と表示されるオーバーバランス率δおよびクラン
クピン相対角βを、△δおよび△βを0を越える
値に調整することによつて1次に高次を含めた残
存不平衡慣性力を最小にしたことを特徴とするV
形内燃機関。
[Claims] 1. The included angle α between one cylinder row and the other cylinder row is 60, in which both the reciprocating system mass and the rotating system mass are equal.
At around 40 degrees, only the first-order unbalanced inertia force is 0.
When the deviation in the overbalance rate of the crankshaft is △δ, the deviation in the crank pin relative angle β is △β, and the included angle is α, then β=2α+180°+△β δ=0.5+△δ (△β>0, △δ>0) The overbalance rate δ and crank pin relative angle β, which are expressed as V characterized by minimizing the included residual unbalanced inertia force
internal combustion engine.
JP17127284A 1984-08-16 1984-08-16 V-type internal-combustion engine Granted JPS6148628A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17127284A JPS6148628A (en) 1984-08-16 1984-08-16 V-type internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17127284A JPS6148628A (en) 1984-08-16 1984-08-16 V-type internal-combustion engine

Publications (2)

Publication Number Publication Date
JPS6148628A JPS6148628A (en) 1986-03-10
JPH0253651B2 true JPH0253651B2 (en) 1990-11-19

Family

ID=15920246

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17127284A Granted JPS6148628A (en) 1984-08-16 1984-08-16 V-type internal-combustion engine

Country Status (1)

Country Link
JP (1) JPS6148628A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3910016B2 (en) * 2001-01-10 2007-04-25 本田技研工業株式会社 Odd-cylinder V-type internal combustion engine
JP2007120429A (en) * 2005-10-28 2007-05-17 Toyota Central Res & Dev Lab Inc Internal combustion engine and compressor

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58113646A (en) * 1981-12-26 1983-07-06 Honda Motor Co Ltd motorcycle

Also Published As

Publication number Publication date
JPS6148628A (en) 1986-03-10

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