CN104400452A - High-temperature alloy honeycomb part milling processing clamping method - Google Patents
High-temperature alloy honeycomb part milling processing clamping method Download PDFInfo
- Publication number
- CN104400452A CN104400452A CN201410605880.5A CN201410605880A CN104400452A CN 104400452 A CN104400452 A CN 104400452A CN 201410605880 A CN201410605880 A CN 201410605880A CN 104400452 A CN104400452 A CN 104400452A
- Authority
- CN
- China
- Prior art keywords
- alloy honeycomb
- honeycomb part
- heat
- temperature alloy
- resisting alloy
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
- B23Q3/02—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
- B23Q3/06—Work-clamping means
- B23Q3/08—Work-clamping means other than mechanically-actuated
- B23Q3/086—Work-clamping means other than mechanically-actuated using a solidifying liquid, e.g. with freezing, setting or hardening means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
- B23Q3/15—Devices for holding work using magnetic or electric force acting directly on the work
- B23Q3/154—Stationary devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q2703/00—Work clamping
- B23Q2703/02—Work clamping means
- B23Q2703/10—Devices for clamping workpieces of a particular form or made from a particular material
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Heat Treatment Of Articles (AREA)
Abstract
The invention provides a high-temperature alloy honeycomb part milling processing clamping method, and belongs to the technical field of aerogenerator manufacturing. The invention provides the high-temperature alloy honeycomb part milling processing clamping method with the advantages of operation and removal simplicity, low cost and high clamping reliability. The clamping method provided by the invention comprises the following steps that 1, industrial paraffin and steel pills or cast iron pills are mixed and heated to a fusion state; 2, lattices of the high-temperature alloy honeycomb part to be processed are filled with the mixture of the industrial paraffin and the steel pills or cast iron pills heated to the fusion state, after the cooling, the two sides are trimmed to a flat state, and a high-temperature alloy honeycomb part blank is obtained; 3, the high-temperature alloy honeycomb part blank is absorbed by a magnetic force platform, and can be subjected to the milling processing.
Description
Technical field
The invention belongs to aero-engine manufacturing technology field, particularly relate to a kind of heat-resisting alloy honeycomb part Milling Machining clamp method.
Background technology
At present, existing heat-resisting alloy honeycomb part Milling Machining clamp method is: stick with glue or fix heat-resisting alloy honeycomb part by the method for vacuum suction.Gluing method operation and removal complexity, clamping poor reliability; The method cost of investment of vacuum suction is relatively large, and the part of clamping has certain limitation.
Summary of the invention
For prior art Problems existing, the invention provides a kind of operation and remove simple, that cost is low, clamping reliability is strong heat-resisting alloy honeycomb part Milling Machining clamp method.
To achieve these goals, the present invention adopts following technical scheme, and a kind of heat-resisting alloy honeycomb part Milling Machining clamp method, comprises the steps:
Step one: industrial paraffin and shot or cast iron pellets are mixed and heated to molten condition;
Step 2: be filled in the space of heat-resisting alloy honeycomb part to be processed by the mixture of the industrial paraffin and shot or cast iron pellets that are heated to molten condition, two sides equating after cooling obtains heat-resisting alloy honeycomb part blank;
Step 3: by the magnetic force platform absorption of heat-resisting alloy honeycomb part blank, Milling Machining can be carried out to it.
Being mixed with shot or cast iron pellets by industrial paraffin described in step one is with percentage by weight 1: the ratio of (0.3 ~ 1) mixes.
Beneficial effect of the present invention:
The invention solves heat-resisting alloy honeycomb part because the problem of nonmagnetic NC Milling clamping difficulty, make heat-resisting alloy honeycomb part by numerical control Milling Machining become very simple, effective; Its operation and removal are simply, cost is low, clamping reliability is strong.
Be applied in by clamp method of the present invention in the development process of aircraft of new generation or engine, the Huge value created, annual material of saving at least is worth millions of.
Accompanying drawing explanation
Fig. 1 is the structural representation of heat-resisting alloy honeycomb part to be processed;
Fig. 2 is the top view of Fig. 1;
Fig. 3 is the structural representation of heat-resisting alloy honeycomb part blank;
In figure: 1-heat-resisting alloy honeycomb part to be processed, the space of 2-heat-resisting alloy honeycomb part to be processed, the mixture (i.e. filler) of 3-industrial paraffin and shot or cast iron pellets.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention is described in further detail.
A kind of heat-resisting alloy honeycomb part Milling Machining clamp method, comprises the steps:
Step one: by the shot of industrial paraffin and shot-peening or cast iron pellets with percentage by weight 1: the ratio of (0.3 ~ 1) is mixed and heated to molten condition;
Step 2: the mixture of the industrial paraffin and shot or cast iron pellets that are heated to molten condition is filled in the space 2 of heat-resisting alloy honeycomb part to be processed, two sides equating after cooling obtains heat-resisting alloy honeycomb part blank, the structure of heat-resisting alloy honeycomb part blank, as shown in Figure 3; The structure of heat-resisting alloy honeycomb part to be processed, as shown in Figure 1 and Figure 2;
Step 3: by the magnetic force platform absorption of heat-resisting alloy honeycomb part blank, namely by digital control processing, its Milling Machining is become the shape of needs.
After machining, by adding the mixture (i.e. filler) 3 of heat abstraction industrial paraffin and shot or cast iron pellets; Then clean, the heat-resisting alloy honeycomb part needed can be obtained.
Claims (2)
1. a heat-resisting alloy honeycomb part Milling Machining clamp method, is characterized in that, comprise the steps:
Step one: industrial paraffin and shot or cast iron pellets are mixed and heated to molten condition;
Step 2: be filled in the space of heat-resisting alloy honeycomb part to be processed by the mixture of the industrial paraffin and shot or cast iron pellets that are heated to molten condition, two sides equating after cooling obtains heat-resisting alloy honeycomb part blank;
Step 3: by the magnetic force platform absorption of heat-resisting alloy honeycomb part blank, Milling Machining can be carried out to it.
2. heat-resisting alloy honeycomb part Milling Machining clamp method according to claim 1, is characterized in that being mixed with shot or cast iron pellets by industrial paraffin described in step one is with percentage by weight 1: the ratio of (0.3 ~ 1) mixes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410605880.5A CN104400452A (en) | 2014-10-31 | 2014-10-31 | High-temperature alloy honeycomb part milling processing clamping method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410605880.5A CN104400452A (en) | 2014-10-31 | 2014-10-31 | High-temperature alloy honeycomb part milling processing clamping method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104400452A true CN104400452A (en) | 2015-03-11 |
Family
ID=52638151
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410605880.5A Pending CN104400452A (en) | 2014-10-31 | 2014-10-31 | High-temperature alloy honeycomb part milling processing clamping method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104400452A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104690572A (en) * | 2015-03-17 | 2015-06-10 | 什邡市明日宇航工业股份有限公司 | Weakly rigid aviation structural member small stress filling and shock absorption clamping machining method |
| CN115139126A (en) * | 2022-08-12 | 2022-10-04 | 姚青叶 | Positioning device for machining engine body of internal combustion engine |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5131637A (en) * | 1991-05-13 | 1992-07-21 | Vaught James V | Work holder for honeycomb structure |
| DE4130623A1 (en) * | 1990-06-02 | 1993-03-18 | Eurocopter Deutschland | Process to mfr. sandwich panel with honeycomb core and convex surfaces - has sheet of thermoplastics on one side of core which is heated and drawn into cells by pneumatic pressure or suction |
| CN1346730A (en) * | 2001-10-18 | 2002-05-01 | 浙江大学 | Method for machining cellular flexible structure material |
| CN1775467A (en) * | 2005-12-07 | 2006-05-24 | 浙江大学 | Non ferromagnetic honey comb core material high-speed milling fixing platform |
| CN102581650A (en) * | 2011-11-01 | 2012-07-18 | 成都飞机工业（集团）有限责任公司 | Method for vacuum absorbing fixedly holding honeycomb part |
| CN103801740A (en) * | 2012-11-14 | 2014-05-21 | 江西昌河航空工业有限公司 | Honeycomb part machining method |
-
2014
- 2014-10-31 CN CN201410605880.5A patent/CN104400452A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4130623A1 (en) * | 1990-06-02 | 1993-03-18 | Eurocopter Deutschland | Process to mfr. sandwich panel with honeycomb core and convex surfaces - has sheet of thermoplastics on one side of core which is heated and drawn into cells by pneumatic pressure or suction |
| US5131637A (en) * | 1991-05-13 | 1992-07-21 | Vaught James V | Work holder for honeycomb structure |
| CN1346730A (en) * | 2001-10-18 | 2002-05-01 | 浙江大学 | Method for machining cellular flexible structure material |
| CN1775467A (en) * | 2005-12-07 | 2006-05-24 | 浙江大学 | Non ferromagnetic honey comb core material high-speed milling fixing platform |
| CN102581650A (en) * | 2011-11-01 | 2012-07-18 | 成都飞机工业（集团）有限责任公司 | Method for vacuum absorbing fixedly holding honeycomb part |
| CN103801740A (en) * | 2012-11-14 | 2014-05-21 | 江西昌河航空工业有限公司 | Honeycomb part machining method |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104690572A (en) * | 2015-03-17 | 2015-06-10 | 什邡市明日宇航工业股份有限公司 | Weakly rigid aviation structural member small stress filling and shock absorption clamping machining method |
| CN115139126A (en) * | 2022-08-12 | 2022-10-04 | 姚青叶 | Positioning device for machining engine body of internal combustion engine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150311 |
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| RJ01 | Rejection of invention patent application after publication |