WO2012147823A1 - 複合材部品の締結方法 - Google Patents
複合材部品の締結方法 Download PDFInfo
- Publication number
- WO2012147823A1 WO2012147823A1 PCT/JP2012/061150 JP2012061150W WO2012147823A1 WO 2012147823 A1 WO2012147823 A1 WO 2012147823A1 JP 2012061150 W JP2012061150 W JP 2012061150W WO 2012147823 A1 WO2012147823 A1 WO 2012147823A1
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- WO
- WIPO (PCT)
- Prior art keywords
- fastening
- smoothness
- fastened
- countersink
- countersink depth
- Prior art date
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- 238000000034 method Methods 0.000 title claims abstract description 57
- 239000002131 composite material Substances 0.000 title claims abstract description 31
- 238000005553 drilling Methods 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 239000002184 metal Substances 0.000 description 2
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 239000011151 fibre-reinforced plastic Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J15/00—Riveting
- B21J15/10—Riveting machines
- B21J15/14—Riveting machines specially adapted for riveting specific articles, e.g. brake lining machines
- B21J15/142—Aerospace structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J15/00—Riveting
- B21J15/10—Riveting machines
- B21J15/14—Riveting machines specially adapted for riveting specific articles, e.g. brake lining machines
- B21J15/147—Composite articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
- B29C66/21—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
-
- 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
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49764—Method of mechanical manufacture with testing or indicating
Definitions
- the present invention relates to a fastening method for fastening composite parts using fastening parts (fasteners) such as bolts and rivets.
- Patent Document 1 Japanese Patent Laid-Open No. 2007-2033057 discloses a striking device for joining objects to be joined.
- the striking device adjusts the amount of pushing for immersing the rivet into the workpiece based on the thickness of the workpiece. As a result, the surface of the rivet and the surface of the object to be joined are flush with each other.
- FIG. 1 shows a fastened object 300 fastened by a fastening part 420 and a nut 440.
- the fastening component 420 includes a countersunk bolt.
- the fastened object 300 includes parts 351 and 352 that are stacked.
- the fastened object 300 is formed with a countersunk hole 300a penetrating from one surface 300b of the fastened object 300 to the other surface 300c.
- the countersink portion of the countersunk hole 300a is disposed on the surface 300b side.
- the method of fastening the article to be fastened 300 includes disposing the fastening part 420 in the countersunk hole 300a and attaching the nut 440 to the fastening part 420.
- the smoothness B 300 as the axial distance of the countersunk hole 300a from the surface 300b to the head upper surface 421a of the fastening component 420 is managed within a predetermined range.
- the smoothness B 300 represents the sinking or protrusion of the head upper surface 421a from the surface 300b.
- the inventor has recognized as follows.
- the composite material has a larger crush when subjected to compressive force than metal. Therefore, when the parts 351 and 352 are composite parts, even if the thickness of the fastened object 300 before the nut 440 is tightened is measured, it is difficult to manage the smoothness B 300 based only on the thickness.
- fastening a composite material to be fastened using rivets it is difficult to manage the smoothness of the rivet based on only the thickness of the fastened material before fastening for the same reason.
- an object of the present invention is to provide a fastening method in which the smoothness of fastening parts for fastening composite parts can be easily managed.
- the fastening method of the composite material component by the 1st viewpoint of this invention is the 1st fastening component arrange
- the first fastening object is fastened using the first fastening part, and the first fastening object is fastened. And further measuring a second smoothness of the first fastening part. In determining the second countersink depth, the second countersink depth is determined based on the first smoothness and the second smoothness.
- the fastening method is based on measuring the thickness of the second fastened object at a portion where the second countersunk hole is to be formed, and on the second countersink depth and the thickness. And selecting the second fastening part.
- the second countersink depth is determined using a countersink depth arithmetic expression.
- the fastening method includes measuring the second smoothness of the second fastening part of the second fastening part disposed in the second countersunk hole before fastening the second fastened object; Measuring a second fastening part second smoothness of the second fastening part disposed in the second countersunk hole after fastening the second fastened object; and Updating the countersink depth calculation formula based on 1 smoothness, the second fastening component second smoothness, and the second countersink depth, and based on the updated countersink depth calculation formula Determining a third countersink depth, forming a third countersink hole with a third countersink depth in a third article to be fastened as a plurality of stacked composite parts, Fastening the third fastened object using a third fastening part disposed in the third countersunk hole.
- the first fastening part includes a first countersunk bolt.
- the second fastening component includes a second countersunk bolt.
- Fastening the second fastened object includes attaching a nut to the second countersunk bolt.
- FIG. 1 is a cross-sectional view of a part fastened with a fastening part.
- FIG. 2 is a conceptual diagram for explaining database construction in the fastening method according to the first embodiment of the present invention.
- FIG. 3 is a cross-sectional view of an object to be fastened for explaining a process of measuring the thickness of the fastened object in the fastening method according to the first embodiment.
- FIG. 4 is a cross-sectional view of an object to be fastened for explaining a step of forming a countersink in the fastening method according to the first embodiment.
- FIG. 1 is a cross-sectional view of a part fastened with a fastening part.
- FIG. 2 is a conceptual diagram for explaining database construction in the fastening method according to the first embodiment of the present invention.
- FIG. 3 is a cross-sectional view of an object to be fastened for explaining a process of measuring the thickness of the fastened object in the fastening method according to the first embodiment.
- FIG. 4
- FIG. 5 shows a fastening part for fastening a fastened object in the fastening method according to the first embodiment.
- FIG. 6 is a cross-sectional view of an object to be fastened in which fastening parts are arranged in the fastening method according to the first embodiment.
- FIG. 7 shows a combined body as a result in the fastening method according to the first embodiment.
- FIG. 8 is a conceptual diagram for explaining a step of obtaining a countersink depth calculation formula in the fastening method according to the first embodiment.
- FIG. 9 is a conceptual diagram for explaining a method of fastening an object to be fastened using a countersink depth calculation formula in the fastening method according to the first embodiment.
- FIG. 10 is a conceptual diagram for explaining a method for fastening an object to be fastened using a grip length determination table in the fastening method according to the second embodiment of the present invention.
- the fastening method which concerns on the 1st Embodiment of this invention is demonstrated.
- the combined body 200 is manufactured from the workpiece 100 as a fastened object through a drilling step, a fastening part arranging step, and a fastening step.
- a drilling step a plurality of countersunk holes are formed in the workpiece 100.
- a fastening component arranging step a plurality of fastening components are arranged in the plurality of countersunk holes.
- the workpiece 100 is fastened by attaching a plurality of nuts to the plurality of fastening parts, respectively.
- the Nth hole as one of the plurality of countersunk holes will be described, the same applies to the other holes.
- the thickness t and the countersink depth d are measured.
- the smoothness A is measured.
- the smoothness B is measured.
- the thickness t is the thickness of the workpiece 100 at a portion where a countersunk hole 100a to be described later is to be formed.
- the workpiece 100 includes a plurality of superimposed composite parts 51 and 52.
- the thickness measuring device 15 is brought into contact with the surface 100b on one side and the surface 100c on the other side of the workpiece 100, and the thickness t is measured.
- the thickness t is measured before the countersunk hole 100a is formed in the workpiece 100.
- countersunk hole 100 a that penetrates workpiece 100 from surface 100 b to surface 100 c is formed.
- the countersunk hole 100 a is the Nth hole among the plurality of countersunk holes formed in the workpiece 100.
- the countersink portion of the countersunk hole 100a is disposed on the surface 100b side.
- the countersink depth d of the countersunk hole 100a is detected.
- the countersink depth d may be detected based on the actual feed amount of the countersink forming tool 16, or the countersink depth d may be formed based on the command value of the feed amount of the countersink forming tool 16.
- the countersink depth d may be detected by another method after the countersunk hole 100a is formed.
- the fastening component (fastener) 25 used for fastening the workpiece 100 includes a countersunk bolt 20 and a sleeve 40.
- the countersunk bolt 20 includes a head portion 21, a cylindrical portion 22, and a screw portion 23.
- the head 21 has a head upper surface 21a.
- the cylindrical portion 22 is disposed between the head portion 21 and the screw portion 23.
- a screw is not formed on the cylindrical portion 22.
- the sleeve 40 covers the cylindrical portion 22.
- the axial distance of the fastening component 25 between the end portion 40a of the sleeve 40 near the head 21 and the end portion 22a of the cylindrical portion 22 near the screw portion 23 is the grip length L of the fastening component 25. It is called.
- the fastening part 25 is inserted into the countersunk hole 100a, and the fastening part 25 is driven using an air hammer or the like to place the fastening part 25 in the countersunk hole 100a.
- the fastening component 25 is disposed in the countersunk hole 100a
- the head 21 is disposed in the countersunk hole portion of the countersunk hole 100a
- the screw portion 23 protrudes from the surface 100c.
- the smoothness A and the protrusion amount P are measured.
- the smoothness A is a distance in the axial direction of the countersunk hole 100a from the surface 100b to the head upper surface 21a.
- the smoothness A represents sinking or protrusion from the surface 100b of the head upper surface 21a.
- the protrusion amount P is the distance in the axial direction of the countersunk hole 100a from the surface 100c to the end 22a of the cylindrical portion 22.
- the protruding amount P is within a predetermined range.
- the fastening component 25 is removed, and another fastening component 25 having a grip length L different from the removed fastening component 25 is disposed in the countersunk hole 100a.
- the nut 30 is attached to the screw portion 23 and the composite parts 51 and 52 are fastened to manufacture the combined body 200.
- the smoothness B is measured.
- the smoothness B is the axial distance of the countersunk hole 100a from the surface 100b to the head upper surface 21a.
- the smoothness B represents the sinking or protrusion from the surface 100b of the head upper surface 21a. It is necessary to manage the smoothness B within a predetermined range.
- the composite parts 51 and 52 are tightened and crushed by attaching the nut 30 to the fastening part 25. As a result, the head upper surface 21a is drawn toward the back of the countersunk hole 100a.
- the difference (BA) between the smoothness B and the smoothness A is defined as the pull-in amount ⁇ t of the fastening part 25.
- each of workpieces 101 to 110 is workpiece 100.
- Each of the combined bodies 201 to 210 is a combined body 200.
- the bonded bodies 201 to 210 are manufactured from the workpieces 101 to 110 through a drilling process, a fastening part arranging process, and a fastening process.
- the database 11 stored in the computer 10 is constructed.
- the thickness t of the first N-holes of the workpiece 101, countersink depth d, the thickness t 1 of the smoothness A, and smoothness B, countersink depth d 1, smoothness A 1, and smoothness B 1 Measure each.
- the thicknesses t 2 to t 10 , countersink depths d 2 to d 10 , smoothness A 2 to A 10 , and smoothness B 2 to B 10 are measured for the workpieces 102 to 110.
- the database 11 is constructed to include the thickness t 1 to t 10 , countersink depths d 1 to d 10 , smoothness A 1 to A 10 , and smoothness B 1 to B 10 for the Nth hole. .
- data is managed for each hole.
- a countersink depth arithmetic expression 13 for the Nth hole is determined based on the database 11 and the drawing data 12 of the combined body 200.
- the drawing data 12 is data for designating dimensions and the like of the combined body 200.
- the countersink depth calculation formula 13 is determined based on the countersink depths d 1 to d 10 , the smoothness A 1 to A 10 , and the smoothness B 1 to B 10 .
- the countersink depth calculation formula 13 calculates the countersink depth d of the subsequent work 100 (work to be fastened later) from the smoothness A and B for the previous work 100 (work fastened first). This is an equation for determining the smoothness B of the workpiece 100 to be within a predetermined range.
- Each of the workpieces 111 to 121 is a workpiece 100.
- Each of the combined bodies 211 to 221 is a combined body 200.
- the workpieces 211 to 221 are manufactured from the workpieces 111 to 121 through a drilling process, a fastening part arranging process, and a fastening process.
- a method of manufacturing the joined bodies 211 to 221 from the workpieces 111 to 121 using the countersink depth calculation formula 13 is the same as the method described with reference to FIGS. 2 to 7 except for the following description. .
- the computer 10 determines the countersink depth d 11 from the smoothness A 10 and B 10 using the countersink depth calculation formula 13 and outputs the countersink depth d 11 to be used in the drilling process of the workpiece 111. To do. In the drilling process of the work 111, forming a countersunk hole 100a of the countersink depth d 11. The thickness t 11 , countersink depth d 11 , smoothness A 11 , and smoothness B 11 for the workpiece 111 are measured and added to the database 11.
- the countersink depths d 12 to d 21 are determined from the smoothness A and B for the previous workpiece using the countersink depth calculation formula 13, A countersunk hole 100a having a countersink depth of d 12 to d 21 is formed. Further, the thicknesses t 12 to t 21 , countersink depths d 12 to d 21 , smoothness A 12 to A 21 , and smoothness B 12 to B 21 for the workpieces 112 to 221 are measured and added to the database 11. To do.
- the smoothness B of the subsequent workpiece 100 is set to a predetermined range. Easy to manage.
- the average value of the smoothness A 11 ⁇ mean and smoothness B 11 ⁇ B 20 of A 20 of workpiece 121 countersink it may determine the depth d 21.
- the smoothness A and B of the workpiece 100 is prevented from greatly affecting the determination of the countersink depth d for the subsequent workpiece 100.
- the countersink depth arithmetic expression 13 is determined so that the countersink depth d can be determined only from the smoothness A. It is preferable to determine the countersink depth d for the subsequent workpiece 100 from the smoothness A for the previous workpiece 100 using the depth calculation formula 13. By doing in this way, the drilling process about the subsequent workpiece
- the fastening method according to the second embodiment of the present invention is the same as the fastening method according to the first embodiment except for the following description.
- the grip length determination table 14 determines the grip length L of the fastening component 25 used for fastening the workpiece 100 from the thickness t and countersink depth d of the workpiece 100 and the protrusion amount P for the workpiece 100 is predetermined. It is a table for determining so that it may become in the range.
- the computer 10 determines the grip length L from the thickness t 11 and the countersink depth d 11 using the grip length determination table 14 for use in the fastening part arrangement process of the workpiece 111.
- the fastening component 25 having the determined grip length L is selected, and the selected fastening component is arranged in the countersunk hole 100a of the workpiece 111.
- the fastening component 25 to be placed in the countersunk hole 100a of the workpieces 112 to 121 is selected.
- the protrusion amount P can be reliably within a predetermined range. Therefore, the operation
- the data obtained after the determination of the countersink depth calculation formula 13 (for example, countersink depths d 11 to d 15 for the workpieces 111 to 115, degrees a 11 ⁇ a 15 updates the countersink depth calculation equation 13 based on, and smoothness B 11 ⁇ B 15), the countersink depth of the workpiece 121 with a countersink depth calculation equation 13 the updated d 21 may be determined. In this way, the latest data can be reflected in the countersink depth calculation formula 13.
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Abstract
Description
図2を参照して、本発明の第1の実施形態に係る締結方法を説明する。本実施形態に係る締結方法において、被締結物としてのワーク100から、穴あけ工程、締結部品配置工程、及び締結工程を経て、結合体200が製造される。穴あけ工程において、ワーク100に複数の皿穴付き孔が形成される。締結部品配置工程において、複数の皿穴付き孔にそれぞれ複数の締結部品が配置される。締結工程において、複数の締結部品にそれぞれ複数のナットが装着されてワーク100が締結される。以下、複数の皿穴付き孔の一つとしての第N孔について説明するが、他の孔についても同様である。
本発明の第2の実施形態に係る締結方法は、以下の説明を除いて第1の実施形態に係る締結方法と同じである。
Claims (5)
- 重ねられた複数の複合材部品としての第1被締結物に形成された第1皿穴付き孔に配置された第1締結部品の第1平滑度を測定することと、
前記第1平滑度に基づいて第2皿穴深さを決定することと、
重ねられた複数の複合材部品としての第2被締結物に前記第2皿穴深さの第2皿穴付き孔を形成することと、
前記第2皿穴付き孔に配置される第2締結部品を用いて前記第2被締結物を締結することと
を具備する
複合材部品の締結方法。 - 請求項1に記載の複合材部品の締結方法であって、
前記第1平滑度を測定することの後に、前記第1締結部品を用いて前記第1被締結物を締結することと、
前記第1被締結物を締結することの後に、前記第1締結部品の第2平滑度を測定することと
を更に具備し、
前記第2皿穴深さを決定することにおいて、前記第1平滑度及び前記第2平滑度に基づいて前記第2皿孔深さを決定する
複合材部品の締結方法。 - 請求項1又は2に記載の複合材部品の締結方法であって、
前記第2皿穴付き孔が形成されるべき部位における前記第2被締結物の厚さを測定することと、
前記第2皿穴深さ及び前記厚さに基づいて前記第2締結部品を選択することと
を更に具備する
複合材部品の締結方法。 - 請求項1乃至3のいずれかに記載の複合材部品の締結方法であって、
前記第2皿穴深さを決定することにおいて、皿穴深さ演算式を用いて前記第2皿穴深さを決定し、
前記第2被締結物を締結することの前に、前記第2皿穴付き孔に配置された前記第2締結部品の第2締結部品第1平滑度を測定することと、
前記第2被締結物を締結することの後に、前記第2皿穴付き孔に配置された前記第2締結部品の第2締結部品第2平滑度を測定することと、
前記第2締結部品第1平滑度、前記第2締結部品第2平滑度、及び前記第2皿穴深さに基づいて前記皿穴深さ演算式を更新することと、
更新された前記皿穴深さ演算式に基づいて第3皿穴深さを決定することと、
重ねられた複数の複合材部品としての第3被締結物に前記第3皿穴深さの第3皿穴付き孔を形成することと、
前記第3皿穴付き孔に配置される第3締結部品を用いて前記第3被締結物を締結することと
を更に具備する
複合材部品の締結方法。 - 請求項1乃至4のいずれかに記載の複合材部品の締結方法であって、
前記第1締結部品は第1皿ボルトを備え、
前記第2締結部品は第2皿ボルトを備え、
前記第2被締結物を締結することは、前記第2皿ボルトにナットを装着することを含む
複合材部品の締結方法。
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BR112013027587A BR112013027587B1 (pt) | 2011-04-28 | 2012-04-25 | método de fixação de partes de material compósito |
EP12777026.1A EP2703654B1 (en) | 2011-04-28 | 2012-04-25 | Method for fastening composite material component |
CA2833858A CA2833858C (en) | 2011-04-28 | 2012-04-25 | Fastening method of composite material parts |
US14/112,320 US9360031B2 (en) | 2011-04-28 | 2012-04-25 | Fastening method of composite material parts |
CN201280020246.4A CN103492729B (zh) | 2011-04-28 | 2012-04-25 | 复合材料部件的紧固方法 |
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JP2011100643A JP5675482B2 (ja) | 2011-04-28 | 2011-04-28 | 複合材部品の締結方法 |
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US (1) | US9360031B2 (ja) |
EP (1) | EP2703654B1 (ja) |
JP (1) | JP5675482B2 (ja) |
CN (1) | CN103492729B (ja) |
BR (1) | BR112013027587B1 (ja) |
CA (1) | CA2833858C (ja) |
WO (1) | WO2012147823A1 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10316695B2 (en) | 2015-12-10 | 2019-06-11 | General Electric Company | Metallic attachment system integrated into a composite structure |
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CN111941857B (zh) * | 2020-06-11 | 2021-12-31 | 德峰兴元(江苏)生物科技有限公司 | 一种新型木剑捶打装置 |
US11841697B2 (en) | 2020-10-07 | 2023-12-12 | The Boeing Company | Methods and systems for selecting and pre-feeding fasteners into automated drilling machines using repeatability rating |
Citations (4)
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JP2007203307A (ja) | 2006-01-30 | 2007-08-16 | Kawasaki Heavy Ind Ltd | 接合装置 |
JP2008075876A (ja) * | 2006-09-21 | 2008-04-03 | Alcoa Global Fasteners Inc | 複合材料用途のための高性能スリーブ付き干渉締結具 |
JP2009144914A (ja) * | 2007-11-06 | 2009-07-02 | Boeing Co:The | 複合構造の組立て方法及び装置 |
JP2010537881A (ja) * | 2007-08-30 | 2010-12-09 | ザ・ボーイング・カンパニー | ファスナ取り付け前の落雷保護システムの高速点検 |
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US3748948A (en) * | 1970-08-05 | 1973-07-31 | Boeing Co | Fatigue resistant fasteners |
US4877138A (en) * | 1987-07-27 | 1989-10-31 | The Boeing Company | Fastener head elevation measuring apparatus |
US5673839A (en) * | 1995-11-29 | 1997-10-07 | The Boeing Company | Real-time fastener measurement system |
GB0525691D0 (en) | 2005-12-16 | 2006-01-25 | Airbus Uk Ltd | A fastener assembly |
ITTO20060581A1 (it) * | 2006-08-04 | 2008-02-05 | Bruno Bisiach | Dispositivo e metodo di lavorazione di un pezzo da lavorare, quale per esempio una struttura a guscio di un velivolo |
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2011
- 2011-04-28 JP JP2011100643A patent/JP5675482B2/ja active Active
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- 2012-04-25 EP EP12777026.1A patent/EP2703654B1/en not_active Not-in-force
- 2012-04-25 CN CN201280020246.4A patent/CN103492729B/zh not_active Expired - Fee Related
- 2012-04-25 US US14/112,320 patent/US9360031B2/en active Active
- 2012-04-25 WO PCT/JP2012/061150 patent/WO2012147823A1/ja active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007203307A (ja) | 2006-01-30 | 2007-08-16 | Kawasaki Heavy Ind Ltd | 接合装置 |
JP2008075876A (ja) * | 2006-09-21 | 2008-04-03 | Alcoa Global Fasteners Inc | 複合材料用途のための高性能スリーブ付き干渉締結具 |
JP2010537881A (ja) * | 2007-08-30 | 2010-12-09 | ザ・ボーイング・カンパニー | ファスナ取り付け前の落雷保護システムの高速点検 |
JP2009144914A (ja) * | 2007-11-06 | 2009-07-02 | Boeing Co:The | 複合構造の組立て方法及び装置 |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10316695B2 (en) | 2015-12-10 | 2019-06-11 | General Electric Company | Metallic attachment system integrated into a composite structure |
US11859509B2 (en) | 2015-12-10 | 2024-01-02 | General Electric Company | Metallic attachment system integrated into a composite structure |
Also Published As
Publication number | Publication date |
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BR112013027587A2 (pt) | 2017-02-14 |
CA2833858A1 (en) | 2012-11-01 |
EP2703654A1 (en) | 2014-03-05 |
CN103492729B (zh) | 2015-06-24 |
US9360031B2 (en) | 2016-06-07 |
EP2703654B1 (en) | 2018-10-17 |
JP5675482B2 (ja) | 2015-02-25 |
EP2703654A4 (en) | 2015-01-21 |
JP2012233500A (ja) | 2012-11-29 |
BR112013027587B1 (pt) | 2020-04-14 |
CN103492729A (zh) | 2014-01-01 |
CA2833858C (en) | 2016-08-23 |
US20140047689A1 (en) | 2014-02-20 |
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