JPS59201929A - internal combustion engine intake port - Google Patents
internal combustion engine intake portInfo
- Publication number
- JPS59201929A JPS59201929A JP58075430A JP7543083A JPS59201929A JP S59201929 A JPS59201929 A JP S59201929A JP 58075430 A JP58075430 A JP 58075430A JP 7543083 A JP7543083 A JP 7543083A JP S59201929 A JPS59201929 A JP S59201929A
- Authority
- JP
- Japan
- Prior art keywords
- intake
- valve
- cylinder chamber
- intake port
- combustion engine
- 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.)
- Granted
Links
- 238000002485 combustion reaction Methods 0.000 title claims description 14
- 230000007423 decrease Effects 0.000 claims description 5
- 230000003247 decreasing effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 10
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B31/00—Modifying induction systems for imparting a rotation to the charge in the cylinder
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】
本発明は、シリンダ室の端面にその中・Uから偏芯した
位fffに吸気孔を開口し、吸気孔に吸気弁を設けると
共に吸気通路を接続した内燃機関の吸気ポートに関する
。DETAILED DESCRIPTION OF THE INVENTION The present invention provides an air intake system for an internal combustion engine in which an intake hole is opened in the end face of a cylinder chamber at a position offset from the center U, an intake valve is provided in the intake hole, and an intake passage is connected to the intake hole. Regarding ports.
本発明者は、従前、Cの種の吸気ポートにおいて、適度
の安定した渦流を体積効率を低下させずに生類させる目
的で、吸気通路を、吸気孔に連通して吸気弁を囲む通路
端の渦流生起部とこの通路端以外の導入部から構成し、
吸気弁の弁軸周面とこれに対面した渦流生起部の局面間
の幅を、シリンダ室周面側の外側部分ではシリンダ室中
心側の内側部分エリ広くし、渦流生起部の幅広の外側部
分に導入部を接続し、吸気孔の開口面とCれに対面した
渦流生起部の天井間の高さを、弁軸の回りに幅広の外側
部分から幅狭の内側部分に至る間に同一とし又は減少さ
せ、その平均減少量を弁軸の回りに7度当り吸気孔の径
の07g%以内に設定した内燃機関の吸気ポートを発明
した。The inventor of the present invention has previously proposed that, in an intake port of type C, in order to generate a moderately stable vortex flow without reducing the volumetric efficiency, the intake passage was connected to the intake hole at the end of the passage surrounding the intake valve. Consists of a vortex generating part and an introduction part other than the end of this passage,
The width between the circumferential surface of the valve shaft of the intake valve and the opposite surface of the vortex generating part is made wider at the outer part on the cylinder chamber circumferential side and the inner part on the center side of the cylinder chamber, and the wider outer part of the vortex generating part The height between the opening surface of the intake hole and the ceiling of the vortex generation part facing the C groove is the same from the wide outer part to the narrow inner part around the valve stem. The present invention has invented an intake port for an internal combustion engine in which the average reduction amount is set within 07g% of the diameter of the intake hole per 7 degrees around the valve stem.
本発明の目的は、上記の従前の発明を改良し、スワール
比の高い内燃機関の吸気ポートを提供することである。An object of the present invention is to improve the above-mentioned previous invention and provide an intake port for an internal combustion engine with a high swirl ratio.
本発明は、スワール比を高めるため、シリンダ室の端面
に開口する吸気孔の配置位置についているいろ工夫をし
たものである。In the present invention, in order to increase the swirl ratio, various improvements have been made to the arrangement position of the intake hole opening at the end face of the cylinder chamber.
即ち、第1発明は、上記の従前の発明において、吸気孔
の中Iuとシリンダ室の端面の中心を結ぶ線が複数個の
直列に配置した′シリンダ室の端面の中心を結ぶ線に対
してなす角度を70度以内に設定したことを特徴とする
内燃機関の吸気ポートである。この吸気ポートにおいて
は、後記の実験結果から明らかなように、スワール比の
高い渦流を生起させることができる。That is, in the first invention, in the above-mentioned previous invention, the line connecting the center of the intake hole Iu and the center of the end surface of the cylinder chamber is different from the line connecting the centers of the end surfaces of the cylinder chambers arranged in series. This is an intake port for an internal combustion engine, characterized in that the angle formed is set within 70 degrees. In this intake port, a vortex flow with a high swirl ratio can be generated, as is clear from the experimental results described later.
また、第2発明は、上記の従前の発明において、吸気孔
の中・むとシリンダ室の端面の中心間の距離をシリンダ
室の径の30%以内に設定したことを特徴とする内燃機
関の吸気ポートである。この吸気ホードにおいては、後
記の実験結果から明らかなように、スワール比の高い渦
流を生起させることができる。Further, a second invention is an intake air intake of an internal combustion engine according to the above-mentioned previous invention, characterized in that the distance between the centers of the inner and outer ends of the intake hole and the end face of the cylinder chamber is set to within 30% of the diameter of the cylinder chamber. It is a port. In this intake hoard, it is possible to generate a vortex flow with a high swirl ratio, as is clear from the experimental results described later.
次に、本発明の実施例について説明する。Next, examples of the present invention will be described.
本例の内燃機関の吸気ポートは、第1図と第2図に示す
よりに、シリンダ室αυの円形端面にその中心から周辺
側に偏芯した位置に円形の吸気孔θ峻を開口し、吸気孔
(6)にポペット弁の吸気弁(L3を設けると共に吸気
通路aつを接続し、吸気通路αQを、吸気孔Q匂に連通
して吸気弁Q3を囲む通路端の渦流生起部αQとこの通
路端以外の導入部(11から構成し、渦流生起部QQの
周面を吸気弁の弁軸(14)の周面に対面した2枚の円
筒面を滑らかに接続して形成し、弁軸α→の周面とCれ
に対面した渦流生起部QfjO周面間の幅を、シリンダ
室0υ周面側の外側部分α力ではシリンダ室中・D側の
内側部分α均よシ広くして、弁軸α弔の回りに外側部分
(17)から内側部分(至)に至る間に徐々に狭くし、
渦流生起部OQの幅広の外側部分Oηにその接線方向に
沿って導入部OCJを接続し、吸気孔@の開口面とこれ
に対面した渦流生起部Q・の天井間の高さを、弁軸(1
4)の回りに幅広の外側部分αηから幅狭の内側部分(
至)に至る間に同一とし又は徐々に減少させ、その減少
量を弁軸(14)の回りに7度当り吸気孔の径dの07
g%以内に、具体的には00%%に設定し、第3図に示
すように、吸気孔(2)の中心とシリンダ室0υの端面
の中・Uを結ぶ線が複数個の直列に配置したシリンダ室
の端面の中+L)を結ぶ線に対してなす角度θを70度
以内に、具体的には6度に設定し、また、第2図に示す
ように、吸気孔0りの中心とシリンダ室0υの端面の中
Iu闇の距離rをシリンダ室01)の径りの30%以内
に、具体的には25%に設定している。As shown in FIGS. 1 and 2, the intake port of the internal combustion engine of this example has a circular intake hole θ steeply opened at a position eccentric from the center toward the periphery in the circular end face of the cylinder chamber αυ. An intake valve (L3) of a poppet valve is provided in the intake hole (6) and an intake passage is connected to the intake passage αQ, and the intake passage αQ is connected to the vortex flow generating portion αQ at the end of the passage surrounding the intake valve Q3. The introduction section (11) other than this passage end is formed by smoothly connecting the circumferential surface of the vortex generating section QQ with two cylindrical surfaces facing the circumferential surface of the valve shaft (14) of the intake valve. The width between the circumferential surface of the axis α → and the circumferential surface of the vortex generating part QfjO facing C is made wider evenly in the outer part α on the cylinder chamber 0υ circumferential side than the inner part α in the cylinder chamber and on the D side. Then, it is gradually narrowed around the valve axis α from the outer part (17) to the inner part (to),
The introduction part OCJ is connected to the wide outer part Oη of the vortex generating part Oη along its tangential direction, and the height between the opening surface of the intake hole @ and the ceiling of the vortex generating part Q facing it is determined as the valve axis. (1
4) from the wide outer part αη to the narrow inner part (
(to) or gradually decreases, and the amount of decrease is set to 07 of the intake hole diameter d per 7 degrees around the valve stem (14).
g%, specifically set to 00%%, and as shown in Figure 3, multiple lines connecting the center of the intake hole (2) and the inside/U of the end face of the cylinder chamber 0υ are connected in series. The angle θ formed with the line connecting the center of the end surface of the cylinder chamber + L) is set within 70 degrees, specifically 6 degrees, and as shown in Figure 2, the angle θ of the intake hole 0 The distance r between the center and the end face of the cylinder chamber 0υ is set within 30%, specifically 25%, of the diameter of the cylinder chamber 01).
この吸気ポートにおいては、吸気通路a9を流れる吸気
流は、導入部01から渦流生起部049に流入し、吸気
孔(2)を経てシリンダ室0υに流入し、捷た、吸気流
の主流は、導入部01の軸芯位置から渦流生起部の外側
部分0ηの周面と弁軸α→の局面間の中間位置に流入し
、吸気孔0のを経てシリンダ室0υにその局面の吸気孔
近接部分の接線方向に沿って流入し、シリンダ室(I]
)の周面に沿って旋回する渦流となる。In this intake port, the intake air flow flowing through the intake passage a9 flows from the introduction part 01 into the vortex generation part 049, flows into the cylinder chamber 0υ via the intake hole (2), and the main flow of the interrupted intake air flow is as follows: The flow flows from the axial center position of the introduction part 01 to an intermediate position between the circumferential surface of the outer part 0η of the vortex generating part and the phase of the valve axis α→, passes through the intake hole 0, and enters the cylinder chamber 0υ in the vicinity of the intake hole of that phase. flows along the tangential direction of the cylinder chamber (I)
) becomes a vortex that swirls along the circumferential surface.
本例の吸気ポートにおいて、吸気孔@の中心とシリンダ
室01)の端面の中−〇を結ぶ線が複数個の直列に配置
したシリンダ室(11)の端面の中心分結ぶ線に対して
なす角度θを各位に設定し、その各位についてそれぞれ
シリンダ室(l])に生起する渦流の強さ即ちスワール
比SR,とシリンダ室αυの体積効率VBを求めてみた
ところ、第≠図の線図に示すような実験結果を得た。な
お、同M図においては、上記の配置角度θの符号は、吸
気孔(6)の中Iひが複数個の直列に配置したシリンダ
室0υの端面の中・Uを結ぶ線に対し吸気通路の導入部
Ql 911に位置するときにプラスとし、導入部OI
と反対側に位置するときにマイナスとしている。同線図
の上部から明らかな工9に、スワール比8Rは、配置角
度θが70度を越すと、急激に減少し、75度以内にお
いて非常に高い値となる。体積効率VE は、同線図の
下部から明らかなように、配置角度θの大小によって大
きく変化しない。従って、配置角度θを70度以内に設
定すると、体積効率を低下させずに、スワール比を高く
することができ、配置角度θを75度以内に設定すると
、スワール比を非常に高くすることができる。In the intake port of this example, the line connecting the center of the intake hole @ and the center of the end face of the cylinder chamber 01) is made with respect to the line connecting the center of the end face of a plurality of cylinder chambers (11) arranged in series. When the angle θ was set at various positions and the strength of the vortex generated in the cylinder chamber (l), that is, the swirl ratio SR, and the volumetric efficiency VB of the cylinder chamber αυ were determined for each position, the line diagram shown in Fig. The experimental results shown are obtained. In addition, in the same drawing M, the sign of the above-mentioned arrangement angle θ indicates that the center I of the intake hole (6) is located in the intake passage with respect to the line connecting the center and U of the end faces of the cylinder chambers 0υ arranged in series. It is positive when the introduction part Ql is located at 911, and the introduction part OI
It is considered negative when it is located on the opposite side. As is clear from the upper part of the diagram, the swirl ratio 8R decreases rapidly when the arrangement angle θ exceeds 70 degrees, and reaches a very high value within 75 degrees. As is clear from the lower part of the diagram, the volumetric efficiency VE does not change significantly depending on the magnitude of the arrangement angle θ. Therefore, if the arrangement angle θ is set within 70 degrees, the swirl ratio can be increased without reducing the volumetric efficiency, and if the arrangement angle θ is set within 75 degrees, the swirl ratio can be made very high. can.
また、本例の吸気ポートにおいて、吸気孔@の中JL)
とシリンダ室αυの端面の中心間の距1111rをシリ
ンダ室(1υの径りに対して各位に設定し、その各位r
/1)についてそれぞれスワール比SRと体積効率VE
を求めてみたところ、第5図の線図に示すような実験結
果を得た。同線図の上部から明らかなように、スワール
比SRは、上記の値即ち無次元配置距離r/Dが03を
越すと、急激に減少し、O,/ 3以上で02乙以下に
おいて非常に高い値となる。体積効率VEは、同線図の
下部から明らかなように、無次元配置距離r /D
の大小によって大きく変化しない。従って、無次元配置
距離r/D を30%以内に設定すると、体積効率を
低下させずに、スワール比を高くすることができ、無次
元配置距離r /D を75%以上で26%以下に設
定すると、スワール比を非常に高くすることができる。In addition, in the intake port of this example, the intake hole @ middle JL)
The distance 1111r between the centers of the end faces of the cylinder chamber αυ and the center of the end face of the cylinder chamber αυ is set at each position relative to the diameter of the cylinder chamber (1υ), and each position r
Swirl ratio SR and volumetric efficiency VE for /1), respectively.
When we tried to find this, we obtained experimental results as shown in the diagram in Figure 5. As is clear from the upper part of the diagram, the swirl ratio SR decreases rapidly when the above value, that is, the dimensionless arrangement distance r/D exceeds 03, and becomes extremely It becomes a high value. As is clear from the bottom of the diagram, the volumetric efficiency VE is determined by the dimensionless arrangement distance r/D
It does not change much depending on the size of the Therefore, if the dimensionless arrangement distance r/D is set within 30%, the swirl ratio can be increased without reducing the volumetric efficiency, and the dimensionless arrangement distance r/D can be set to 75% or more and 26% or less. When set, the swirl ratio can be made very high.
【図面の簡単な説明】
第1図は本発明の実施例の吸気ポートの略示斜斜図、第
2図は同吸気ボートの平面図、第3図は同吸気ボートの
配列状態を示す略示平面図であり、第グ図は同吸気ボー
トにおける吸気孔の配置角度とスワール比又は体積効率
の関係を示す線図、第S図は同吸気ボートにおける吸気
孔の配置距離とスワール比又は体積効率の関係を示す線
図である。
11ニジリング室 12:吸気孔13:吸気弁
14:弁 軸15:吸気通路
16:渦流生起部17:外側部分 18:
内側部分19:導入部 θ:吸気孔の配置
角度r :吸気孔の配置距離 Dニジリンダ室の径第
3 図[Brief Description of the Drawings] Fig. 1 is a schematic oblique view of an intake port according to an embodiment of the present invention, Fig. 2 is a plan view of the intake boat, and Fig. 3 is a schematic diagram showing the arrangement of the intake boats. Figure 1 is a diagram showing the relationship between the intake hole arrangement angle and swirl ratio or volumetric efficiency in the same intake boat, and Figure S is a diagram showing the relationship between the intake hole arrangement distance and the swirl ratio or volume in the same intake boat. FIG. 3 is a diagram showing the relationship between efficiency. 11 Nijiring chamber 12: Intake hole 13: Intake valve 14: Valve Shaft 15: Intake passage
16: Eddy current generating part 17: Outside part 18:
Inner part 19: Introduction part θ: Arrangement angle of intake hole r: Arrangement distance of intake hole D Diameter of cylinder chamber Fig. 3
Claims (1)
位置に吸気孔を開口し、吸気孔に吸気弁を設けると共に
吸気通路を接続した内燃機関の吸気ポートにおいて、吸
気通路を、吸気孔に連通して吸気弁を囲む通路端の渦流
生起部とこの通路端以外の導入部から構成し、吸気弁の
弁軸周面とこれに対面した渦流生起部の周面間の幅を、
シリンダ室局面側の外側部分ではシリンダ室中ID側の
内側部分より広くし、渦流生起部の幅広の外側部分に導
入部を接続し、吸気孔の開口面とこれに対面した渦流生
起部の天井間の高さを、弁軸の回シに幅広の外側部分力
・ら幅狭の内側部分に至る間に同一とし又は減少させ、
その平均減少意を弁軸の回りに7度当り吸気孔の径の0
7g%以内に設定し、シリンダ室の端面の中心と吸気孔
の中Iuを結ぶ線が複数個の直列に配置したシリンダ室
の端面の中・Uを結ぶ線に対してなす角度を70度以内
に設定したことを特徴とする内燃機関の吸気ポート。 (2) 前記の角度を”75度以内に設定したことを
特徴とする特許請求の範囲第1項記載の内燃機関の吸気
ポート。 (勺 シリンダ室の端面の中IDと吸気孔の中心間の距
離をシリンダ室の径の30%以内に設定したことを特徴
とする特許請求の範囲第1項又は第2項記載の内燃機関
の吸気ポート。 (4) シリンダ室の端面にその中心から偏芯した位置
に吸気孔を開口し、吸気孔に吸気弁を設けると共に吸気
通路を接続した内燃機関の吸気ポートにおいて、吸気通
路を、吸気孔に連通して吸気弁を囲む通路端の渦流生起
部とこの通路端以外の導入部から構成し、吸気弁の弁軸
周面とこれに対面した渦流生起部の周面間の幅を、シリ
ンダ室周面側の外側部分ではシリンダ室中・U側の内側
部分より広くし、渦流生起部の幅広の外側部分に導入部
を接続し、吸気孔の開口面とこれに対面した渦流生起部
の天井間の高さを、弁軸の回りに幅広の外側部分から幅
狭の内側部分に至る間に同一とし又は減少させ、その平
均減少量を弁軸の回りに7度当り吸気孔の径の07g%
以内に設定し、シリンダ室の端面の中juと吸気孔の中
・U間の距離をシリンダ室の径の30%以内に設定した
Cとを特徴とする内燃機関の吸気ポート。 (5) 前記の距離をシリンダ室の径の75%以上で
26%以下に設定したことを特徴とする特許請求の範囲
第4項記載の内燃機関の吸気ポート。[Scope of Claims] (1) In an intake port of an internal combustion engine in which an intake hole is opened in an end face of a cylinder chamber at a position eccentric from the center IL), an intake valve is provided in the intake hole, and an intake passage is connected to the intake port, The intake passage is composed of a vortex generating part at the end of the passage that communicates with the intake hole and surrounds the intake valve, and an introduction part other than the end of the passage, and includes a circumferential surface of the valve shaft of the intake valve and a circumferential surface of the vortex generating part facing it. The width between
The outer part on the side of the cylinder chamber is made wider than the inner part on the ID side of the cylinder chamber, and the introduction part is connected to the wide outer part of the vortex generating part, and the opening surface of the intake hole and the ceiling of the vortex generating part facing this are made. the height between the valve stem turning from the wide outer part to the narrow inner part, the height being the same or decreasing;
The average decrease is 0 for the diameter of the intake hole per 7 degrees around the valve stem.
Set within 7g%, and set the angle between the line connecting the center of the end surface of the cylinder chamber and Iu inside the intake hole to the line connecting the inside U of the end surface of multiple cylinder chambers arranged in series within 70 degrees. An intake port of an internal combustion engine characterized by being set to . (2) An intake port of an internal combustion engine according to claim 1, characterized in that the angle is set within 75 degrees. The intake port of an internal combustion engine according to claim 1 or 2, characterized in that the distance is set within 30% of the diameter of the cylinder chamber. In an intake port of an internal combustion engine in which an intake port is opened at a position where an intake port is opened, an intake valve is provided in the intake port, and an intake passage is connected, the intake passage is connected to a vortex flow generating portion at the end of the passage that communicates with the intake hole and surrounds the intake valve. The width between the circumferential surface of the valve shaft of the intake valve and the circumferential surface of the vortex generating section facing the intake valve is determined by the width between the circumferential surface of the valve shaft of the intake valve and the circumferential surface of the vortex generating section facing it. The introduction part is connected to the wide outer part of the vortex generating part, and the height between the opening surface of the intake hole and the ceiling of the vortex generating part facing this is made wider than the inner part, and the wide outer part is connected around the valve stem. from the inner part to the narrow inner part, and the average reduction is 07g% of the intake hole diameter per 7 degrees around the valve stem.
An intake port for an internal combustion engine, characterized in that the distance between the middle ju of the end face of the cylinder chamber and the middle U of the intake hole is set within 30% of the diameter of the cylinder chamber. (5) The intake port of an internal combustion engine according to claim 4, wherein the distance is set to be 75% or more and 26% or less of the diameter of the cylinder chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58075430A JPS59201929A (en) | 1983-04-28 | 1983-04-28 | internal combustion engine intake port |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58075430A JPS59201929A (en) | 1983-04-28 | 1983-04-28 | internal combustion engine intake port |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59201929A true JPS59201929A (en) | 1984-11-15 |
| JPH0520564B2 JPH0520564B2 (en) | 1993-03-19 |
Family
ID=13575991
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58075430A Granted JPS59201929A (en) | 1983-04-28 | 1983-04-28 | internal combustion engine intake port |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59201929A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0667414U (en) * | 1993-03-10 | 1994-09-22 | 株式会社椿本チエイン | Article stagnation release structure and article stagnation release system of first-in first-out article storage rack device |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS543515U (en) * | 1977-06-10 | 1979-01-11 |
-
1983
- 1983-04-28 JP JP58075430A patent/JPS59201929A/en active Granted
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS543515U (en) * | 1977-06-10 | 1979-01-11 |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0667414U (en) * | 1993-03-10 | 1994-09-22 | 株式会社椿本チエイン | Article stagnation release structure and article stagnation release system of first-in first-out article storage rack device |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0520564B2 (en) | 1993-03-19 |
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