WO2011000205A1 - Carburetor with throttle standing-vortex rear fin - Google Patents

Carburetor with throttle standing-vortex rear fin Download PDF

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Publication number
WO2011000205A1
WO2011000205A1 PCT/CN2010/000735 CN2010000735W WO2011000205A1 WO 2011000205 A1 WO2011000205 A1 WO 2011000205A1 CN 2010000735 W CN2010000735 W CN 2010000735W WO 2011000205 A1 WO2011000205 A1 WO 2011000205A1
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WO
WIPO (PCT)
Prior art keywords
throttle
vortex
diaphragm
tail
plunger
Prior art date
Application number
PCT/CN2010/000735
Other languages
French (fr)
Chinese (zh)
Inventor
张龙
Original Assignee
Zhang Long
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 Zhang Long filed Critical Zhang Long
Publication of WO2011000205A1 publication Critical patent/WO2011000205A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/12Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves
    • F02M7/22Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves fuel flow cross-sectional area being controlled dependent on air-throttle-valve position
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M19/00Details, component parts, or accessories of carburettors, not provided for in, or of interest apart from, the apparatus of groups F02M1/00 - F02M17/00
    • F02M19/08Venturis
    • F02M19/088Whirl devices and other atomising means in or on the venturi walls

Definitions

  • the invention belongs to the field of automobile and motorcycle engine parts, and relates to a throttle valve vortex tail carburetor. Background technique
  • the present invention provides a throttle vortex tail carburetor, which reduces the pressure loss caused by the airflow separation through the trapped vortex shedding effect of the throttle vortex tail fin, thereby causing the airflow pressure loss. Smaller into the combustion chamber.
  • a triangular-shaped or dovetail-shaped station is arranged behind the plunger throttle (2) or the diaphragm throttle (6) in the carburetor body assembly (1).
  • the vortex tail (4) is such that the lower bottom surface of the vortex empennage (4) is flush with the bottom surface of the plunger throttle (2) or the diaphragm throttle (6), and the root of the vortex empennage (4) is in close contact with the plunger
  • On the rear wall of the throttle (2) or diaphragm throttle (6) one end of the connecting rod (5) is connected to the upper surface of the trapped empennage (4), and the other end of the connecting hole is inserted into the plunger throttle (2) ) or the rear wall of the diaphragm throttle (6), the oil needle (3) passes through the connecting hole on the connecting rod (5) to connect the trapped vortex tail (4) to the plunger throttle (2) or the diaphragm throttle (6) on the back wall.
  • the airflow when the airflow enters from the air inlet (11) and passes through the throat (12), it does not directly enter the air outlet (13), but flows through the lower bottom surface of the trapped vortex (4), from the vortex tail ( 4)
  • the two edge lines (7) on either side of the triangular piece or the two edge lines (7) in the dovetail shape are peeled off, and then enter the air outlet (13). Since the angle between the direction of the edge line (7) and the flow direction of the airflow is greatly reduced compared with the case of the edge without the 'tail, the airflow flow vortex vortex shedding backswept effect is generated, so the airflow pressure loss is greatly reduced.
  • the fuel is mixed with the airflow from the float chamber (10) in the carburetor body assembly (1), and the vortex formed by the trapped vortex shedding effect of the edge line (7) causes the oil-gas
  • the degree of blending is increased.
  • the reduction in gas flow pressure loss and the increase in oil-gas blending result in an increase in engine power and combustion efficiency, thereby achieving fuel saving.
  • the invention has the beneficial effects of reducing the oil flow pressure loss while increasing the oil-gas blending degree, and using the aerodynamic principle to change only the shape of the gas flow out of the throttle contact bottom edge, and the structure is simple. - BRIEF DESCRIPTION OF THE DRAWINGS
  • Fig. 1 is a longitudinal sectional structural view showing a first embodiment of a throttle trap vortex fin carburetor.
  • Fig. 2 is a cross-sectional structural view of Fig. 1;
  • Figure 3 is a cross-sectional structural view of a second embodiment of a throttle-mounted vortex tail carburetor.
  • Figure 4 is a longitudinal cross-sectional structural view of a third embodiment of a throttle-mounted vortex tail carburetor.
  • Figure 2 is also a cross-sectional structural view of Figure 4 63 ⁇ 4.
  • Fig. 3 is also a cross-sectional structural view of a fourth embodiment of the throttle-mounted vortex tail carburetor.
  • Figure 5 is a longitudinal sectional structural view of a fifth embodiment of a throttle trapped flank carburetor.
  • Figure 7 is a transverse structural view of the underside of the throttle valve of Figure 5.
  • Figure 6 is a longitudinal cross-sectional structural view of a sixth embodiment of a throttle-mounted vortex tail carburetor.
  • Figure 8 is a transverse structural view of the bottom surface of the throttle valve of Figure 6.
  • Figure 9 is a longitudinal cross-sectional structural view of a seventh embodiment of a throttle-mounted vortex tail carburetor.
  • FIG 11 is a transverse structural view of the bottom surface of the throttle valve of Figure 9; '
  • Figure 10 is a longitudinal sectional structural view of an eighth embodiment of a throttle trapped flank carburetor.
  • Figure 12 is a transverse structural view of the bottom surface of the throttle valve of Figure 10;
  • Figure 13 is a cross-sectional structural view of a ninth embodiment of a throttle vortex tail carburetor.
  • Figure 14 is a cross-sectional structural view of a tenth embodiment of a throttle vortex tail carburetor.
  • Figure 15 is a cross-sectional structural view of an eleventh embodiment of a throttle trapped flank carburetor.
  • Figure 16 is a cross-sectional structural view of a twelfth embodiment of a throttle trapped flank carburetor.
  • Figure carburetor body assembly (1), plunger throttle (2), oil needle (3), vortex tail (4), connecting rod (5), diaphragm throttle (6), edge line (7 ), bevel (8), chute (9), float chamber (10), air inlet (11), throat (12), air outlet (13).
  • the trapped vortex fin (4) is a triangular piece disposed behind the plunger throttle (2), the lower bottom surface of the vortex empennage (4) and the plunger throttle (2)
  • the bottom surface of the connecting rod (5) is connected to the upper surface of the trapped vortex fin (4), and the other end has a connecting hole, and one end of the connecting hole is inserted into the rear wall surface of the plunger throttle (2).
  • the oil needle (3) is connected to the rear wall surface of the plunger throttle (2) through a connecting hole in the connecting rod (5). As shown in Fig.
  • the triangular-shaped trapped vortex empennage (4) has a triangular line whose root is close to the rear wall surface of the plunger throttle (2), and the root width is equal to the diameter of the plunger throttle (2).
  • the width of the airway (13) channel, and the other two sides of the triangle form two edge lines (7) which may be straight lines, elliptical lines, arcs or streamline shapes, and triangular plate-shaped trapped vortex fins (4)
  • the lower bottom surface is a curved surface or a flat surface.
  • the trapped vortex tail (4) behind the plunger throttle (2) is a dovetail piece, and the two edge lines (7) formed by the two middle sides are from the middle. Separated to the two sides, respectively intersecting the two edge lines (7) formed by the other two sides extending rearward from both sides of the root.
  • the vortex empennage (4) is a triangular piece disposed behind the diaphragm throttle (6), the lower bottom surface of the vortex tail (4) and the diaphragm section.
  • the bottom surface of the valve (6) is flush, and one end of the connecting rod (5) is connected to the upper surface of the trapped vortex fin (4), and the other end has a connecting hole, Note that one end of the connecting hole is inserted into the rear wall surface of the diaphragm throttle (6), and the oil needle (3) passes through the connecting hole on the connecting rod (5) to connect the standing vortex tail (4) to the diaphragm throttle (6).
  • the connecting hole is inserted into the rear wall surface of the diaphragm throttle (6), and the oil needle (3) passes through the connecting hole on the connecting rod (5) to connect the standing vortex tail (4) to the diaphragm throttle (6).
  • On the back wall As shown in Fig.
  • the triangular sheet-shaped trapped vortex fin (4) has a triangular side with the root of the circular arc line close to the rear wall surface of the diaphragm throttle (6), and the root width is equal to the diameter of the diaphragm throttle (6).
  • the other two sides of the triangle also form two edge lines (7) which can be straight lines, elliptical lines, arcs or streamline shapes.
  • the trapped vortex tail (4) behind the diaphragm throttle (6) is a dovetail piece, and the two edges (7) formed by the middle two sides are from the middle. Separated to the two sides, respectively intersecting the two edge lines (7) formed by the other two sides extending rearward from both sides of the root.
  • the vortex tail fin (4) is integrated with the bottom surface of the plunger throttle (2), and the lower bottom surface of the vortex empennage (4) borrows the plunger throttle (2).
  • the inclined surface (8) is a plane or a curved surface formed by the rear half cylinder of the plunger throttle (2) inclined from the bottom surface to remove the quarter bottom edge, and the rear half cylinder has a slope (8) on each side, two The intersection of the bevel (8) and the bottom surface of the plunger throttle (2) forms the two edge lines (7) of the triangular trapped vortex (4).
  • Figure 7 shows the integrated structure of the vortex empennage (4) and the plunger throttle (2).
  • the first half is the bottom of the plunger throttle (2)
  • the rear half is the bottom of the plunger throttle (2) and the lower bottom of the trapped vortex (4).
  • the vortex tail fin (4) is integrated with the bottom surface of the diaphragm throttle (6), and the diaphragm bottom throttle (4) is borrowed from the lower bottom surface of the vortex empennage (4).
  • the bevel (8) is the plane or curved surface formed by the rear half cylinder of the diaphragm throttle (6) which is inclined upward from the bottom surface to remove the quarter bottom edge.
  • the rear half cylinder has a slope (8) on each side of the cylinder.
  • the intersection of the bevel (8) and the bottom surface of the diaphragm throttle (6) forms the two edge lines (7) of the triangular trapped empennage (4).
  • Figure 8 shows the integrated structure of the vortex tail (4) and the diaphragm throttle (6).
  • the first half is the bottom surface of the diaphragm throttle (6)
  • the rear half is the bottom surface of the diaphragm throttle (6) and the lower bottom surface of the trapped vortex wing (4).
  • the vortex empennage (4) is integrated with the bottom surface of the plunger throttle (2), and the lower bottom surface of the vortex empennage (4) borrows a plunger throttle (2).
  • the chute (9) is a front narrow and wide flank of the plunger throttle (2), and the chute (9) forms two sides on the bottom surface of the plunger throttle (2).
  • the dovetail forms two edge lines (7) in the middle of the vortex tail (4).
  • the integrated structure of the vortex empennage (4) and the plunger throttle (2) as shown in Fig. 11 is shown.
  • the bottom surface is both the bottom surface of the plunger throttle (2) and the lower bottom surface of the trapped vortex fin (4).
  • the vortex empennage (4) is integrated with the bottom surface of the diaphragm throttle (6), and the diaphragm bottom throttle (6) is borrowed from the lower surface of the vortex empennage (4).
  • the chute (9) is a front narrow and wide flank of the diaphragm throttle (6), and the chute (9) forms two sides on the bottom surface of the diaphragm throttle (6).
  • the integrated structure of the trapped vortex fin (4) and the diaphragm throttle (6) as shown in Fig. 12 is shown.
  • the bottom surface is both the bottom surface of the diaphragm throttle (6) and the lower bottom surface of the trapped vortex fin (4).
  • the cylindrical cross section and the bottom surface of the plunger throttle (2) are designed to be elliptical, and the rear half-ellipse of the bottom surface naturally forms a front wide and a narrow design integrated triangular station.
  • the vortex fin (4) and the edge of the rear half-ellipse of the bottom surface form the two edge lines (7) of the trapped vortex fin (4).
  • the cross-section and the bottom surface of the diaphragm throttle (6) are designed to be elliptical, and the rear half-ellipse of the bottom surface naturally forms a front-width, narrow-narrow design integrated triangular trap.
  • the cylindrical cross section and the bottom surface of the plunger throttle (2) are designed to be convex and round, and the rear half convex circle of the bottom surface naturally forms a front wide and a narrow design integrated.
  • the triangular trapped vortex fin (4), the edge of the rear semi-convex circle of the bottom surface constitutes the two edge lines (7) of the trapped vortex fin (4).
  • the cross section and the bottom surface of the diaphragm throttle (6) are designed to be convex and round, and the rear half convex circle of the bottom surface naturally forms a front wide and a narrow design integrated.
  • the triangular trapped vortex fin (4), the edge of the rear semi-convex circle of the bottom surface constitutes the two edge lines (7) of the trapped vortex fin (4).

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Display Devices Of Pinball Game Machines (AREA)

Abstract

A carburetor, attached with one standing-vortex rear fin (4) under or behind the plunger throttle (2) or diaphragm throttle (6) inside the carburetor body component (1). With the standing-vortex shedding and sweepback effect of the throttle standing-vortex rear fin (4) and the by-flowing of air to the low pressure area behind the throttle, the separation loss is reduced and the second rotation of the gas mixture is formed, thus increasing the power and the combustion efficiency of the engine and achieving the purpose of saving fuel.

Description

节气门驻涡尾翼化油器 所属技术领域  Throttle valve vortex tail carburetor
本发明属汽车摩托车发动机部件领域, 涉及一种节气门驻涡尾翼化油器。 背景技术  The invention belongs to the field of automobile and motorcycle engine parts, and relates to a throttle valve vortex tail carburetor. Background technique
目前汽车摩托车发动机化油器有两种形式: 柱塞式化油器和等真空膜片式 化油器。 无论哪种化油器, 其工作原理都是依靠发动机活塞运动产生的真空将 空气从化油器的进气道抽吸, 通过化油器节气门喉道所产生的压差使液态燃油 从化油器浮子室吸出, 经过高速气流冲击雾化形成混合气进入燃烧室燃烧。 但 是, 由于化油器节气门喉道出口通道面积垂直突然扩张产生的气流分离,导致燃 烧室进气压力出现较大损失, 造成发动机功率下降。 因此,降低进气压力损失是 提高发动机功率的重要因素。  At present, there are two forms of automobile and motorcycle engine carburetor: plunger type carburetor and equal vacuum diaphragm type carburetor. Regardless of the carburetor, its working principle relies on the vacuum generated by the movement of the engine piston to draw air from the carburetor inlet, and the pressure difference generated by the carburetor throttle throat makes the liquid fuel from the carburetor. The float chamber is sucked out, and is subjected to high-speed airflow impingement to form a mixed gas to enter the combustion chamber for combustion. However, due to the separation of the airflow caused by the vertical expansion of the outlet passage area of the carburetor throttle throat, the intake pressure of the combustion chamber is greatly lost, resulting in a decrease in engine power. Therefore, reducing intake pressure loss is an important factor in increasing engine power.
发明内容 Summary of the invention
为了降低进气压力损失, 本发明提供了一种节气门驻涡尾翼化油器, 通过节 气门驻涡尾翼的驻涡漩涡脱落后掠效应, 降低气流分离导致的压力损失, 从而 使气流压力损失更小进入燃烧室。  In order to reduce the intake pressure loss, the present invention provides a throttle vortex tail carburetor, which reduces the pressure loss caused by the airflow separation through the trapped vortex shedding effect of the throttle vortex tail fin, thereby causing the airflow pressure loss. Smaller into the combustion chamber.
本发明解决其技术问题所采取的方案是: 在化油器本体组件 (1 ) 中柱塞节 气门 (2) 或者膜片节气门 (6)后面设置一个三角形片状或者燕尾形片状的驻 涡尾翼(4),使驻涡尾翼(4)的下底面与柱塞节气门(2)或者膜片节气门(6) 的底面平齐,驻涡尾翼(4)的根部紧贴在柱塞节气门(2)或者膜片节气门 (6) 的后壁面上, 连结杆 (5) 的一端连接在驻涡尾翼 (4) 的上表面,有连接孔的另 一端插入柱塞节气门 (2 ) 或者膜片节气门 (6) 的后壁面,油针 (3 ) 穿过连结 杆(5)上的连接孔将驻涡尾翼(4)连结在柱塞节气门(2)或者膜片节气门(6) 的后壁面上。 这样,当气流从进气道 (11 )进入, 经过喉道 (12) 后,不再直接 进入出气道(13 ) ,而是流经驻涡尾翼 (4) 的下底面,从驻涡尾翼 (4) 的三角 形片状的两侧两条边缘线 (7)或者燕尾形片状的中间两条边缘线(7)上脱落, 然后再进入出气道 (13)。 由于边缘线 (7) 的走向与气流流动方向的夹角和无 ' 尾翼的边缘情况相比大为减小,产生气流流动驻涡漩涡脱落后掠效应,因此气流 压力损失大为减小。 同时,燃油从化油器本体组件 (1 ) 中的浮子室 (10) 吸入 喉道(12 ) 与气流掺混,由边缘线 (7) 的驻涡漩涡脱落后掠效应形成的涡流使 油-气的掺混程度提高。气流压力损失减小和油-气的掺混程度提高,使得发动机 的功率和燃烧效率提高, 从而达到了节省燃油的目的。  The solution adopted by the present invention to solve the technical problem is: a triangular-shaped or dovetail-shaped station is arranged behind the plunger throttle (2) or the diaphragm throttle (6) in the carburetor body assembly (1). The vortex tail (4) is such that the lower bottom surface of the vortex empennage (4) is flush with the bottom surface of the plunger throttle (2) or the diaphragm throttle (6), and the root of the vortex empennage (4) is in close contact with the plunger On the rear wall of the throttle (2) or diaphragm throttle (6), one end of the connecting rod (5) is connected to the upper surface of the trapped empennage (4), and the other end of the connecting hole is inserted into the plunger throttle (2) ) or the rear wall of the diaphragm throttle (6), the oil needle (3) passes through the connecting hole on the connecting rod (5) to connect the trapped vortex tail (4) to the plunger throttle (2) or the diaphragm throttle (6) on the back wall. Thus, when the airflow enters from the air inlet (11) and passes through the throat (12), it does not directly enter the air outlet (13), but flows through the lower bottom surface of the trapped vortex (4), from the vortex tail ( 4) The two edge lines (7) on either side of the triangular piece or the two edge lines (7) in the dovetail shape are peeled off, and then enter the air outlet (13). Since the angle between the direction of the edge line (7) and the flow direction of the airflow is greatly reduced compared with the case of the edge without the 'tail, the airflow flow vortex vortex shedding backswept effect is generated, so the airflow pressure loss is greatly reduced. At the same time, the fuel is mixed with the airflow from the float chamber (10) in the carburetor body assembly (1), and the vortex formed by the trapped vortex shedding effect of the edge line (7) causes the oil-gas The degree of blending is increased. The reduction in gas flow pressure loss and the increase in oil-gas blending result in an increase in engine power and combustion efficiency, thereby achieving fuel saving.
本发明的有益效果是,降低气流流动压力损失的同时, 提高油 -气的掺混程 度, 利用空气动力学原理仅改变气流流出节气门接触底面边缘的形状,结构简 单。 - 附图说明  The invention has the beneficial effects of reducing the oil flow pressure loss while increasing the oil-gas blending degree, and using the aerodynamic principle to change only the shape of the gas flow out of the throttle contact bottom edge, and the structure is simple. - BRIEF DESCRIPTION OF THE DRAWINGS
下面结合附图和实施例对本发明进一步说明。 说 明 书 图 1是节气门驻涡尾翼化油器第一个实施例的纵剖面构造图。 The invention will now be further described with reference to the drawings and embodiments. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a longitudinal sectional structural view showing a first embodiment of a throttle trap vortex fin carburetor.
图 2是图 1的横剖面构造图。  Fig. 2 is a cross-sectional structural view of Fig. 1;
图 3是节气门驻涡尾翼化油器第二个实施例的横剖面构造图。  Figure 3 is a cross-sectional structural view of a second embodiment of a throttle-mounted vortex tail carburetor.
图 4是节气门驻涡尾翼化油器第三个实施例的纵剖面构造图。  Figure 4 is a longitudinal cross-sectional structural view of a third embodiment of a throttle-mounted vortex tail carburetor.
图 2也是图 4 6¾横剖面构造图。  Figure 2 is also a cross-sectional structural view of Figure 4 63⁄4.
图 3也是节气门驻涡尾翼化油器第四个实施例的横剖面构造图。  Fig. 3 is also a cross-sectional structural view of a fourth embodiment of the throttle-mounted vortex tail carburetor.
图 5是节气门驻涡尾翼化油器第五个实施例的纵剖面构造图。  Figure 5 is a longitudinal sectional structural view of a fifth embodiment of a throttle trapped flank carburetor.
图 7是图 5中节气门底面横向构造图。  Figure 7 is a transverse structural view of the underside of the throttle valve of Figure 5.
图 6是节气门驻涡尾翼化油器第六个实施例的纵剖面构造图。  Figure 6 is a longitudinal cross-sectional structural view of a sixth embodiment of a throttle-mounted vortex tail carburetor.
图 8是图 6中节气门底面横向构造图。  Figure 8 is a transverse structural view of the bottom surface of the throttle valve of Figure 6.
图 9是节气门驻涡尾翼化油器第七个实施例的纵剖面构造图。  Figure 9 is a longitudinal cross-sectional structural view of a seventh embodiment of a throttle-mounted vortex tail carburetor.
图 11是图 9中节气门底面横向构造图。 '  Figure 11 is a transverse structural view of the bottom surface of the throttle valve of Figure 9; '
图 10是节气门驻涡尾翼化油器第八个实施例的纵剖面构造图。  Figure 10 is a longitudinal sectional structural view of an eighth embodiment of a throttle trapped flank carburetor.
图 12是图 10中节气门底面横向构造图。  Figure 12 is a transverse structural view of the bottom surface of the throttle valve of Figure 10;
图 13是节气门驻涡尾翼化油器第九个实施例的横剖面构造图。  Figure 13 is a cross-sectional structural view of a ninth embodiment of a throttle vortex tail carburetor.
图 14是节气门驻涡尾翼化油器第十个实施例的横剖面构造图。  Figure 14 is a cross-sectional structural view of a tenth embodiment of a throttle vortex tail carburetor.
图 15是节气门驻涡尾翼化油器第十一个实施例的横剖面构造图。  Figure 15 is a cross-sectional structural view of an eleventh embodiment of a throttle trapped flank carburetor.
图 16是节气门驻涡尾翼化油器第十二个实施例的横剖面构造图。  Figure 16 is a cross-sectional structural view of a twelfth embodiment of a throttle trapped flank carburetor.
图中化油器本体组件 (1 ),柱塞节气门 (2) , 油针 (3) , 驻涡尾翼 (4), 连结杆(5) ,膜片节气门 (6) , 边缘线 (7) ,斜面 (8) ,斜槽(9) , 浮子室 ( 10), 进气道 (11 ) , 喉道(12), 出气道 (13)。  Figure carburetor body assembly (1), plunger throttle (2), oil needle (3), vortex tail (4), connecting rod (5), diaphragm throttle (6), edge line (7 ), bevel (8), chute (9), float chamber (10), air inlet (11), throat (12), air outlet (13).
具体实施方式 Detailed ways
在图 1所示的第一个实施例中, 驻涡尾翼 (4) 是一个三角形片, 设置在柱 塞节气门 (2) 的后面, 驻涡尾翼(4)的下底面与柱塞节气门 (2) 的底面平齐, 连结杆(5) 的一端连接在驻涡尾翼 (4) 的上表面, 另一端有连接孔, 有连接 孔的一端插入柱塞节气门 (2) 的后壁面, 油针 (3) 穿过连结杆(5)上的连接 孔将驻涡尾翼 (4)连结在柱塞节气门 (2) 的后壁面上。 如图 2所示的三角形 片状驻涡尾翼(4),其三角形一边为圆弧线的根部紧贴柱塞节气门 (2) 的后壁 面, 根部宽度等于柱塞节气门 (2) 的直径或者是出气道 (13)通道的宽度, 三 角形另外两条边构成可以是直线、 椭圆线、 弧线或者是流线形状的两条边缘线 (7), 三角形片状驻涡尾翼 (4) 的下底面为弧形面或者是平面。  In the first embodiment shown in Fig. 1, the trapped vortex fin (4) is a triangular piece disposed behind the plunger throttle (2), the lower bottom surface of the vortex empennage (4) and the plunger throttle (2) The bottom surface of the connecting rod (5) is connected to the upper surface of the trapped vortex fin (4), and the other end has a connecting hole, and one end of the connecting hole is inserted into the rear wall surface of the plunger throttle (2). The oil needle (3) is connected to the rear wall surface of the plunger throttle (2) through a connecting hole in the connecting rod (5). As shown in Fig. 2, the triangular-shaped trapped vortex empennage (4) has a triangular line whose root is close to the rear wall surface of the plunger throttle (2), and the root width is equal to the diameter of the plunger throttle (2). Or the width of the airway (13) channel, and the other two sides of the triangle form two edge lines (7) which may be straight lines, elliptical lines, arcs or streamline shapes, and triangular plate-shaped trapped vortex fins (4) The lower bottom surface is a curved surface or a flat surface.
在图 3所示的第二个实施例中, 柱塞节气门 (2)后面的驻涡尾翼(4) 是一 个燕尾形片, 中间两条边所构成的两条边缘线 (7 ) 从中间向两侧分开,分别与 从根部两侧向后延伸的另外两条边构成的两条边缘线 (7)相交。  In the second embodiment shown in Fig. 3, the trapped vortex tail (4) behind the plunger throttle (2) is a dovetail piece, and the two edge lines (7) formed by the two middle sides are from the middle. Separated to the two sides, respectively intersecting the two edge lines (7) formed by the other two sides extending rearward from both sides of the root.
在图 4所示的第三个实施例中, 驻涡尾翼 (4) 同是一个三角形片, 设置在 膜片节气门 (6) 的后面, 驻涡尾翼 (4) 的下底面与膜片节气门 (6) 的底面平 齐, 连结杆(5) 的一端连接在驻涡尾翼 (4) 的上表面, 另一端有连接孔, 有 说 明 连接孔的一端插入膜片节气门 (6) 的后壁面, 油针 (3) 穿过连结杆 (5) 上的连接孔将驻涡尾翼 (4)连结在膜片节气门 (6) 的后壁面上。 如图 2所示 的三角形片状驻涡尾翼 (4),其三角形一边为圆弧线的根部紧贴膜片节气门(6) 的后壁面, 根部宽度等于膜片节气门 (6) 的直径或者是出气道(13)通道的宽 度, 三角形另外两条边同样构成可以是直线、 椭圆线、 弧线或者是流线形状的 两条边缘线 (7)。 In the third embodiment shown in Fig. 4, the vortex empennage (4) is a triangular piece disposed behind the diaphragm throttle (6), the lower bottom surface of the vortex tail (4) and the diaphragm section. The bottom surface of the valve (6) is flush, and one end of the connecting rod (5) is connected to the upper surface of the trapped vortex fin (4), and the other end has a connecting hole, Note that one end of the connecting hole is inserted into the rear wall surface of the diaphragm throttle (6), and the oil needle (3) passes through the connecting hole on the connecting rod (5) to connect the standing vortex tail (4) to the diaphragm throttle (6). On the back wall. As shown in Fig. 2, the triangular sheet-shaped trapped vortex fin (4) has a triangular side with the root of the circular arc line close to the rear wall surface of the diaphragm throttle (6), and the root width is equal to the diameter of the diaphragm throttle (6). Or the width of the airway (13) channel, the other two sides of the triangle also form two edge lines (7) which can be straight lines, elliptical lines, arcs or streamline shapes.
在图 3所示的第四个实施例中, 膜片节气门 (6)后面的驻涡尾翼 (4) 同是 一个燕尾形片, 中间两条边所构成的两条边缘 ( 7 ) 从中间向两侧分开,分别 与从根部两侧向后延伸的另外两条边构成的两条边缘线 (7)相交。  In the fourth embodiment shown in Fig. 3, the trapped vortex tail (4) behind the diaphragm throttle (6) is a dovetail piece, and the two edges (7) formed by the middle two sides are from the middle. Separated to the two sides, respectively intersecting the two edge lines (7) formed by the other two sides extending rearward from both sides of the root.
在图 5所示的第五个实施例中, 驻涡尾翼 (4) 与柱塞节气门 (2)底面设计 一体化,驻涡尾翼(4)的下底面借用了柱塞节气门(2)的后半圆底面。斜面(8) 是柱塞节气门 (2)的后半圆柱体从底面倾斜向上去掉四分之一底面边缘所形成 的平面或者曲面,后半圆柱体两侧各有一个斜面 (8) ,两个斜面 (8) 与柱塞节 气门 (2) 的底面的交线构成了三角形驻涡尾翼(4) 的两条边缘线(7)。 如图 7 所示的驻涡尾翼 (4) 与柱塞节气门 (2 )底面一体化构造图。 其前半部分是柱 塞节气门 (2) 的底面,后半部分既是柱塞节气门 (2 ) 的底面,同时又是驻涡尾 翼(4) 的下底面。  In the fifth embodiment shown in FIG. 5, the vortex tail fin (4) is integrated with the bottom surface of the plunger throttle (2), and the lower bottom surface of the vortex empennage (4) borrows the plunger throttle (2). The bottom half of the back. The inclined surface (8) is a plane or a curved surface formed by the rear half cylinder of the plunger throttle (2) inclined from the bottom surface to remove the quarter bottom edge, and the rear half cylinder has a slope (8) on each side, two The intersection of the bevel (8) and the bottom surface of the plunger throttle (2) forms the two edge lines (7) of the triangular trapped vortex (4). Figure 7 shows the integrated structure of the vortex empennage (4) and the plunger throttle (2). The first half is the bottom of the plunger throttle (2), and the rear half is the bottom of the plunger throttle (2) and the lower bottom of the trapped vortex (4).
在图 6所示的第六个实施例中, 驻涡尾翼 (4) 与膜片节气门 (6)底面设计 一体化,驻涡尾翼(4)的下底面借用了膜片节气门(6)的后半圆底面。斜面(8) 是膜片节气门 (6) 的后半圆柱体从底面倾斜向上去掉四分之一底面边缘所形成 的平面或者曲面,后半圆柱体两侧各有一个斜面(8) ,两个斜面(8) 与膜片节 气门 (6) 的底面的交线构成了三角形驻涡尾翼(4) 的两条边缘线(7)。 如图 8 所示的驻涡尾翼 (4) 与膜片节气门 (6 )底面一体化构造图。 其前半部分是膜 片节气门 (6 ) 的底面,后半部分既是膜片节气门 (6) 的底面,同时又是驻涡尾 翼(4) 的下底面。  In the sixth embodiment shown in Fig. 6, the vortex tail fin (4) is integrated with the bottom surface of the diaphragm throttle (6), and the diaphragm bottom throttle (4) is borrowed from the lower bottom surface of the vortex empennage (4). The bottom half of the back. The bevel (8) is the plane or curved surface formed by the rear half cylinder of the diaphragm throttle (6) which is inclined upward from the bottom surface to remove the quarter bottom edge. The rear half cylinder has a slope (8) on each side of the cylinder. The intersection of the bevel (8) and the bottom surface of the diaphragm throttle (6) forms the two edge lines (7) of the triangular trapped empennage (4). Figure 8 shows the integrated structure of the vortex tail (4) and the diaphragm throttle (6). The first half is the bottom surface of the diaphragm throttle (6), and the rear half is the bottom surface of the diaphragm throttle (6) and the lower bottom surface of the trapped vortex wing (4).
在图 9所示的第七个实施例中, 驻涡尾翼 (4) 与柱塞节气门 (2)底面设计 一体化, 驻涡尾翼 (4) 的下底面借用了柱塞节气门 (2) 的底面。 斜槽 (9)是 柱塞节气门 (2 ) 的底面开的一个前窄后宽的喇叭形斜槽, 斜槽 (9) 在柱塞节 气门(2)的底面上的两条边构成了燕尾形驻涡尾翼(4)中间的两条边缘线(7)。 如图 11所示的驻涡尾翼 (4)与柱塞节气门 (2)底面一体化构造图。 该底面既 是柱塞节气门 (2) 的底面,同时又是驻涡尾翼 (4) 的下底面。  In the seventh embodiment shown in Fig. 9, the vortex empennage (4) is integrated with the bottom surface of the plunger throttle (2), and the lower bottom surface of the vortex empennage (4) borrows a plunger throttle (2). The bottom surface. The chute (9) is a front narrow and wide flank of the plunger throttle (2), and the chute (9) forms two sides on the bottom surface of the plunger throttle (2). The dovetail forms two edge lines (7) in the middle of the vortex tail (4). The integrated structure of the vortex empennage (4) and the plunger throttle (2) as shown in Fig. 11 is shown. The bottom surface is both the bottom surface of the plunger throttle (2) and the lower bottom surface of the trapped vortex fin (4).
在图 10所示的第八个实施例中, 驻涡尾翼 (4) 与膜片节气门 (6)底面设 计一体化, 驻涡尾翼 (4) 的下底面借用了膜片节气门 (6) 的底面。 斜槽(9) 是膜片节气门 (6) 的底面开的一个前窄后宽的喇叭形斜槽, 斜槽 (9) 在膜片 节气门 (6 ) 的底面上的两条边构成了燕尾形驻涡尾翼 (4) 中间的两条边缘线 (7)。 如图 12所示的驻涡尾翼 (4)与膜片节气门 (6)底面一体化构造图。 该 底面既是膜片节气门 (6) 的底面,同时又是驻涡尾翼 (4) 的下底面。 说 明 在图 13所示的第九个实施例中, 柱塞节气门 (2) 的柱体横截面及底面设计 成椭圆形,其底面后半椭圆自然形成前宽后窄设计一体化的三角形驻涡尾翼(4) , 底面后半椭圆的边线构成了驻涡尾翼(4) 的两条边缘线 (7)。 In the eighth embodiment shown in Fig. 10, the vortex empennage (4) is integrated with the bottom surface of the diaphragm throttle (6), and the diaphragm bottom throttle (6) is borrowed from the lower surface of the vortex empennage (4). The bottom surface. The chute (9) is a front narrow and wide flank of the diaphragm throttle (6), and the chute (9) forms two sides on the bottom surface of the diaphragm throttle (6). Two edge lines (7) in the middle of the dovetail shaped vortex tail (4). The integrated structure of the trapped vortex fin (4) and the diaphragm throttle (6) as shown in Fig. 12 is shown. The bottom surface is both the bottom surface of the diaphragm throttle (6) and the lower bottom surface of the trapped vortex fin (4). In the ninth embodiment shown in FIG. 13, the cylindrical cross section and the bottom surface of the plunger throttle (2) are designed to be elliptical, and the rear half-ellipse of the bottom surface naturally forms a front wide and a narrow design integrated triangular station. The vortex fin (4) and the edge of the rear half-ellipse of the bottom surface form the two edge lines (7) of the trapped vortex fin (4).
在图 14所示的第十个实施例中, 膜片节气门 (6 ) 的柱体横截面及底面设计 成椭圆形,其底面后半椭圆自然形成前宽后窄设计一体化的三角形驻涡尾翼(4), 底面后半椭圆的边线构成了驻涡尾翼(4) 的两条边缘线 (7)。  In the tenth embodiment shown in FIG. 14, the cross-section and the bottom surface of the diaphragm throttle (6) are designed to be elliptical, and the rear half-ellipse of the bottom surface naturally forms a front-width, narrow-narrow design integrated triangular trap. The empennage (4), the edge of the rear half-ellipse of the bottom surface, forms the two edge lines (7) of the trapped vortex fin (4).
在图 15所示的第十一个实施例中, 柱塞节气门 (2) 的柱体横截面及底面设 计成凸圆形,其底面后半凸圆自然形成前宽后窄设计一体化的三角形驻涡尾翼 (4), 底面后半凸圆的边线构成了驻涡尾翼 (4) 的两条边缘线 (7)。  In the eleventh embodiment shown in FIG. 15, the cylindrical cross section and the bottom surface of the plunger throttle (2) are designed to be convex and round, and the rear half convex circle of the bottom surface naturally forms a front wide and a narrow design integrated. The triangular trapped vortex fin (4), the edge of the rear semi-convex circle of the bottom surface constitutes the two edge lines (7) of the trapped vortex fin (4).
在图 16所示的第十二个实施例中, 膜片节气门 (6) 的柱体横截面及底面设 计成凸圆形,其底面后半凸圆自然形成前宽后窄设计一体化的三角形驻涡尾翼 (4), 底面后半凸圆的边线构成了驻涡尾翼 (4) 的两条边缘线 (7)。  In the twelfth embodiment shown in FIG. 16, the cross section and the bottom surface of the diaphragm throttle (6) are designed to be convex and round, and the rear half convex circle of the bottom surface naturally forms a front wide and a narrow design integrated. The triangular trapped vortex fin (4), the edge of the rear semi-convex circle of the bottom surface constitutes the two edge lines (7) of the trapped vortex fin (4).

Claims

权 利 要 求 书 Claims
.1. 一种节气门驻涡尾翼化油器, 其特征是: 在化油器本体组件(1 )中柱 塞节气门 (2) 或者膜片节气门 (6)后面是一个三角形片状的驻涡尾 翼 (4) , 驻涡尾翼 (4) 的下底面与节气门的底面平齐, 连结杆(5) 的一端连接在驻涡尾翼 (4) 的上表面,有连接孔的另一端插入节气门 的后壁面,油针 (3) 穿过连结杆 (5) 上的连接孔将驻涡尾翼 (4) 连 结在节气门的后壁面上,三角形驻涡尾翼(4) 的根部一边紧贴在节气 门的后壁面,根部宽度等于节气门的直径或者是出气道(13)通道的宽 度, 另外两条边构成可以是直线、 椭圆线、 弧线或者是流线形状的两 条边缘线 (7) ,驻涡尾翼 (4) 的下底面为弧形面或者是平面。 .1. A throttle-mounted vortex tail carburetor, characterized in that: in the carburetor body assembly (1), the plunger throttle (2) or the diaphragm throttle (6) is followed by a triangular sheet The lower end of the trapped vortex tail (4) is flush with the bottom surface of the throttle vortex (4), and one end of the connecting rod (5) is connected to the upper surface of the vortex empennage (4), and the other end of the connecting hole is inserted. On the rear wall of the throttle, the oil needle (3) passes through the connecting hole on the connecting rod (5) to connect the standing vortex tail (4) to the rear wall surface of the throttle, and the root of the triangular trapped vortex (4) is closely attached to one side. On the rear wall of the throttle, the root width is equal to the diameter of the throttle or the width of the passage of the air outlet (13), and the other two sides form two edge lines which may be straight lines, elliptical lines, arcs or streamlined shapes ( 7) The lower bottom surface of the trapped vortex fin (4) is a curved surface or a flat surface.
2. 根据权利要求 1所述的节气门驻涡尾翼化油器, 其特征是: 在化油器 本体组件(1 ) 中柱塞节气门 (2)或者膜片节气门 (6)后面是一个燕 尾形片状的驻涡尾翼 (4) , 燕尾形驻涡尾翼 (4) 中间两条边所构成 的两条边缘线 (7)从中间向两侧分开,分别与从根部两侧向后延伸的 另外两条边构成的两条边缘线 (7)相交。  2. The throttle vortex tail carburetor according to claim 1, wherein: in the carburetor body assembly (1), behind the plunger throttle (2) or the diaphragm throttle (6) is a The dovetail-shaped vortex empennage (4), the dovetail-shaped vortex empennage (4) The two edge lines (7) formed by the two middle sides are separated from the middle to the sides, respectively, and extend backward from both sides of the root The two edge lines (7) formed by the other two sides intersect.
3. 根据权利要求 1所述的节气门驻涡尾翼化油器, 其特征是: 斜面(8) 是柱塞节气门 (2)或者膜片节气门 (6) 的后半圆柱体从底面倾斜向 上去掉四分之一底面边缘所形成的平面或者曲面,后半圆柱体两侧各 有一个斜面(8),两个斜面(8) 与柱塞节气门 (2) 或者膜片节气门 3. The throttle valve vortex tail carburetor according to claim 1, wherein: the slope (8) is a plunger throttle (2) or the rear half cylinder of the diaphragm throttle (6) is inclined from the bottom surface Remove the plane or curved surface formed by the edge of the bottom of the quarter. The rear half of the cylinder has a slope (8), two slopes (8) and the plunger throttle (2) or the diaphragm throttle.
(6) 的底面的交线构成了三角形驻涡尾翼 (4) 的两条边缘线 (7)。The intersection line of the bottom surface of (6) constitutes the two edge lines (7) of the triangular trapped vortex fin (4).
4. 根据权利要求 1所述的令气门驻涡尾翼化油器, 其特征是: 斜槽(9) 是柱塞节气门 (2)或者膜片节气门 ('6) 的底面开的一个前窄后宽的 喇叭形斜槽,斜槽(9)在柱塞节气门 (2)或者膜片节气门 (6) 的底 面上的两条边构成了燕尾形驻涡尾翼(4) 中间的两条边缘线 (7)。4. The valve vortex tail carburetor according to claim 1, wherein: the chute (9) is a front side of the plunger throttle (2) or the diaphragm throttle ('6). a narrow rear wide horn chute, the two sides of the chute (9) on the bottom surface of the plunger throttle (2) or the diaphragm throttle (6) form the two in the middle of the dovetail shaped vortex tail (4) Edge line (7).
5. 根据权利要求 1所述的节气门驻涡尾翼化油器, 其特征是: 柱塞节气 门(2)或者膜片节气门(6)的柱体横截面及底面设计成椭圆形,其底 面后半椭圆自然形成前宽后窄设计一体化的三角形驻涡尾翼(4),底 面后半椭圆的边线构成了驻涡尾翼 (4) 的两条边缘线 (7)。 5. The throttle vortex tail carburetor according to claim 1, wherein: a cylindrical throttle cross section and a bottom surface of the plunger throttle (2) or the diaphragm throttle (6) are elliptical, The rear half-ellipse of the bottom surface naturally forms a triangular-shaped vortex empennage (4) with a front wide and a narrow design integrated, and the edge of the rear half-ellipse of the bottom surface constitutes two edge lines (7) of the vortex empennage (4).
6. 根据权利要求 1所述的节气门驻涡尾翼化油器, 其特征是: 柱塞节气 . , 门(2)或者膜片节气门(6)的柱体横截面及底面设计成凸圆形,其底 面后半凸圆自然形成前宽后窄设计一体化的三角形驻涡尾翼(4) ,底 面后半凸圆的边线构成了驻涡尾翼 (4) 的两条边缘线 (7)。  6. The throttle valve vortex tail carburetor according to claim 1, wherein: the piston throttle, the door (2) or the diaphragm throttle (6) have a cylindrical cross section and a bottom surface designed to be convex The shape of the bottom half of the bottom surface naturally forms a front wide and narrow design integrated triangular trapped vortex tail (4), and the edge of the rear half of the bottom convex circle constitutes the two edge lines (7) of the trapped vortex tail (4).
PCT/CN2010/000735 2009-06-28 2010-05-24 Carburetor with throttle standing-vortex rear fin WO2011000205A1 (en)

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CN2470547Y (en) * 2001-02-28 2002-01-09 上海市浦东管道件厂 Secondary-atomizing micro-regulating plunger type throtting valve type carburator
CN2888108Y (en) * 2006-01-04 2007-04-11 江门天钇金属工业有限公司 Air intake device of carburetor
CN2898334Y (en) * 2005-12-28 2007-05-09 江门天钇金属工业有限公司 Plunger-valve adjuster for carburator

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JPH11351061A (en) * 1998-06-04 1999-12-21 Nippon Walbro:Kk Carburetor of constant-vacuum sliding throttle valve type
CN2470547Y (en) * 2001-02-28 2002-01-09 上海市浦东管道件厂 Secondary-atomizing micro-regulating plunger type throtting valve type carburator
CN2898334Y (en) * 2005-12-28 2007-05-09 江门天钇金属工业有限公司 Plunger-valve adjuster for carburator
CN2888108Y (en) * 2006-01-04 2007-04-11 江门天钇金属工业有限公司 Air intake device of carburetor

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