CN111299956A - An engine maintenance method - Google Patents
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- CN111299956A CN111299956A CN201911241090.2A CN201911241090A CN111299956A CN 111299956 A CN111299956 A CN 111299956A CN 201911241090 A CN201911241090 A CN 201911241090A CN 111299956 A CN111299956 A CN 111299956A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B3/00—Cleaning by methods involving the use or presence of liquid or steam
- B08B3/02—Cleaning by the force of jets or sprays
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
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Abstract
本发明公开了一种发动机保养方法,具体按照以下步骤实施:步骤1、利用高压水对发动机进行冲洗,去除发动机周围的杂质;步骤2、将发动机内参残余的油放出;步骤3、第一次镗孔,通过机械加工统一发动机缸孔尺寸;步骤4、喷涂,将涂层涂覆至发动机缸孔内;步骤5、铣顶面,对发动机空空顶部进行表面清理;步骤6、第二次镗孔,通过机械加工修正发动机缸孔的圆柱度;步骤7、珩磨,恢复发动机缸孔的尺寸和粗糙度。本发明一种发动机保养方法,对发动机清洗的同时进行了局部易损部位的修复。The invention discloses an engine maintenance method, which is specifically implemented according to the following steps: step 1, use high-pressure water to flush the engine to remove impurities around the engine; step 2, release the residual oil of the engine internal reference; step 3, the first Boring, unifying the size of the engine cylinder hole by machining; Step 4, spraying, applying the coating to the engine cylinder hole; Step 5, milling the top surface, cleaning the surface of the empty top of the engine; Step 6, the second boring The cylindricity of the engine cylinder hole is corrected by machining; Step 7, honing, to restore the size and roughness of the engine cylinder hole. The invention provides an engine maintenance method, which repairs local vulnerable parts while cleaning the engine.
Description
技术领域technical field
本发明属于发动机保养技术领域,具体涉及一种发动机保养方法。The invention belongs to the technical field of engine maintenance, and particularly relates to an engine maintenance method.
背景技术Background technique
发动机是一种能够把其它形式的能转化为机械能的机器,包括如内燃机(往复活塞式发动机)、外燃机(斯特林发动机、蒸汽机等)、喷气发动机、电动机等。如内燃机通常是把化学能转化为机械能。发动机既适用于动力发生装置,也可指包括动力装置的整个机器(如:汽油发动机、航空发动机)。发动机最早诞生在英国,所以,发动机的概念也源于英语,它的本义是指那种“产生动力的机械装置”。An engine is a machine that can convert other forms of energy into mechanical energy, including internal combustion engines (reciprocating piston engines), external combustion engines (Stirling engines, steam engines, etc.), jet engines, electric motors, and the like. For example, internal combustion engines usually convert chemical energy into mechanical energy. The engine applies to both the power generating device and the entire machine including the power device (eg gasoline engine, aero engine). The engine was first born in the United Kingdom, so the concept of the engine is also derived from English, and its original meaning refers to the kind of "mechanical device that generates power".
外燃机,就是说它的燃料在发动机的外部燃烧,1816年由苏格兰的R.斯特林所发明,故又称斯特林发动机。发动机将这种燃烧产生的热能转化成动能,瓦特改良的蒸汽机就是一种典型的外燃机,当大量的煤燃烧产生热能把水加热成大量的水蒸汽时,高压便产生了,然后这种高压又推动机械做功,从而完成了热能向动能的转变。The external combustion engine, which means that its fuel is burned outside the engine, was invented by R. Stirling of Scotland in 1816, so it is also called the Stirling engine. The engine converts the heat energy generated by this combustion into kinetic energy. Watt's improved steam engine is a typical external combustion engine. When a large amount of coal is burned to generate heat energy to heat water into a large amount of water vapor, high pressure is generated, and then this kind of The high pressure pushes the machine to do work, thus completing the conversion of thermal energy to kinetic energy.
内燃机即往复活塞式发动机,这一类型的发动机与外燃机的最大不同在于它的燃料在其内部燃烧。内燃机的种类十分繁多,常见的汽油机、柴油机是典型的内燃机。The internal combustion engine is a reciprocating piston engine. The biggest difference between this type of engine and an external combustion engine is that its fuel is burned inside it. There are many types of internal combustion engines. Common gasoline engines and diesel engines are typical internal combustion engines.
燃气轮机,这种发动机的工作特点是燃烧产生高压燃气,利用燃气的高压推动燃气轮机的叶片旋转,从而输出动力。燃气轮机使用范围很广,但由于很难精细地调节输出的功率,所以汽车和摩托车很少使用燃气轮机,只有部分赛车装用过燃气轮机。Gas turbine, the working characteristic of this engine is to generate high-pressure gas by combustion, and use the high pressure of the gas to drive the blades of the gas turbine to rotate, thereby outputting power. Gas turbines are widely used, but because it is difficult to finely adjust the output power, gas turbines are rarely used in cars and motorcycles, and only some racing cars have used gas turbines.
喷气发动机,是指靠喷管高速喷出的气流直接产生反作用推力的发动机。广泛用作飞行器的动力装置。燃料和氧化剂在燃烧室内起化学反应而释放热能.然后热能在喷管中转化为调整气流的功能。除燃料外,氧化剂由飞行器携带的称为火箭发动机,包括固体燃料火箭发动机和液体燃料火箭发动机。A jet engine refers to an engine that directly generates reaction thrust by the airflow ejected at high speed from the nozzle. Widely used as a power plant for aircraft. The fuel and oxidant react chemically in the combustion chamber to release heat energy. Then the heat energy is converted into the function of adjusting the airflow in the nozzle. In addition to fuel, the oxidizer carried by the aircraft is called a rocket motor, including solid-fuel rocket motors and liquid-fuel rocket motors.
发明内容SUMMARY OF THE INVENTION
本发明的目的是提供一种发动机保养方法,对发动机清洗的同时进行了局部易损部位的修复。The purpose of the present invention is to provide an engine maintenance method, which repairs local vulnerable parts while cleaning the engine.
本发明所采用的技术方案是,一种发动机保养方法,具体按照以下步骤实施:The technical solution adopted in the present invention is, an engine maintenance method, which is specifically implemented according to the following steps:
步骤1、利用高压水对发动机进行冲洗,去除发动机周围的杂质;Step 1. Rinse the engine with high-pressure water to remove impurities around the engine;
步骤2、将发动机内参残余的油放出;Step 2. Drain the residual oil from the engine internal reference;
步骤3、第一次镗孔,通过机械加工统一发动机缸孔尺寸;Step 3. Boring for the first time, unify the cylinder hole size of the engine through machining;
步骤4、喷涂,将涂层涂覆至发动机缸孔内;Step 4, spray, and apply the coating to the cylinder bore of the engine;
步骤5、铣顶面,对发动机空空顶部进行表面清理;Step 5. Mill the top surface and clean the surface of the empty top of the engine;
步骤6、第二次镗孔,通过机械加工修正发动机缸孔的圆柱度;Step 6. Boring for the second time, correct the cylindricity of the engine cylinder hole by machining;
步骤7、珩磨,恢复发动机缸孔的尺寸和粗糙度。Step 7. Honing to restore the size and roughness of the engine cylinder bore.
本发明的特点还在于:The feature of the present invention also lies in:
步骤3具体过程如下:The specific process of step 3 is as follows:
采用镗刀进行粗镗孔,将发动机缸孔尺寸进行统一。The boring tool is used for rough boring, and the size of the engine cylinder hole is unified.
镗刀主偏角为45~75°。The main declination angle of the boring tool is 45 to 75°.
镗孔尺寸精度为IT18~IT17;表面粗糙度Ra为1.6~0.8μm。The dimensional accuracy of boring is IT18~IT17; the surface roughness Ra is 1.6~0.8μm.
步骤6具体过程如下:The specific process of step 6 is as follows:
采用镗刀进行静镗孔,修正发动机缸孔的圆柱度。The boring tool is used for static boring to correct the cylindricity of the engine cylinder bore.
镗刀主偏角为60~70°。The main declination angle of the boring tool is 60-70°.
本发明的有益效果是:The beneficial effects of the present invention are:
本发明一种发动机保养方法,能防止机油洒出,节约资源,避免注油时沙石的进入,也可防止灰尘进入,对发动机清洗的同时进行了局部易损部位的修复,不仅能清洁好发动机,延长其使用寿命,同时,提高了发动机的性能,使得发动机能更好的进行工作。The engine maintenance method of the invention can prevent oil from spilling, save resources, avoid the entry of sand and gravel during oil filling, and also prevent dust from entering, and repairs local vulnerable parts while cleaning the engine, not only can clean the engine well , prolong its service life, at the same time, improve the performance of the engine, so that the engine can work better.
具体实施方式Detailed ways
下面结合具体实施方式对本发明进行详细说明。The present invention will be described in detail below with reference to specific embodiments.
本发明一种发动机保养方法,具体按照以下步骤实施:An engine maintenance method of the present invention is specifically implemented according to the following steps:
步骤1、利用高压水对发动机进行冲洗,去除发动机周围的杂质;Step 1. Rinse the engine with high-pressure water to remove impurities around the engine;
步骤2、将发动机内参残余的油放出;Step 2. Drain the residual oil from the engine internal reference;
步骤3、第一次镗孔,通过机械加工统一发动机缸孔尺寸;Step 3. Boring for the first time, unify the cylinder hole size of the engine through machining;
步骤3具体过程如下:The specific process of step 3 is as follows:
采用镗刀进行粗镗孔,将发动机缸孔尺寸进行统一。The boring tool is used for rough boring, and the size of the engine cylinder hole is unified.
其中,镗刀主偏角为45~75°。Among them, the main declination angle of the boring tool is 45-75°.
镗孔尺寸精度为IT18~IT17;表面粗糙度Ra为1.6~0.8μm。The dimensional accuracy of boring is IT18~IT17; the surface roughness Ra is 1.6~0.8μm.
步骤4、喷涂,将涂层涂覆至发动机缸孔内;Step 4, spray, and apply the coating to the cylinder bore of the engine;
步骤5、铣顶面,对发动机空空顶部进行表面清理;Step 5. Mill the top surface and clean the surface of the empty top of the engine;
步骤6、第二次镗孔,通过机械加工修正发动机缸孔的圆柱度;Step 6. Boring for the second time, correct the cylindricity of the engine cylinder hole by machining;
步骤6具体过程如下:The specific process of step 6 is as follows:
采用镗刀进行静镗孔,修正发动机缸孔的圆柱度。The boring tool is used for static boring to correct the cylindricity of the engine cylinder bore.
其中,镗刀主偏角为60~70°。Among them, the main declination angle of the boring tool is 60-70°.
步骤7、珩磨,恢复发动机缸孔的尺寸和粗糙度。Step 7. Honing to restore the size and roughness of the engine cylinder bore.
实施例1Example 1
步骤1、利用高压水对发动机进行冲洗,去除发动机周围的杂质;Step 1. Rinse the engine with high-pressure water to remove impurities around the engine;
步骤2、将发动机内参残余的油放出;Step 2. Drain the residual oil from the engine internal reference;
步骤3、第一次镗孔,通过机械加工统一发动机缸孔尺寸;Step 3. Boring for the first time, unify the cylinder hole size of the engine through machining;
步骤3具体过程如下:The specific process of step 3 is as follows:
采用镗刀进行粗镗孔,将发动机缸孔尺寸进行统一。The boring tool is used for rough boring, and the size of the engine cylinder hole is unified.
其中,镗刀主偏角为45°。Among them, the main declination angle of the boring tool is 45°.
镗孔尺寸精度为IT18;表面粗糙度Ra为1.6μm。The dimensional accuracy of the boring hole is IT18; the surface roughness Ra is 1.6 μm.
步骤4、喷涂,将涂层涂覆至发动机缸孔内;Step 4, spray, and apply the coating to the cylinder bore of the engine;
步骤5、铣顶面,对发动机空空顶部进行表面清理;Step 5. Mill the top surface and clean the surface of the empty top of the engine;
步骤6、第二次镗孔,通过机械加工修正发动机缸孔的圆柱度;Step 6. Boring for the second time, correct the cylindricity of the engine cylinder hole by machining;
步骤6具体过程如下:The specific process of step 6 is as follows:
采用镗刀进行静镗孔,修正发动机缸孔的圆柱度。The boring tool is used for static boring to correct the cylindricity of the engine cylinder bore.
其中,镗刀主偏角为60°。Among them, the main declination angle of the boring tool is 60°.
步骤7、珩磨,恢复发动机缸孔的尺寸和粗糙度。Step 7. Honing to restore the size and roughness of the engine cylinder bore.
实施例2Example 2
步骤1、利用高压水对发动机进行冲洗,去除发动机周围的杂质;Step 1. Rinse the engine with high-pressure water to remove impurities around the engine;
步骤2、将发动机内参残余的油放出;Step 2. Drain the residual oil from the engine internal reference;
步骤3、第一次镗孔,通过机械加工统一发动机缸孔尺寸;Step 3. Boring for the first time, unify the cylinder hole size of the engine through machining;
步骤3具体过程如下:The specific process of step 3 is as follows:
采用镗刀进行粗镗孔,将发动机缸孔尺寸进行统一。The boring tool is used for rough boring, and the size of the engine cylinder hole is unified.
其中,镗刀主偏角为75°。Among them, the main declination angle of the boring tool is 75°.
镗孔尺寸精度为IT17;表面粗糙度Ra为0.8μm。The dimensional accuracy of the boring hole is IT17; the surface roughness Ra is 0.8 μm.
步骤4、喷涂,将涂层涂覆至发动机缸孔内;Step 4, spray, and apply the coating to the cylinder bore of the engine;
步骤5、铣顶面,对发动机空空顶部进行表面清理;Step 5. Mill the top surface and clean the surface of the empty top of the engine;
步骤6、第二次镗孔,通过机械加工修正发动机缸孔的圆柱度;Step 6. Boring for the second time, correct the cylindricity of the engine cylinder hole by machining;
步骤6具体过程如下:The specific process of step 6 is as follows:
采用镗刀进行静镗孔,修正发动机缸孔的圆柱度。The boring tool is used for static boring to correct the cylindricity of the engine cylinder bore.
其中,镗刀主偏角为0°。Among them, the main declination angle of the boring tool is 0°.
步骤7、珩磨,恢复发动机缸孔的尺寸和粗糙度。Step 7. Honing to restore the size and roughness of the engine cylinder bore.
实施例3Example 3
步骤1、利用高压水对发动机进行冲洗,去除发动机周围的杂质;Step 1. Rinse the engine with high-pressure water to remove impurities around the engine;
步骤2、将发动机内参残余的油放出;Step 2. Drain the residual oil from the engine internal reference;
步骤3、第一次镗孔,通过机械加工统一发动机缸孔尺寸;Step 3. Boring for the first time, unify the cylinder hole size of the engine through machining;
步骤3具体过程如下:The specific process of step 3 is as follows:
采用镗刀进行粗镗孔,将发动机缸孔尺寸进行统一。The boring tool is used for rough boring, and the size of the engine cylinder hole is unified.
其中,镗刀主偏角为60°。Among them, the main declination angle of the boring tool is 60°.
镗孔尺寸精度为IT18;表面粗糙度Ra为1.2μm。The dimensional accuracy of the boring hole is IT18; the surface roughness Ra is 1.2μm.
步骤4、喷涂,将涂层涂覆至发动机缸孔内;Step 4, spray, and apply the coating to the cylinder bore of the engine;
步骤5、铣顶面,对发动机空空顶部进行表面清理;Step 5. Mill the top surface and clean the surface of the empty top of the engine;
步骤6、第二次镗孔,通过机械加工修正发动机缸孔的圆柱度;Step 6. Boring for the second time, correct the cylindricity of the engine cylinder hole by machining;
步骤6具体过程如下:The specific process of step 6 is as follows:
采用镗刀进行静镗孔,修正发动机缸孔的圆柱度。The boring tool is used for static boring to correct the cylindricity of the engine cylinder bore.
其中,镗刀主偏角为65°。Among them, the main declination angle of the boring tool is 65°.
步骤7、珩磨,恢复发动机缸孔的尺寸和粗糙度。Step 7. Honing to restore the size and roughness of the engine cylinder bore.
本发明一种发动机保养方法,能防止机油洒出,节约资源,避免注油时沙石的进入,也可防止灰尘进入,对发动机清洗的同时进行了局部易损部位的修复,不仅能清洁好发动机,延长其使用寿命,同时,提高了发动机的性能,使得发动机能更好的进行工作。The engine maintenance method of the invention can prevent oil from spilling, save resources, avoid the entry of sand and gravel during oil filling, and also prevent dust from entering, and repairs local vulnerable parts while cleaning the engine, not only can clean the engine well , prolong its service life, at the same time, improve the performance of the engine, so that the engine can work better.
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1254738A2 (en) * | 2001-04-30 | 2002-11-06 | United Technologies Corporation | Automated system for repairing components |
| CN102114548A (en) * | 2010-01-05 | 2011-07-06 | 赵明理 | Special cutter bar for processing oil sleeve coupling |
| CN203791647U (en) * | 2014-01-20 | 2014-08-27 | 郑州市钻石精密制造有限公司 | Boring cutter for machining inner bore of automobile engine |
| CN106078077A (en) * | 2016-08-25 | 2016-11-09 | 张家港清研再制造产业研究院有限公司 | A kind of engine cylinder hole restorative procedure |
| CN107030447A (en) * | 2017-04-21 | 2017-08-11 | 张家港清研再制造产业研究院有限公司 | A kind of engine cylinder hole restorative procedure |
| CN109098816A (en) * | 2018-08-14 | 2018-12-28 | 倪岚霖 | A kind of vehicle motor maintenance method |
| CN109396476A (en) * | 2018-11-13 | 2019-03-01 | 武汉船用机械有限责任公司 | A kind of borehole processing method of parallel interior bores oil cylinder |
-
2019
- 2019-12-06 CN CN201911241090.2A patent/CN111299956A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1254738A2 (en) * | 2001-04-30 | 2002-11-06 | United Technologies Corporation | Automated system for repairing components |
| CN102114548A (en) * | 2010-01-05 | 2011-07-06 | 赵明理 | Special cutter bar for processing oil sleeve coupling |
| CN203791647U (en) * | 2014-01-20 | 2014-08-27 | 郑州市钻石精密制造有限公司 | Boring cutter for machining inner bore of automobile engine |
| CN106078077A (en) * | 2016-08-25 | 2016-11-09 | 张家港清研再制造产业研究院有限公司 | A kind of engine cylinder hole restorative procedure |
| CN107030447A (en) * | 2017-04-21 | 2017-08-11 | 张家港清研再制造产业研究院有限公司 | A kind of engine cylinder hole restorative procedure |
| CN109098816A (en) * | 2018-08-14 | 2018-12-28 | 倪岚霖 | A kind of vehicle motor maintenance method |
| CN109396476A (en) * | 2018-11-13 | 2019-03-01 | 武汉船用机械有限责任公司 | A kind of borehole processing method of parallel interior bores oil cylinder |
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