CN111299956A - Engine maintenance method - Google Patents
Engine maintenance method Download PDFInfo
- Publication number
- 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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- Prior art keywords
- engine
- boring
- cylinder hole
- maintenance method
- machining
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Classifications
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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
-
- 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
-
- 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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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
The invention discloses an engine maintenance method, which is implemented according to the following steps: step 1, washing an engine by using high-pressure water to remove impurities around the engine; step 2, discharging residual oil of the internal parameters of the engine; step 3, boring for the first time, wherein the size of the engine cylinder hole is unified through machining; step 4, spraying, namely coating the coating into the cylinder hole of the engine; step 5, milling a top surface, and performing surface cleaning on the empty top of the engine; step 6, boring for the second time, wherein the cylindricity of the engine cylinder hole is corrected through machining; and 7, honing, and recovering the size and the roughness of the engine cylinder hole. The invention relates to an engine maintenance method, which repairs a local vulnerable part while cleaning an engine.
Description
Technical Field
The invention belongs to the technical field of engine maintenance, and particularly relates to an engine maintenance method.
Background
An engine is a machine capable of converting other forms of energy into mechanical energy, including, for example, internal combustion engines (reciprocating piston engines), external combustion engines (stirling engines, steam engines, etc.), jet engines, electric motors, and the like. Such as internal combustion engines, typically convert chemical energy into mechanical energy. The engine is suitable for a power generation device, and can also refer to the whole machine (such as a gasoline engine and an aircraft engine) comprising the power device. Engines were first introduced in the united kingdom, and the engine concept is also derived from english, which is meant in its meaning as "power generating machinery".
External combustion engines, that is, their fuel is burned externally of the engine, invented in 1816 by r. The engine converts the heat energy generated by the combustion into kinetic energy, the watt-improved steam engine is a typical external combustion engine, when a large amount of coal is combusted to generate heat energy to heat water into a large amount of water vapor, high pressure is generated, and then the high pressure pushes the machine to do work, so that the conversion of the heat energy into the kinetic energy is completed.
Internal combustion engines, i.e. reciprocating piston engines, differ from external combustion engines in that their fuel is burnt in the interior thereof. The internal combustion engines are very diverse, and common gasoline engines and common diesel engines are typical internal combustion engines.
The gas turbine engine is characterized in that high-pressure gas is generated by combustion, and the high pressure of the gas is used for pushing blades of the gas turbine to rotate so as to output power. Gas turbines are used in a wide range, but since it is difficult to finely adjust the output power, automobiles and motorcycles rarely use gas turbines, and only some racing vehicles use gas turbines.
Jet engines are engines that generate reactive thrust directly from the high velocity jet of air from a jet. Widely used as power devices for aircrafts. The fuel and oxidant chemically react in the combustion chamber to release thermal energy, which is then converted in the nozzle to a function of conditioning the gas stream. In addition to fuel, oxidants carried by aircraft are known as rocket engines, including solid-fuel rocket engines and liquid-fuel rocket engines.
Disclosure of Invention
The invention aims to provide an engine maintenance method, which is used for repairing a partially damaged part while cleaning an engine.
The invention adopts the technical scheme that an engine maintenance method is implemented according to the following steps:
step 1, washing an engine by using high-pressure water to remove impurities around the engine;
step 2, discharging residual oil of the internal parameters of the engine;
step 3, boring for the first time, wherein the size of the engine cylinder hole is unified through machining;
step 4, spraying, namely coating the coating into the cylinder hole of the engine;
step 5, milling a top surface, and performing surface cleaning on the empty top of the engine;
step 6, boring for the second time, wherein the cylindricity of the engine cylinder hole is corrected through machining;
and 7, honing, and recovering the size and the roughness of the engine cylinder hole.
The invention is also characterized in that:
the specific process of the step 3 is as follows:
and carrying out rough boring by using a boring cutter, and unifying the sizes of the engine cylinder holes.
The main deflection angle of the boring cutter is 45-75 degrees.
The size precision of the boring hole is IT 18-IT 17; the surface roughness Ra is 1.6-0.8 μm.
The specific process of the step 6 is as follows:
and (4) performing static boring by using a boring cutter, and correcting the cylindricity of the engine cylinder hole.
The main deflection angle of the boring cutter is 60-70 degrees.
The invention has the beneficial effects that:
the engine maintenance method can prevent engine oil from spilling, save resources, avoid sand and stone entering during oil injection, prevent dust from entering, repair local vulnerable parts while cleaning the engine, clean the engine, prolong the service life of the engine, improve the performance of the engine and enable the engine to work better.
Detailed Description
The present invention will be described in detail with reference to the following embodiments.
The invention relates to an engine maintenance method, which is implemented according to the following steps:
step 1, washing an engine by using high-pressure water to remove impurities around the engine;
step 2, discharging residual oil of the internal parameters of the engine;
step 3, boring for the first time, wherein the size of the engine cylinder hole is unified through machining;
the specific process of the step 3 is as follows:
and carrying out rough boring by using a boring cutter, and unifying the sizes of the engine cylinder holes.
Wherein, the main deflection angle of the boring cutter is 45-75 degrees.
The size precision of the boring hole is IT 18-IT 17; the surface roughness Ra is 1.6-0.8 μm.
Step 4, spraying, namely coating the coating into the cylinder hole of the engine;
step 5, milling a top surface, and performing surface cleaning on the empty top of the engine;
step 6, boring for the second time, wherein the cylindricity of the engine cylinder hole is corrected through machining;
the specific process of the step 6 is as follows:
and (4) performing static boring by using a boring cutter, and correcting the cylindricity of the engine cylinder hole.
Wherein, the main deflection angle of the boring cutter is 60-70 degrees.
And 7, honing, and recovering the size and the roughness of the engine cylinder hole.
Example 1
Step 1, washing an engine by using high-pressure water to remove impurities around the engine;
step 2, discharging residual oil of the internal parameters of the engine;
step 3, boring for the first time, wherein the size of the engine cylinder hole is unified through machining;
the specific process of the step 3 is as follows:
and carrying out rough boring by using a boring cutter, and unifying the sizes of the engine cylinder holes.
Wherein, the main deflection angle of the boring cutter is 45 degrees.
The bore hole size precision is IT 18; the surface roughness Ra was 1.6. mu.m.
Step 4, spraying, namely coating the coating into the cylinder hole of the engine;
step 5, milling a top surface, and performing surface cleaning on the empty top of the engine;
step 6, boring for the second time, wherein the cylindricity of the engine cylinder hole is corrected through machining;
the specific process of the step 6 is as follows:
and (4) performing static boring by using a boring cutter, and correcting the cylindricity of the engine cylinder hole.
Wherein, the main deflection angle of the boring cutter is 60 degrees.
And 7, honing, and recovering the size and the roughness of the engine cylinder hole.
Example 2
Step 1, washing an engine by using high-pressure water to remove impurities around the engine;
step 2, discharging residual oil of the internal parameters of the engine;
step 3, boring for the first time, wherein the size of the engine cylinder hole is unified through machining;
the specific process of the step 3 is as follows:
and carrying out rough boring by using a boring cutter, and unifying the sizes of the engine cylinder holes.
Wherein, the main deflection angle of the boring cutter is 75 degrees.
The bore hole size precision is IT 17; the surface roughness Ra was 0.8. mu.m.
Step 4, spraying, namely coating the coating into the cylinder hole of the engine;
step 5, milling a top surface, and performing surface cleaning on the empty top of the engine;
step 6, boring for the second time, wherein the cylindricity of the engine cylinder hole is corrected through machining;
the specific process of the step 6 is as follows:
and (4) performing static boring by using a boring cutter, and correcting the cylindricity of the engine cylinder hole.
Wherein, the main deflection angle of the boring cutter is 0 degree.
And 7, honing, and recovering the size and the roughness of the engine cylinder hole.
Example 3
Step 1, washing an engine by using high-pressure water to remove impurities around the engine;
step 2, discharging residual oil of the internal parameters of the engine;
step 3, boring for the first time, wherein the size of the engine cylinder hole is unified through machining;
the specific process of the step 3 is as follows:
and carrying out rough boring by using a boring cutter, and unifying the sizes of the engine cylinder holes.
Wherein, the main deflection angle of the boring cutter is 60 degrees.
The bore hole size precision is IT 18; the surface roughness Ra was 1.2. mu.m.
Step 4, spraying, namely coating the coating into the cylinder hole of the engine;
step 5, milling a top surface, and performing surface cleaning on the empty top of the engine;
step 6, boring for the second time, wherein the cylindricity of the engine cylinder hole is corrected through machining;
the specific process of the step 6 is as follows:
and (4) performing static boring by using a boring cutter, and correcting the cylindricity of the engine cylinder hole.
Wherein, the main deflection angle of the boring cutter is 65 degrees.
And 7, honing, and recovering the size and the roughness of the engine cylinder hole.
The engine maintenance method can prevent engine oil from spilling, save resources, avoid sand and stone entering during oil injection, prevent dust from entering, repair local vulnerable parts while cleaning the engine, clean the engine, prolong the service life of the engine, improve the performance of the engine and enable the engine to work better.
Claims (6)
1. An engine maintenance method is characterized by being implemented according to the following steps:
step 1, washing an engine by using high-pressure water to remove impurities around the engine;
step 2, discharging residual oil of the internal parameters of the engine;
step 3, boring for the first time, wherein the size of the engine cylinder hole is unified through machining;
step 4, spraying, namely coating the coating into the cylinder hole of the engine;
step 5, milling a top surface, and performing surface cleaning on the empty top of the engine;
step 6, boring for the second time, wherein the cylindricity of the engine cylinder hole is corrected through machining;
and 7, honing, and recovering the size and the roughness of the engine cylinder hole.
2. The engine servicing method according to claim 1, wherein the step 3 is embodied as follows:
and carrying out rough boring by using a boring cutter, and unifying the sizes of the engine cylinder holes.
3. The engine maintenance method according to claim 2, wherein the boring tool main slip angle is 45 to 75 °.
4. The engine servicing method of claim 2, wherein the bore hole dimensional accuracy is IT 18-IT 17; the surface roughness Ra is 1.6-0.8 μm.
5. The engine servicing method according to claim 1, wherein the step 6 is embodied as follows:
and (4) performing static boring by using a boring cutter, and correcting the cylindricity of the engine cylinder hole.
6. The engine maintenance method according to claim 5, wherein the boring tool main slip angle is 60 to 70 °.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201911241090.2A CN111299956A (en) | 2019-12-06 | 2019-12-06 | Engine maintenance method |
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CN201911241090.2A CN111299956A (en) | 2019-12-06 | 2019-12-06 | Engine maintenance method |
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CN111299956A true CN111299956A (en) | 2020-06-19 |
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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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