CN108890230A - A kind of loaded cylinder and its processing technology - Google Patents

A kind of loaded cylinder and its processing technology Download PDF

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Publication number
CN108890230A
CN108890230A CN201810795217.4A CN201810795217A CN108890230A CN 108890230 A CN108890230 A CN 108890230A CN 201810795217 A CN201810795217 A CN 201810795217A CN 108890230 A CN108890230 A CN 108890230A
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CN
China
Prior art keywords
construction section
inner cavity
pilot hole
section
processing technology
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
Application number
CN201810795217.4A
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Chinese (zh)
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CN108890230B (en
Inventor
王道
梁微子
赵李军
谢磊
徐宇超
杨文彪
邹吉亮
黄靖
姚珍军
潘忠
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hunan Nanfang General Aviation Engine Co Ltd
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Hunan Nanfang General Aviation Engine Co Ltd
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Publication date
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Priority to CN201810795217.4A priority Critical patent/CN108890230B/en
Publication of CN108890230A publication Critical patent/CN108890230A/en
Application granted granted Critical
Publication of CN108890230B publication Critical patent/CN108890230B/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B77/00Component parts, details or accessories, not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B77/00Component parts, details or accessories, not otherwise provided for
    • F02B77/08Safety, indicating, or supervising devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B77/00Component parts, details or accessories, not otherwise provided for
    • F02B77/08Safety, indicating, or supervising devices
    • F02B77/088Safety, indicating, or supervising devices relating to tightness

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

The invention discloses a kind of processing technologys of loaded cylinder, in processing, the construction section in the first process and assemble hole on the end face of inner cylinder, then inner cylinder and runner outer wall are welded, the construction section of the pilot hole is then sealed, the load segment of pilot hole is reprocessed.Since construction section is connected to inner cavity, it is not used to turn to match, therefore, the positioning requirements of construction section are reduced, and in process and assemble section, construction section can be sealed, the connection of load segment and inner cavity is obstructed, it prevents iron filings and other impurities to fall into inner cavity, to fundamentally prevent the pollution of inner cavity, greatly reduces security risk present in engine use process.Invention additionally discloses a kind of loaded cylinders with above-mentioned processing technology.

Description

A kind of loaded cylinder and its processing technology
Technical field
The present invention relates to technical field of engines, in particular to the processing technology of a kind of loaded cylinder and the processing technology is used Loaded cylinder.
Background technique
As shown in Figure 1, load tube kind part is since it is ventilated, thus all can be by a runner in design outside Wall 02 and an inner cylinder 01 are welded, and being situated between, there are inner cavities to guarantee that air-flow can pass through.In actual processing In the process, three pilot holes 03 being located on large end face communicated with inner cavity are due to needs and other component in subsequent assembly Positioning, therefore, there is the requirement of position degree, so three on the end face pilot hole 03 must be welded in runner outer wall 02 and inner cylinder 01 Completion is connect to be processed later.
But the cross-sectional view (Fig. 2) from the part assembling hole can be seen that pilot hole 03 and be connected directly with inner cavity of component, And pilot hole 03 is formed using number Milling Machining at this, inevitably having iron filings in process in this way can be along with cooling Liquid enters inner cavity of component, subsequent to be difficult to clean off completely, and inside parts is caused to have fifth wheel residual.
The type part is currently a part more crucial during new machine is developed, occurred in the past the type part due to Inner cavity of component has the presence of fifth wheel and whole part is caused to be decomposed again, so that there are great peaces in engine use process Full hidden danger.
Summary of the invention
In view of this, being used the purpose of the present invention is to provide a kind of processing technology of loaded cylinder with reducing engine Security risk present in journey.In addition, it is another object of the present invention to provide a kind of loaded cylinder using above-mentioned processing technology.
To achieve the above object, the present invention provides the following technical solutions:
A kind of processing technology of loaded cylinder comprising step:
The construction section in process and assemble hole on the predeterminated position of the end face of inner cylinder;
The inner cylinder and runner outer wall that the construction section will be processed weld, and the inner cylinder and the runner outer wall it Between form inner cavity, the construction section is connected to the inner cavity;
Seal the construction section of the pilot hole;
The end face positioning of the inner cylinder and the runner outer wall after welding, and the load segment in process and assemble hole, are opened The construction section, and the construction section is connected to the corresponding load segment.
Preferably, in above-mentioned processing technology, the construction section of the pilot hole is stepped hole, and one far from the inner cavity The diameter of section is greater than one section of the diameter close to the inner cavity.
Preferably, in above-mentioned processing technology, the protective plug that elasticity is installed in the construction section seals the pilot hole Construction section.
Preferably, in above-mentioned processing technology, the protective plug is located at the construction section close to one section of the inner cavity.
Preferably, in above-mentioned processing technology, the construction section is threaded hole, and seals the installation by screw element Section.
Preferably, in above-mentioned processing technology, the diameter of the construction section of the pilot hole is less than the assembly of the pilot hole The diameter of section.
Preferably, in above-mentioned processing technology, the load segment uses number Milling Machining.
A kind of loaded cylinder, including:It welds the inner cylinder for forming inner cavity and runner outer wall and is located at the inner cylinder and the stream The pilot hole of pipeline outer wall end face, wherein the pilot hole includes the construction section of the load segment and removable seal for assembly, institute It states construction section to be connected to the inner cavity, the load segment can be connected to the construction section.
As can be seen from the above technical solutions, loaded cylinder disclosed in this invention is in processing, first on the end face of inner cylinder The construction section in process and assemble hole, then inner cylinder and runner outer wall are welded, then seal the construction section of the pilot hole, reprocessing assembly The load segment in hole.It since construction section is connected to inner cavity, is not used to turn to match, therefore, the positioning requirements of construction section is reduced, and In process and assemble section, construction section can be sealed, obstruct the connection of load segment and inner cavity, it is therefore prevented that iron filings are miscellaneous with other Matter is fallen into inner cavity, to fundamentally prevent the pollution of inner cavity, is greatly reduced present in engine use process Security risk.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below to embodiment or existing Attached drawing needed in technical description is briefly described, it is clear that, the accompanying drawings in the following description is only this hair Bright embodiment for those of ordinary skill in the art without creative efforts, can also be according to mentioning The attached drawing of confession obtains other attached drawings.
Fig. 1 is the top view of loaded cylinder disclosed in the prior art;
Fig. 2 is the front sectional view of loaded cylinder disclosed in the prior art;
Fig. 3 is the flow chart of the processing technology of the loaded cylinder disclosed in the embodiment of the present invention;
Fig. 4 is the front sectional view of the loaded cylinder disclosed in the embodiment of the present invention.
Specific embodiment
In view of this, core of the invention is to provide a kind of processing technology of loaded cylinder, used with reducing engine Security risk present in journey.Another core of the invention is providing a kind of loaded cylinder using above-mentioned processing technology.
In order to enable those skilled in the art to better understand the solution of the present invention, with reference to the accompanying drawings and detailed description The present invention is described in further detail.
As shown in Figure 3 and Figure 4, the invention discloses a kind of loaded cylinders in processing, and dress is first processed on the end face of inner cylinder 1 The construction section 3 of distribution, then inner cylinder 1 and runner outer wall 2 are welded, the construction section 3 of the pilot hole is then sealed, pilot hole is reprocessed Load segment 4.
Specific procedure of processing is as follows:
Step S1:The construction section in process and assemble hole on the predeterminated position of the end face of inner cylinder.
The construction section 3 of the pilot hole is directly processed when inner cylinder 1 is processed, specifically, can pass through several Milling Machinings.This Shen Please in predeterminated position be former loaded cylinder pilot hole Position Approximate, due to the construction section 3 of pilot hole be not intended to and other The part of component assembling, therefore, the status requirement of the construction section 3 are lower, do not need to be accurately positioned.
Step S2:The inner cylinder for processing construction section and runner outer wall are welded, and formed between inner cylinder and runner outer wall Inner cavity, and above-mentioned construction section is connected to inner cavity.
Inner cylinder 1 and runner outer wall 2 are welded again after processing construction section 3, which is connected to inner cavity, on the one hand needs It completes pipeline with inner cavity connection, on the other hand can also reduce the requirement to assembly hole site.
Step S3:Seal the construction section of pilot hole.
The construction section 3 of pilot hole is sealed, inner cavity and extraneous connection can be prevented in this way, is prevented in extraneous impurity entrance Chamber avoids the pollution of inner cavity.
Step S4:The end face positioning of inner cylinder and runner outer wall after welding, and the load segment in process and assemble hole, open peace Section is filled, and the construction section is connected to corresponding load segment.
It since construction section 3 is connected to inner cavity, is not used to assemble, therefore, low to the positioning requirements of construction section 3, Er Qie When process and assemble section 4, construction section 3 can be sealed, obstruct the connection of load segment 3 Yu inner cavity, it is therefore prevented that iron filings and other Impurity is fallen into inner cavity, to fundamentally prevent the pollution of inner cavity, greatly reduces and exists in engine use process Security risk.
The construction section 3 of pilot hole in the application is stepped hole, and one section of the diameter far from inner cavity is greater than close to interior One section of diameter of chamber.Furthermore the purpose for stepped hole being arranged is sealed for the ease of the construction section 3 to pilot hole.In reality In, the size of stepped hole can be set as needed, specifically, one section of the diameter that can will be close to inner cavity is set as 9.5mm, it will One section of the diameter far from inner cavity is set as 10.25mm.
There is provided herein the sealing means of construction section 3, specifically, installing the protective plug of elasticity in construction section 3 to realize Sealing to construction section 3.One section of diameter of the stepped hole close to inner cavity in the application is smaller, blocks protective plug to facilitate.It adopts With the mode not only good airproof performance, but also easy disassembly of spring protective plug.
In order to avoid influencing the processing to the load segment 4 of pilot hole, it is preferred that protective plug is arranged close in construction section 3 One section of inner cavity.It is lower than the depth of the load segment 4 of pilot hole after mounting for protective plug.
In another embodiment, also threaded hole can be set by the construction section 3 of pilot hole, and is pacified by screw element sealing cover Fill section 3.As long as it will be appreciated by persons skilled in the art that can be realized it is being connected to inner cavity and can dismountable mode it is equal In protection scope.
Based on the above technical solution, the diameter of the construction section of pilot hole 3 is set smaller than to the assembly of pilot hole The diameter of section 4.It, can be directly on the basis of construction section 3 when the load segment 4 to pilot hole is processed in conjunction with above-mentioned setting Expand a hole to come out.
The processing of load segment 4 can be completed by way of several Milling Machinings.
In addition, including the inner cylinder 1 and runner outer wall 2 welded together, the two exists disclosed herein as well is a kind of loaded cylinder Gap is formed between after welding, and end face has pilot hole, the core of the application is that the pilot hole includes for assembly The construction section 3 of load segment 4 and removable seal, wherein construction section 3 is connected to inner cavity, and load segment 4 can connect with construction section 3 It is logical.
It since construction section 3 is connected to inner cavity, is not used to assemble, therefore, the positioning requirements of construction section 3 is reduced, and In process and assemble section 4, construction section 3 can be sealed, obstruct the connection of load segment 4 Yu inner cavity, it is therefore prevented that iron filings and its He falls into inner cavity impurity, to fundamentally prevent the pollution of inner cavity, greatly reduces and deposits in engine use process Security risk.
The structure in the structure of construction section 3 and load segment 4 and the processing technology of loaded cylinder for the pilot hole of loaded cylinder It is identical, not described in detail herein.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other The difference of embodiment, the same or similar parts in each embodiment may refer to each other.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one The widest scope of cause.

Claims (8)

1. a kind of processing technology of loaded cylinder, which is characterized in that including step:
The construction section (3) in process and assemble hole on the predeterminated position of the end face of inner cylinder (1);
The inner cylinder (1) and runner outer wall (2) that the construction section (3) will be processed weld, and the inner cylinder (1) and the stream Inner cavity is formed between pipeline outer wall (2), the construction section (3) is connected to the inner cavity (1);
Seal the construction section (3) of the pilot hole;
The end face positioning of the inner cylinder (1) and the runner outer wall (2) after welding, and the load segment (4) in process and assemble hole, It opens the construction section (3), and the construction section (1) is connected to the corresponding load segment (4).
2. processing technology according to claim 1, which is characterized in that the construction section (3) of the pilot hole is stepped hole, and One section of the diameter far from the inner cavity is greater than one section of the diameter close to the inner cavity.
3. processing technology according to claim 2, which is characterized in that the protection of installation elasticity in the construction section (3) Plug seals the construction section (3) of the pilot hole.
4. processing technology according to claim 3, which is characterized in that it is close that the protective plug is located at the construction section (3) One section of the inner cavity.
5. processing technology according to claim 1, which is characterized in that the construction section (3) is threaded hole, and passes through screw thread Part seals the construction section (3).
6. processing technology according to claim 1-5, which is characterized in that the construction section (3) of the pilot hole Diameter is less than the diameter of the load segment (4) of the pilot hole.
7. processing technology according to claim 1-5, which is characterized in that the load segment (4) is added using number milling Work.
8. a kind of loaded cylinder is processed using the described in any item processing technologys of such as claim 1-7, including:Welding forms inner cavity Inner cylinder (1) and runner outer wall (2) and be located at the inner cylinder (1) and the runner outer wall (2) end face pilot hole, feature Be, the pilot hole includes the construction section (4) of the load segment (3) and removable seal for assembly, the construction section (3) with The inner cavity connection, the load segment (4) can be connected to the construction section (3).
CN201810795217.4A 2018-07-19 2018-07-19 A kind of loaded cylinder and its processing technology Active CN108890230B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810795217.4A CN108890230B (en) 2018-07-19 2018-07-19 A kind of loaded cylinder and its processing technology

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Application Number Priority Date Filing Date Title
CN201810795217.4A CN108890230B (en) 2018-07-19 2018-07-19 A kind of loaded cylinder and its processing technology

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CN108890230A true CN108890230A (en) 2018-11-27
CN108890230B CN108890230B (en) 2019-10-01

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60259336A (en) * 1985-04-19 1985-12-21 Hiroshi Teramachi Method of manufacturing outer bearing cylinder used in endlessly sliding ball spline
CN103302453A (en) * 2013-06-07 2013-09-18 浙江坤博机械制造有限公司 Machining method for valve body of low temperature resistance hard seal check valve
CN103647133A (en) * 2013-12-17 2014-03-19 西安航天复合材料研究所 Composite material base for satellite antenna bearing cylinder and preparation method
CN103682562A (en) * 2013-12-17 2014-03-26 西安航天复合材料研究所 Base made of composite materials and manufacturing method thereof
CN105034355A (en) * 2015-06-26 2015-11-11 上海复合材料科技有限公司 Preparing method of bearing cylinder
CN108019484A (en) * 2016-11-02 2018-05-11 晋江市华峰齿轮制造有限公司 The wheel stand and its manufacture craft of a kind of high finished product rate

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60259336A (en) * 1985-04-19 1985-12-21 Hiroshi Teramachi Method of manufacturing outer bearing cylinder used in endlessly sliding ball spline
CN103302453A (en) * 2013-06-07 2013-09-18 浙江坤博机械制造有限公司 Machining method for valve body of low temperature resistance hard seal check valve
CN103647133A (en) * 2013-12-17 2014-03-19 西安航天复合材料研究所 Composite material base for satellite antenna bearing cylinder and preparation method
CN103682562A (en) * 2013-12-17 2014-03-26 西安航天复合材料研究所 Base made of composite materials and manufacturing method thereof
CN105034355A (en) * 2015-06-26 2015-11-11 上海复合材料科技有限公司 Preparing method of bearing cylinder
CN108019484A (en) * 2016-11-02 2018-05-11 晋江市华峰齿轮制造有限公司 The wheel stand and its manufacture craft of a kind of high finished product rate

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