WO2015041908A1 - Rivet - Google Patents
Rivet Download PDFInfo
- Publication number
- WO2015041908A1 WO2015041908A1 PCT/US2014/054995 US2014054995W WO2015041908A1 WO 2015041908 A1 WO2015041908 A1 WO 2015041908A1 US 2014054995 W US2014054995 W US 2014054995W WO 2015041908 A1 WO2015041908 A1 WO 2015041908A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- pin member
- lock ring
- rivet
- panel
- lock
- Prior art date
Links
- 239000011324 bead Substances 0.000 claims abstract description 8
- 230000007704 transition Effects 0.000 claims description 4
- 238000009434 installation Methods 0.000 description 6
- 229910001069 Ti alloy Inorganic materials 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000792 Monel Inorganic materials 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 229910000883 Ti6Al4V Inorganic materials 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000036316 preload Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
Classifications
-
- 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
- B21J15/02—Riveting procedures
- B21J15/022—Setting rivets by means of swaged-on locking collars, e.g. lockbolts
-
- 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
- F16B19/00—Bolts without screw-thread; Pins, including deformable elements; Rivets
- F16B19/04—Rivets; Spigots or the like fastened by riveting
- F16B19/05—Bolts fastening by swaged-on collars
-
- 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
- F16B19/00—Bolts without screw-thread; Pins, including deformable elements; Rivets
- F16B19/04—Rivets; Spigots or the like fastened by riveting
- F16B19/08—Hollow rivets; Multi-part rivets
- F16B19/10—Hollow rivets; Multi-part rivets fastened by expanding mechanically
- F16B19/1027—Multi-part rivets
- F16B19/1036—Blind rivets
- F16B19/1045—Blind rivets fastened by a pull - mandrel or the like
- F16B19/1054—Blind rivets fastened by a pull - mandrel or the like the pull-mandrel or the like being frangible
Definitions
- the present invention relates to a fastener and, more particularly, a rivet for securing a plurality of work pieces together.
- Rivets are used to fasten a plurality of work pieces to one another.
- trailing edge areas of control surfaces such as ailerons, flaps, elevators, and rudders, are fastened with small, semi-tubular solid rivets.
- a rivet in an embodiment, includes a pin member including an elongated shank having a first end, a second end opposite the first end, a lock groove located proximate to the first end, a frangible portion, and a break neck groove located intermediate the lock groove and the frangible portion, and a head located at the first end; and a lock ring having a first end, a second end opposite the first end of the lock ring, an aperture extending from the first end of the lock ring to the second end of the lock ring, an outer surface extending from the first end of the lock ring to the second end of the lock ring, and a flange located at the second end of the lock ring, wherein the lock ring is installed on the pin member proximate to the first end of the pin member such that the flange of the lock ring is aligned with the lock groove of the pin member, wherein the lock ring is adapted to be secured to the pin member such that the flange of the lock ring is swaged
- the lock groove of the pin member is annular. In an embodiment, the lock groove has an hourglass shape. In an embodiment, the pin member includes a first smooth cylindrical portion and a second smooth cylindrical portion, and wherein the lock groove of the pin member is located intermediate the first smooth cylindrical portion and the second smooth cylindrical portion. In an embodiment, the frangible portion includes a pull portion having pull grooves. In an embodiment, the frangible portion includes a third smooth cylindrical portion, a fourth smooth cylindrical portion, and a transition portion intermediate the third and fourth smooth cylindrical portions.
- the rivet is adapted to be installed within a structure, wherein the structure includes a first panel having an outer surface, an inner surface, and a first hole extending from the outer surface of the first panel to the inner surface of the first panel, and a second panel juxtaposed with the first panel and having an outer surface, an inner surface, and a second hole extending from the outer surface of the second panel to the inner surface of the second panel and aligned with the first hole, wherein the rivet is adapted to be installed within the first and second holes in an installed position, and wherein when the rivet is in its installed position, a surface of the head of the pin member is flush with the outer surface of the second panel and the portion of the outer surface of the lock ring is flush with the outer surface of the first panel.
- the frangible portion of the pin member when the rivet is in its installed position, the frangible portion of the pin member is broken off from the pin member at the breakneck groove, forming an exposed surface on the second smooth cylindrical portion, and wherein the exposed surface is aligned with the outer surface of the first panel.
- the head of the pin member is a countersink head
- the second hole is a countersink hole.
- FIG. 1 is a perspective view of a rivet in accordance with an embodiment, with a lock ring employed by the rivet shown in cross-section, and the rivet being positioned within a structure;
- FIG. 2 is a side elevational view of a pin member employed by the rivet shown in
- FIG. 1 is a diagrammatic representation of FIG. 1 ;
- FIG. 3 is a perspective view of the lock ring employed by the rivet shown in FIG.
- FIG. 4 is a side elevational view of the pin member and lock ring shown in FIGS. 2 and 3, respectively, and which are engaged with one another prior to swaging of the lock ring to the pin member;
- FIG. 5 is a side elevational view of the pin member and lock ring shown in FIG. 4 with the lock ring swaged onto the pin member;
- FIG. 6 is a side elevational view of the rivet shown in FIG. 1 and being engaged by a fastener installation tool;
- FIG. 7 is a side elevational view of the rivet shown in FIG. 6 with the lock ring being further swaged by the fastener installation tool;
- FIG. 8 is a bottom perspective view of the rivet shown in FIG. 7 within its installed position
- FIG. 9 is a top perspective view of the rivet shown in FIG. 8;
- FIG. 10 is a side elevational view of a rivet in accordance with another embodiment, with a lock ring employed by the rivet shown in cross-section;
- FIG. 11 is a side elevational view of the rivet shown in FIG. 10 positioned within a structure, with the lock ring being swaged by a fastener installation tool.
- FIG. 1 illustrates an embodiment of a rivet 10.
- the rivet 10 includes a pin member 12 and a lock ring 14 that is sized and shaped to engage the pin member 12.
- the pin member 12 includes an elongated shank 16 having a first end 18, a second end 20 opposite the first end 18, a first smooth cylindrical portion 22 located proximate to the first end 18, a second smooth cylindrical portion 24 located intermediate the first and second ends 18 20, and an annular lock groove 26 intermediate the first smooth cylindrical portion 22 and the second smooth cylindrical portion 24.
- the lock groove 26 has an hourglass shape. In other embodiments, the lock groove 26 can consist of other shapes and sizes.
- a diameter of the lock groove 26 is smaller than a diameter of the first smooth cylindrical portion 22 and a diameter of the second smooth cylindrical portion 24.
- the pin member 12 includes a frangible portion 28 having third and fourth smooth cylindrical portions 29, 30 and a transition portion 31 intermediate the third and fourth smooth cylindrical portions 29, 30.
- an annular breakneck groove 32 is positioned intermediate the transition portion 31 and the second smooth cylindrical portion 24.
- the pin member 12 includes a head 34 positioned at the first end 18 thereof.
- the head 34 is a countersunk-shaped head.
- the head 34 includes a flat surface 36.
- the head 34 is a protruding head.
- the frangible portion 28 of the pin member 12 includes a pull portion 38 positioned at the second end 20 thereof and having a plurality of annular pull grooves 40 that are adapted to be engaged by a puller of a fastener installation tool.
- the pin member 12 is made from a high-strength titanium alloy.
- the pin member 12 is made from beta-C titanium.
- the pin member 12 is made from other titanium alloys, such as Ti 6-4 or Ti 555 titanium alloys, or other suitable metallic materials.
- the lock ring 14 includes a first end 42, a second end 44 opposite the first end 42, an aperture 46 that extends from the first end 42 to the second end 44, a surface 48 located at the first end 42, an outer surface 50 extending from the first end 42 to the second end 44, and an inner surface 52 extending from the first end 42 to an outwardly extending annular flange 53 located at the second end 44.
- the lock ring 14 is made from a low strength titanium alloy.
- the lock ring 14 is made from CP titanium.
- the lock ring 14 is made from MONEL® nickel alloy.
- the lock ring 14 is made from A286 stainless steel.
- the lock ring 14 is made from shaped wire and wrapped around the pin member 12. With reference to FIGS. 4 and 5, in an embodiment, the lock ring 14 is installed on the pin member 12 and the flange 53 is swaged or rolled into the lock groove 26 of the pin member 12, forming an inwardly extending annular bead 54. In an embodiment, the annular bead 54 of the lock ring 14 engages the lock groove 26 of the pin member 12 and secures the lock ring 14 to the pin member 12.
- the rivet 10 is adapted to be installed within a structure 56 containing a plurality of work pieces.
- the work pieces include an first panel 58, a second panel 60 juxtaposed with the first panel 58, a first strip 62 juxtaposed with and attached to the first panel 58, and a second strip 64 juxtaposed with and attached to the second panel 60.
- the first strip 62 includes an outer surface 66
- the second strip 64 includes an outer surface 68.
- each of the first and second panels 58, 60 includes a hole 70, 72, respectively, while the first strip 62 includes a hole 74 having a countersunk portion 76 within the outer surface 66, and the second strip 64 includes a hole 78 having a countersunk portion 80 within the outer surface 68.
- the holes 70, 72 and the holes 74, 78 are aligned with one another.
- the first and second panels 58, 60 and the first and second strips 62, 64 are made of aluminum, an aluminum alloy, other metallic alloys, composites, or combinations thereof. In other embodiments, the first and second strips 62, 64 need not be included in the structure 56.
- the lock ring 14 is received by the pin member 12 by insertion of the elongated shank 16 of the pin member 12 through the aperture 46 of the lock ring 14.
- the lock ring 14 is positioned on the first cylindrical smooth portion 22 and around the second smooth cylindrical portion 24 and the third cylindrical smooth portion 30.
- the bead 54 of the lock ring 14 engages the lock groove 26 of the pin member 12 in order to secure the pin member 12 and the lock ring 14 to one another.
- a fastener installation tool includes a swaging anvil 82 and a collet (not shown in the Figures).
- a spring member 84 is positioned between the anvil 82 and the first strip 62 first panel 58.
- the spring member 84 is made of rubber.
- the collet engages the pull grooves 40 of the pull portion 38 of the pin member 12 (not shown in the Figures) to apply an axial force thereon and pull the rivet 10 into the structure 56 until the surface 36 of the head 34 is flush (or substantially flush) with the outer surface 68 of the second strip 64.
- the swage anvil 82 housed within a tool housing 86, engages the lock ring 14 and applies an axial force on the surface 48 thereof to commence further swaging of the lock ring 14 to the pin member 12.
- the spring member 84 is compressed by the anvil 82 and the first strip 64. In this regard, the spring member 84 is pushed against the first strip 64 and reacts to the load provided on the structure to facilitate closing the sheet gap between the panels 58, 60. In an embodiment, the spring member 84 generates pre-load.
- the swaging process continues until a portion of the lock ring 14 proximate to the first end 42 thereof deforms into the countersunk portion 76 of the hole 74 of the first strip 62 and the hole 70 of the first panel 58, and a portion P of the outer surface 50 proximate to the first end 42 deforms and rotates inwardly until the portion P is flush (or substantially flush) with the outer surface 66 of the first strip 62.
- the breakneck groove 32 is aligned (or substantially aligned) with the outer surface 66 of the first strip 62.
- the bead 54 of the lock ring 14 maintains its engagement with the lock groove 26 of the pin member 12, thereby securing the rivet 10 to the structure 56.
- the fastener installation tool continues to apply a pulling force on the pull portion 38 of the pin member 12 (not shown) until the pull portion 38 and the frangible portion 28 separates from the remainder of the pin member 12 at the breakneck groove 32.
- the surface 36 of the head 34 of the pin member 12 is flush (or substantially flush) with the outer surface 68 of the second strip 64, while the portion P of the surface 50 of the lock ring 14 and a newly formed pin break fracture surface 88 of the pin member 12 (i.e., at the former location of the breakneck groove 32 proximate to the second smooth cylindrical portion 24) are flush (or substantially flush) with the outer surface 66 of the first strip 62. Accordingly, the rivet 10 is double flush on opposite sides of the structure 56.
- FIGS. 10 and 11 show another embodiment of a rivet 110 having a pin member 112 and a lock ring 114.
- the rivet 110 is constructed and functions similar to the rivet 10 with certain differences. That is, in an embodiment, an elongated shank 116 of the pin member 112 includes a first smooth cylindrical shank portion 122 and a second smooth cylindrical portion 124, but does not include a lock groove therebetween, nor does the lock ring include a corresponding annular bead. Instead, the lock ring 114 is secured to the second smooth cylindrical portion 124 by an annular weld 115.
- the rivets 10, 110 are used in aerospace applications. In another embodiment, the rivets 10, 110 are used in industrial applications.
- the structure 56 may include only two work pieces, i.e., the first and second panels 58, 60. In other embodiments, the structure 56 may incorporate any number of work pieces. All such variations and modifications are intended to be included within the scope of the invention as defined in the appended claims.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Insertion Pins And Rivets (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES14845948T ES2710362T3 (en) | 2013-09-19 | 2014-09-10 | Rivet |
CA2908220A CA2908220C (en) | 2013-09-19 | 2014-09-10 | Rivet |
BR112015025559-0A BR112015025559B1 (en) | 2013-09-19 | 2014-09-10 | rivet |
EP14845948.0A EP2920474B1 (en) | 2013-09-19 | 2014-09-10 | Rivet |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201361879859P | 2013-09-19 | 2013-09-19 | |
US61/879,859 | 2013-09-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2015041908A1 true WO2015041908A1 (en) | 2015-03-26 |
Family
ID=52331155
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2014/054995 WO2015041908A1 (en) | 2013-09-19 | 2014-09-10 | Rivet |
Country Status (7)
Country | Link |
---|---|
US (1) | US9488206B2 (en) |
EP (1) | EP2920474B1 (en) |
CN (2) | CN104454871B (en) |
BR (1) | BR112015025559B1 (en) |
CA (1) | CA2908220C (en) |
ES (1) | ES2710362T3 (en) |
WO (1) | WO2015041908A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2908220C (en) * | 2013-09-19 | 2017-06-27 | Alcoa Inc. | Rivet |
US20170014952A1 (en) * | 2014-06-17 | 2017-01-19 | United Technologies Corporation | Systems and methods for dissimilar material welding |
US20180274578A1 (en) * | 2017-03-23 | 2018-09-27 | GM Global Technology Operations LLC | Joining system and method |
CN112610582B (en) * | 2020-12-25 | 2023-01-24 | 航天精工股份有限公司 | Novel high locking self-plugging rivet |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB766137A (en) * | 1953-09-08 | 1957-01-16 | Huck Mfg Co | Improvements relating to a collar and the combination thereof with a pin of a two-part fastener |
US3459447A (en) * | 1966-12-13 | 1969-08-05 | Huck Mfg Co | Flush fastener for panel assembly including soft core material |
US4254809A (en) * | 1978-09-11 | 1981-03-10 | Hi Shear Corporation | Two-piece rivet |
WO1986006447A2 (en) | 1985-04-29 | 1986-11-06 | Huck Manufacturing Company | Expansion type anchor bolt |
GB2227538A (en) * | 1988-10-20 | 1990-08-01 | Avdel Systems Ltd | Swageable tubular member |
US6659699B2 (en) * | 2001-02-20 | 2003-12-09 | Airbus Deutschland Gmbh | Lockbolt for forming a mechanically secured and sealant sealed connection between components |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2061629A (en) * | 1933-07-20 | 1936-11-24 | Huxon Holding Corp | Rivet |
US3288016A (en) * | 1964-07-06 | 1966-11-29 | Huck Mfg Co | Blind two-piece fastener |
US3460429A (en) * | 1967-04-19 | 1969-08-12 | Jack La Torre | Expansible fastener with expander therefor |
GB1518084A (en) * | 1974-08-16 | 1978-07-19 | Avdel Ltd | Rivet |
US4112811A (en) * | 1977-04-15 | 1978-09-12 | John Olmsted King | Self-dimpling fastener pin |
US4405273A (en) * | 1977-07-19 | 1983-09-20 | Huck Manufacturing Company | Blind fasteners |
US4221041A (en) | 1978-10-02 | 1980-09-09 | Boeing Commercial Airplane Company | Semi-tubular rivets and method of using |
GB8517659D0 (en) * | 1985-07-12 | 1985-08-21 | Avdel Ltd | Self-plugging blind fastener |
US4826372A (en) * | 1986-08-06 | 1989-05-02 | Victor Pastushin | Pre-locked pull-type blind fastener |
US5049016A (en) | 1989-06-07 | 1991-09-17 | Huck Manufacturing Company | Swage fasteners with a high stand-off collar |
US5006024A (en) * | 1990-03-05 | 1991-04-09 | George Siebol | Dual-lock blind fastener |
GB2269873A (en) * | 1992-08-21 | 1994-02-23 | Avdel Systems Ltd | Self-plugging blind fastener |
US5429464A (en) * | 1994-02-16 | 1995-07-04 | Textron Inc. | Blind fastener with two-piece expander |
US6325582B1 (en) | 2000-07-06 | 2001-12-04 | Huck International, Inc. | Swage type fastener with low swage load |
US6551040B1 (en) * | 2001-12-27 | 2003-04-22 | Huck International, Inc. | Blind fastener with a blind side head having a clamp support and lock section |
US7695226B2 (en) | 2006-09-21 | 2010-04-13 | Alcoa Global Fasteners, Inc. | High performance sleeved interference fasteners for composite applications |
FR2914966B1 (en) | 2007-04-12 | 2010-09-10 | Eris | METHOD FOR MANUFACTURING RIVET AND RIVET OBTAINED ACCORDING TO THIS PROCESS |
US8029220B2 (en) * | 2008-12-16 | 2011-10-04 | Self-Fix Metals Ltd. | Blind rivet assembly |
US8434984B2 (en) * | 2009-09-09 | 2013-05-07 | Polaris Fastening Consulting, Llc | Self-interlocking sleeve-core shear pin fastener |
WO2012129390A1 (en) | 2011-03-24 | 2012-09-27 | Alcoa Inc. | Hybrid collar for fastening systems |
US20130202382A1 (en) | 2012-02-02 | 2013-08-08 | Alcoa Inc. | Swage indicating collar |
CA2908220C (en) | 2013-09-19 | 2017-06-27 | Alcoa Inc. | Rivet |
-
2014
- 2014-09-10 CA CA2908220A patent/CA2908220C/en active Active
- 2014-09-10 ES ES14845948T patent/ES2710362T3/en active Active
- 2014-09-10 US US14/482,792 patent/US9488206B2/en active Active
- 2014-09-10 WO PCT/US2014/054995 patent/WO2015041908A1/en active Application Filing
- 2014-09-10 BR BR112015025559-0A patent/BR112015025559B1/en active IP Right Grant
- 2014-09-10 EP EP14845948.0A patent/EP2920474B1/en active Active
- 2014-09-19 CN CN201410482429.9A patent/CN104454871B/en active Active
- 2014-09-19 CN CN201420541912.5U patent/CN204113841U/en not_active Withdrawn - After Issue
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB766137A (en) * | 1953-09-08 | 1957-01-16 | Huck Mfg Co | Improvements relating to a collar and the combination thereof with a pin of a two-part fastener |
US3459447A (en) * | 1966-12-13 | 1969-08-05 | Huck Mfg Co | Flush fastener for panel assembly including soft core material |
US4254809A (en) * | 1978-09-11 | 1981-03-10 | Hi Shear Corporation | Two-piece rivet |
WO1986006447A2 (en) | 1985-04-29 | 1986-11-06 | Huck Manufacturing Company | Expansion type anchor bolt |
GB2227538A (en) * | 1988-10-20 | 1990-08-01 | Avdel Systems Ltd | Swageable tubular member |
US6659699B2 (en) * | 2001-02-20 | 2003-12-09 | Airbus Deutschland Gmbh | Lockbolt for forming a mechanically secured and sealant sealed connection between components |
Also Published As
Publication number | Publication date |
---|---|
CN204113841U (en) | 2015-01-21 |
CN104454871B (en) | 2016-08-10 |
ES2710362T3 (en) | 2019-04-24 |
US9488206B2 (en) | 2016-11-08 |
EP2920474B1 (en) | 2018-11-07 |
CA2908220A1 (en) | 2015-03-26 |
EP2920474A4 (en) | 2016-10-05 |
BR112015025559B1 (en) | 2021-03-02 |
EP2920474A1 (en) | 2015-09-23 |
US20150078856A1 (en) | 2015-03-19 |
CN104454871A (en) | 2015-03-25 |
BR112015025559A2 (en) | 2017-07-18 |
CA2908220C (en) | 2017-06-27 |
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