US20080034565A1 - Methods and apparatus for an annular core cutter - Google Patents
Methods and apparatus for an annular core cutter Download PDFInfo
- Publication number
- US20080034565A1 US20080034565A1 US11/464,082 US46408206A US2008034565A1 US 20080034565 A1 US20080034565 A1 US 20080034565A1 US 46408206 A US46408206 A US 46408206A US 2008034565 A1 US2008034565 A1 US 2008034565A1
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- United States
- Prior art keywords
- cutting
- spindle
- cutting head
- workpiece
- generally
- 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
Links
- 238000000034 method Methods 0.000 title claims description 10
- 238000005520 cutting process Methods 0.000 claims abstract description 73
- 239000011162 core material Substances 0.000 claims description 24
- 239000002699 waste material Substances 0.000 abstract description 2
- 239000000463 material Substances 0.000 description 12
- 238000003754 machining Methods 0.000 description 10
- 239000006260 foam Substances 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- 229910000997 High-speed steel Inorganic materials 0.000 description 1
- 229920000271 Kevlar® Polymers 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 239000004761 kevlar Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C5/00—Milling-cutters
- B23C5/02—Milling-cutters characterised by the shape of the cutter
- B23C5/10—Shank-type cutters, i.e. with an integral shaft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B51/00—Tools for drilling machines
- B23B51/04—Drills for trepanning
- B23B51/0413—Drills for trepanning with core-cutting-off devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C2226/00—Materials of tools or workpieces not comprising a metal
- B23C2226/62—Polystyrene foam
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C2228/00—Properties of materials of tools or workpieces, materials of tools or workpieces applied in a specific manner
- B23C2228/25—Honeycomb
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/51—Plural diverse manufacturing apparatus including means for metal shaping or assembling
- Y10T29/5147—Plural diverse manufacturing apparatus including means for metal shaping or assembling including composite tool
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/51—Plural diverse manufacturing apparatus including means for metal shaping or assembling
- Y10T29/5176—Plural diverse manufacturing apparatus including means for metal shaping or assembling including machining means
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T407/00—Cutters, for shaping
- Y10T407/11—Cutters, for shaping including chip breaker, guide or deflector detachable from tool and tool holder
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T408/00—Cutting by use of rotating axially moving tool
- Y10T408/34—Combined cutting means
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T408/00—Cutting by use of rotating axially moving tool
- Y10T408/50—Cutting by use of rotating axially moving tool with product handling or receiving means
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T409/00—Gear cutting, milling, or planing
- Y10T409/30—Milling
- Y10T409/303752—Process
- Y10T409/303808—Process including infeeding
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T409/00—Gear cutting, milling, or planing
- Y10T409/30—Milling
- Y10T409/304088—Milling with means to remove chip
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T409/00—Gear cutting, milling, or planing
- Y10T409/30—Milling
- Y10T409/304144—Means to trim edge
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T409/00—Gear cutting, milling, or planing
- Y10T409/30—Milling
- Y10T409/30952—Milling with cutter holder
Definitions
- the present invention generally relates to machining technology and, more particularly, to automated core machining of materials such as foam and honeycomb-core materials.
- core materials When performing automated machining of certain materials, such as foam and honeycomb-core materials (generally referred to as “core” materials), certain geometries may be encountered that are difficult or impossible to produce using standard circular disk cutters. That is, the head of such cutters are prone to impacting the core and inadvertently damaging or destroying the workpiece.
- a workpiece 102 is machined using a cutting head 104 including a cutting disk 106 attached to a rotating spindle 105 , wherein spindle 105 has a rotational axis 110 , and wherein the cutting direction 112 of cutting head 104 is substantially perpendicular (within a small lead angle ⁇ ) to rotational axis 110 .
- rotational axis 110 of spindle 105 is maintained, during a cutting operation, substantially normal to the plane of the work surface 103 .
- a core cutting apparatus includes a cutting head including a generally cylindrical sidewall having a first end and a second end, wherein the first end has a cutting edge, and wherein the sidewall includes a plurality of openings having at least one sharpened edge.
- a spindle is coaxially and rigidly coupled to the second end of the cylindrical sidewall, and the spindle configured to rotate about a rotational axis.
- a generally conical member is disposed within the cutting apparatus to assist with grinding and removal of waste material.
- FIG. 1 is an overview of a typical prior art circular disk cutting operation
- FIG. 2 is a core carving apparatus in accordance with one embodiment of the present invention.
- FIG. 3 is an overview of a core carving operation in accordance with the present invention.
- the present invention relates to an improved core cutting apparatus that allows cutting of parts traditionally difficult or impossible to cut due to cutter limitations and/or physical machine head size.
- the annular cutter of the present invention is capable of machining core in an orientation that is parallel to the cutting surface, rather than perpendicular to the cutting surface as with prior art systems.
- a core cutting apparatus generally includes a cutting head 206 which is rigidly and coaxially secured (using any convenient method) to a spindle 202 .
- Spindle 202 during normal operation, spins at an appropriate rate, and may be attached to a variety of manipulators, controllers, computers, and the like. In one embodiment, for example, spindle 202 is coupled to a five-axis manipulator of the type well known in the art.
- Cutting head 206 includes a generally cylindrical sidewall 208 having any convenient length and diameter, depending upon the cutting application. Cutting head 206 is thus generally ring-shaped, or “annular.” One end of sidewall 208 has a cutting edge 220 , which is serrated, saw-tooth-shaped, or has any suitable texture or geometry capable of cutting a core-type material.
- core or “core-type” material refers to a material that has an internal, often regular geometric structure, rather than a homogeneous, contiguous structure. Such structures include, for example, honeycomb-shaped structures and the like. Materials such as Kevlar, steel, aluminum, or any other plastic, metal, or ceramic may be used.
- Cutting head 206 is suitably attached to spindle 202 either removeably or permanently, through any suitable hardware arrangement (e.g., using a chuck and shank configuration, etc.). Spindle 202 and cutting head 206 thus together rotate (either in one direction or both directions) with respect to a rotational axis 204 .
- the speed of rotation will vary depending upon the application, but in various embodiments ranges upwards of 10,000 to 15,000 RPM.
- Sidewall 208 further includes one or more openings 210 (or “flutes”) that extend through the thickness of the sidewall. These openings function, in part, to allow cut-away material (or “offal”) to be removed from cutting head 206 during operation. There may be any number of such openings, depending upon the application, and the openings may have any convenient shape. In the illustrated embodiment, for example, a total of four generally spiral-shaped openings are distributed uniformly around the surface of sidewall 208 . In this embodiment, slightly less than half of the cylindrical surface area of sidewall 208 is taken up by openings 210 ; however, the present invention is not so limited, and comprehends any number of openings having any suitable shape, size, and distribution.
- openings 210 have sharpened or chamfered edges.
- region 212 within each opening 210 is sharpened.
- edges may include any suitable structure, including saw-teeth, serrations, etc.
- a generally conical member 230 is coupled to spindle 202 and/or cutting head 206 adjacent to the end opposite cutting edge 220 (e.g., region 232 ).
- Conical member 230 preferably acts to break up cut-away material prior to it being ejected through openings 210 .
- conical member 230 may comprise, for example, a silicon-carbide grinding surface, such as a surface with screw-like serrations.
- Conical member 230 need not be actually conical in shape: it may have any curvilinear or rectilinear shape capable of assisting with radial movement of offal through the interior of cutting head 206 during operation.
- cutting head 206 may be manufactured using any suitable material or combination of materials.
- sidewall 208 and conical member 230 are fabricated from a high-speed steel and/or silicon-carbide material.
- a workpiece 102 has a surface 103 which, as described early with respect to FIG. 1 , cannot easily be cut using traditional disk cutters.
- a cutting head 206 in according with the present invention moves downward along a cutting direction 112 that is actually substantially parallel to (minus a small lead angle) the rotational axis 204 .
- openings 210 in the embodiment shown in FIG. 3 is somewhat different from that shown in FIG. 2 . That is, simple rectangular openings 210 with sharpened edges on both sides of the opening are used.
- the system is able to make plunge cuts (i.e., cuts consisting of simple downward motion), but is also capable of fabricating fine edge geometries using a proper manipulator path.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Processing Of Stones Or Stones Resemblance Materials (AREA)
- Drilling Tools (AREA)
Abstract
Description
- The present invention generally relates to machining technology and, more particularly, to automated core machining of materials such as foam and honeycomb-core materials.
- When performing automated machining of certain materials, such as foam and honeycomb-core materials (generally referred to as “core” materials), certain geometries may be encountered that are difficult or impossible to produce using standard circular disk cutters. That is, the head of such cutters are prone to impacting the core and inadvertently damaging or destroying the workpiece.
- Conventional core machining is done with the cutter positioned at 90 degrees to the workpiece, and this angular relationship is maintained throughout the machining operation. Referring to
FIG. 1 , for example, aworkpiece 102 is machined using acutting head 104 including acutting disk 106 attached to a rotatingspindle 105, whereinspindle 105 has arotational axis 110, and wherein thecutting direction 112 ofcutting head 104 is substantially perpendicular (within a small lead angle θ) torotational axis 110. Stated another way,rotational axis 110 ofspindle 105 is maintained, during a cutting operation, substantially normal to the plane of thework surface 103. In this illustration, “combing” or “trailing” cutting paths are exclusively used for carving of the core. Complex geometry cannot be reached in this fashion. Furthermore, the sidewalls of workpiece 102 (e.g., surface 113) cannot be cut without rotatingspindle 105 by approximately 90 degrees. - Accordingly, it is desirable to provide improved core machining tools and methods. Furthermore, other desirable features and characteristics of the present invention will become apparent from the subsequent detailed description and the appended claims, taken in conjunction with the accompanying drawings and the foregoing technical field and background.
- The present invention generally relates to an annular core cutting apparatus capable of machining core workpieces along an orientation parallel to the cutting surface. In accordance with one embodiment, for example, a core cutting apparatus includes a cutting head including a generally cylindrical sidewall having a first end and a second end, wherein the first end has a cutting edge, and wherein the sidewall includes a plurality of openings having at least one sharpened edge. A spindle is coaxially and rigidly coupled to the second end of the cylindrical sidewall, and the spindle configured to rotate about a rotational axis. In a further embodiment, a generally conical member is disposed within the cutting apparatus to assist with grinding and removal of waste material.
- The present invention will hereinafter be described in conjunction with the following drawing figures, wherein like numerals denote like elements, and
-
FIG. 1 is an overview of a typical prior art circular disk cutting operation; -
FIG. 2 is a core carving apparatus in accordance with one embodiment of the present invention; and -
FIG. 3 is an overview of a core carving operation in accordance with the present invention. - The following detailed description is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. Furthermore, there is no intention to be bound by any expressed or implied theory presented in the preceding technical field, background, brief summary or the following detailed description. For the sake of brevity, conventional techniques related to computer-aided manufacturing (CAM), machining, and other conventional tools and techniques may not be described in detail herein.
- In general, the present invention relates to an improved core cutting apparatus that allows cutting of parts traditionally difficult or impossible to cut due to cutter limitations and/or physical machine head size. The annular cutter of the present invention is capable of machining core in an orientation that is parallel to the cutting surface, rather than perpendicular to the cutting surface as with prior art systems.
- Referring to
FIG. 1 , a core cutting apparatus generally includes acutting head 206 which is rigidly and coaxially secured (using any convenient method) to aspindle 202. Spindle 202, during normal operation, spins at an appropriate rate, and may be attached to a variety of manipulators, controllers, computers, and the like. In one embodiment, for example,spindle 202 is coupled to a five-axis manipulator of the type well known in the art. -
Cutting head 206 includes a generallycylindrical sidewall 208 having any convenient length and diameter, depending upon the cutting application. Cuttinghead 206 is thus generally ring-shaped, or “annular.” One end ofsidewall 208 has acutting edge 220, which is serrated, saw-tooth-shaped, or has any suitable texture or geometry capable of cutting a core-type material. In this regard, the term “core” or “core-type” material refers to a material that has an internal, often regular geometric structure, rather than a homogeneous, contiguous structure. Such structures include, for example, honeycomb-shaped structures and the like. Materials such as Kevlar, steel, aluminum, or any other plastic, metal, or ceramic may be used. - Cutting
head 206 is suitably attached tospindle 202 either removeably or permanently, through any suitable hardware arrangement (e.g., using a chuck and shank configuration, etc.).Spindle 202 and cuttinghead 206 thus together rotate (either in one direction or both directions) with respect to arotational axis 204. The speed of rotation will vary depending upon the application, but in various embodiments ranges upwards of 10,000 to 15,000 RPM. -
Sidewall 208 further includes one or more openings 210 (or “flutes”) that extend through the thickness of the sidewall. These openings function, in part, to allow cut-away material (or “offal”) to be removed from cuttinghead 206 during operation. There may be any number of such openings, depending upon the application, and the openings may have any convenient shape. In the illustrated embodiment, for example, a total of four generally spiral-shaped openings are distributed uniformly around the surface ofsidewall 208. In this embodiment, slightly less than half of the cylindrical surface area ofsidewall 208 is taken up byopenings 210; however, the present invention is not so limited, and comprehends any number of openings having any suitable shape, size, and distribution. - In one embodiment, all or a portion of
openings 210 have sharpened or chamfered edges. For example, inFIG. 2 ,region 212 within eachopening 210 is sharpened. Such an embodiment is useful when the tool is designed to rotate in a single direction (in this case, clockwise as viewed downspindle 202 to cutting head 206). These edges may include any suitable structure, including saw-teeth, serrations, etc. - In a further embodiment, a generally
conical member 230 is coupled tospindle 202 and/or cuttinghead 206 adjacent to the end opposite cutting edge 220 (e.g., region 232).Conical member 230 preferably acts to break up cut-away material prior to it being ejected throughopenings 210. In this regard,conical member 230 may comprise, for example, a silicon-carbide grinding surface, such as a surface with screw-like serrations.Conical member 230 need not be actually conical in shape: it may have any curvilinear or rectilinear shape capable of assisting with radial movement of offal through the interior of cuttinghead 206 during operation. - The various subcomponents of
cutting head 206 may be manufactured using any suitable material or combination of materials. In one embodiment, for example,sidewall 208 andconical member 230 are fabricated from a high-speed steel and/or silicon-carbide material. - Having thus given a description of a cutting apparatus of the present invention, it can be seen that this arrangement provides certain advantages when machining core materials. Referring to
FIG. 3 , for example, aworkpiece 102 has asurface 103 which, as described early with respect toFIG. 1 , cannot easily be cut using traditional disk cutters. - As shown, however, a
cutting head 206 in according with the present invention moves downward along acutting direction 112 that is actually substantially parallel to (minus a small lead angle) therotational axis 204. It will be noted that the size and shape ofopenings 210 in the embodiment shown inFIG. 3 is somewhat different from that shown inFIG. 2 . That is, simplerectangular openings 210 with sharpened edges on both sides of the opening are used. As illustrated, the system is able to make plunge cuts (i.e., cuts consisting of simple downward motion), but is also capable of fabricating fine edge geometries using a proper manipulator path. - It should also be appreciated that the illustrated embodiments are only examples, and are not intended to limit the scope, applicability, or configuration of the invention in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing the exemplary embodiment or exemplary embodiments. It should be understood that various changes can be made in the function and arrangement of elements without departing from the scope of the invention as set forth in the appended claims and the legal equivalents thereof.
Claims (17)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/464,082 US7337523B1 (en) | 2006-08-11 | 2006-08-11 | Methods and apparatus for an annular core cutter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/464,082 US7337523B1 (en) | 2006-08-11 | 2006-08-11 | Methods and apparatus for an annular core cutter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20080034565A1 true US20080034565A1 (en) | 2008-02-14 |
| US7337523B1 US7337523B1 (en) | 2008-03-04 |
Family
ID=39049097
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/464,082 Active US7337523B1 (en) | 2006-08-11 | 2006-08-11 | Methods and apparatus for an annular core cutter |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US7337523B1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105710424A (en) * | 2016-04-06 | 2016-06-29 | 哈尔滨飞机工业集团有限责任公司 | Numerical control machining method of flight simulation ice-type foam block |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102554327A (en) * | 2012-01-05 | 2012-07-11 | 哈尔滨飞机工业集团有限责任公司 | Disk honeycomb milling cutter capable of discharging chips |
| CN110653408B (en) * | 2019-10-08 | 2020-10-09 | 山东大学 | An internal suction milling tool for honeycomb and composite material processing |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2680898A (en) * | 1950-11-27 | 1954-06-15 | Frank Diosi | Cutting tool |
| US2894583A (en) * | 1958-09-15 | 1959-07-14 | Onsrud Cutter Mfg Company | Honeycomb cutter |
| US3264128A (en) * | 1961-12-13 | 1966-08-02 | Argueso & Co Inc M | Composition for preparing thin-walled cored objects preparatory to performing machining operations thereon |
| US3765789A (en) * | 1971-12-29 | 1973-10-16 | Hougen Everett | Annular hole cutter |
| US4586857A (en) * | 1983-12-17 | 1986-05-06 | Omi Kogyo Co., Ltd. | Hole cutter |
| US4677886A (en) * | 1985-12-12 | 1987-07-07 | Northrop Corporation | Honeycomb cutter and chip breaker/chaf remover |
| US4794836A (en) * | 1987-07-17 | 1989-01-03 | Lockheed Corporation | Honeycomb core cutting tool |
| US4907920A (en) * | 1989-01-18 | 1990-03-13 | The Boeing Company | Milling cutter for honeycomb core material |
| US5015128A (en) * | 1990-03-26 | 1991-05-14 | Ross Jr Donald C | Rotary drill apparatus |
| US5221163A (en) * | 1988-10-31 | 1993-06-22 | Gn Tool Co., Ltd. | Nicked cutting tool |
| US5253961A (en) * | 1989-04-05 | 1993-10-19 | Geissler & Kuper Gesellschaft Mit Beschrankter Haftung Diamantwerkzeuge Maschinen | Coupling for drilling machine with dust extractor |
| US6588992B2 (en) * | 2001-02-06 | 2003-07-08 | Black & Decker Inc. | Hole saw |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3831046A1 (en) * | 1988-09-12 | 1990-03-15 | Felix Leeb | Hollow milling cutter for producing circular recesses of infinitely variable diameter |
-
2006
- 2006-08-11 US US11/464,082 patent/US7337523B1/en active Active
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2680898A (en) * | 1950-11-27 | 1954-06-15 | Frank Diosi | Cutting tool |
| US2894583A (en) * | 1958-09-15 | 1959-07-14 | Onsrud Cutter Mfg Company | Honeycomb cutter |
| US3264128A (en) * | 1961-12-13 | 1966-08-02 | Argueso & Co Inc M | Composition for preparing thin-walled cored objects preparatory to performing machining operations thereon |
| US3765789A (en) * | 1971-12-29 | 1973-10-16 | Hougen Everett | Annular hole cutter |
| US4586857A (en) * | 1983-12-17 | 1986-05-06 | Omi Kogyo Co., Ltd. | Hole cutter |
| US4677886A (en) * | 1985-12-12 | 1987-07-07 | Northrop Corporation | Honeycomb cutter and chip breaker/chaf remover |
| US4794836A (en) * | 1987-07-17 | 1989-01-03 | Lockheed Corporation | Honeycomb core cutting tool |
| US5221163A (en) * | 1988-10-31 | 1993-06-22 | Gn Tool Co., Ltd. | Nicked cutting tool |
| US4907920A (en) * | 1989-01-18 | 1990-03-13 | The Boeing Company | Milling cutter for honeycomb core material |
| US5253961A (en) * | 1989-04-05 | 1993-10-19 | Geissler & Kuper Gesellschaft Mit Beschrankter Haftung Diamantwerkzeuge Maschinen | Coupling for drilling machine with dust extractor |
| US5015128A (en) * | 1990-03-26 | 1991-05-14 | Ross Jr Donald C | Rotary drill apparatus |
| US6588992B2 (en) * | 2001-02-06 | 2003-07-08 | Black & Decker Inc. | Hole saw |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105710424A (en) * | 2016-04-06 | 2016-06-29 | 哈尔滨飞机工业集团有限责任公司 | Numerical control machining method of flight simulation ice-type foam block |
Also Published As
| Publication number | Publication date |
|---|---|
| US7337523B1 (en) | 2008-03-04 |
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