JPH0318945B2 - - Google Patents
Info
- Publication number
- JPH0318945B2 JPH0318945B2 JP10315884A JP10315884A JPH0318945B2 JP H0318945 B2 JPH0318945 B2 JP H0318945B2 JP 10315884 A JP10315884 A JP 10315884A JP 10315884 A JP10315884 A JP 10315884A JP H0318945 B2 JPH0318945 B2 JP H0318945B2
- Authority
- JP
- Japan
- Prior art keywords
- sealant
- hole
- protrusion
- lock collar
- tip
- 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.)
- Expired
Links
Landscapes
- Coating Apparatus (AREA)
- Hand Tools For Fitting Together And Separating, Or Other Hand Tools (AREA)
Description
【発明の詳細な説明】
〔発明の技術分野〕
本発明は打鋲装置におけるシーラント塗布装置
に関する。本発明は航空機の主翼外板のリベツテ
イングに際してのシーラント塗布に特に適してい
る。DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to a sealant application device for a fastener driving device. The present invention is particularly suitable for applying sealant during riveting to aircraft wing skins.
航空機の主翼外板の打鋲の際には、リベツトま
たはロツクピンを挿通する被連結部材の貫通孔の
内面、および貫通孔の開口部近傍にシーラントを
供給、塗布し、打鋲後にリベツトまたはロツクピ
ンと被連結部材との間の隙間が完全にシールされ
るようにする。
When driving rivets on the main wing skin of an aircraft, sealant is supplied and applied to the inner surface of the through-hole of the connected member through which the rivet or lock pin is inserted, and near the opening of the through-hole, and after driving the rivet or lock pin, To ensure that the gap between the connected member and the connected member is completely sealed.
従来、シーラントの塗布のためには、被連結部
材の貫通孔の両端の開口内へ各側からシーラント
塗布ノズルを挿入して貫通孔の内面およびその近
傍にシーラントを供給している。シーラントの塗
布は、貫通孔の一端に設けられる皿取り部の面に
ついては良好に行うことができるが、貫通孔の他
端からシーラント塗布ノズルを挿入して行うシー
ラントの塗布は特に貫通孔の内壁面については必
ずしも十分に行うことができないという問題があ
る。 Conventionally, in order to apply a sealant, a sealant application nozzle is inserted from each side into openings at both ends of a through hole of a connected member to supply sealant to the inner surface of the through hole and its vicinity. The sealant can be applied well to the surface of the countersunk part provided at one end of the through hole, but the application of sealant by inserting the sealant application nozzle from the other end of the through hole is especially effective on the inside of the through hole. There is a problem in that it cannot always be done sufficiently on walls.
航空機の主翼内部は、燃料タンクとして用いら
れているため、前記シール部に欠陥があればその
部分より燃料漏れによる重大事故発生の原因とな
る。特に高性能かつ高安全性を要求される航空機
に関しては、前記不具合を完全に解消しなければ
ならない。 Since the inside of the main wing of an aircraft is used as a fuel tank, if there is a defect in the seal, fuel may leak from that part, causing a serious accident. Especially for aircraft that require high performance and high safety, the above-mentioned problems must be completely eliminated.
本発明はこのような問題に鑑みなされたもの
で、その目的は、貫通孔の皿取り部の反対側の開
口から行なうシーラントの塗布を、貫通孔の内壁
面についても良好に行なうことのできる打鋲装置
におけるシーラント塗布装置を得ることにある。
The present invention has been made in view of these problems, and its purpose is to provide a sealant that can be applied well to the inner wall surface of the through hole when the sealant is applied from the opening on the opposite side of the countersunk portion of the through hole. An object of the present invention is to obtain a sealant application device for a rivet device.
上述の目的を達成するための本発明のシーラン
ト塗布装置は、打鋲により連結すべき被連結部材
に皿取り部を一端に有する貫通孔を形成する装置
と、貫通孔の皿取り部内に挿入されて皿取り部の
面にシーラントを供給する第1のシーラント塗布
ノズルと、貫通孔の皿取り部と反対の側の開口内
に挿入される突部を先端中央部に有し、突部の基
部を囲む先端面にシーラント供給孔をもつ第2の
シーラント塗布ノズルとを備え、前記突部はその
基部へ至るにつれて断面積を減少させたことを特
徴とする。
To achieve the above object, the sealant applicator of the present invention includes a device for forming a through hole having a countersunk portion at one end in connected members to be connected by driving rivets, and a device that is inserted into the countersunk portion of the through hole. a first sealant application nozzle that supplies sealant to the surface of the countersunk portion; a protrusion to be inserted into the opening on the opposite side of the countersunk portion of the through hole; and a second sealant application nozzle having a sealant supply hole in a distal end surface surrounding the protrusion, and the protrusion has a cross-sectional area that decreases as it reaches its base.
第1図において、2は打鋲される被連結部材の
一例としての航空機の主翼である。この主翼2は
加工物支持枠3に図示を省略した固定手段により
固定される。支持枠3は長方形をなし、その長手
方向両端は支軸4によりキヤリツジ6に支持され
ている。支持枠3は支軸4まわりで任意角度に回
転変位させて固定することができる。キヤリツジ
6はY−Y方向にガイド7に沿つて変位できるよ
うに支承されている。
In FIG. 1, reference numeral 2 indicates a main wing of an aircraft as an example of a member to be connected to which rivets are driven. The main wing 2 is fixed to the workpiece support frame 3 by a fixing means (not shown). The support frame 3 has a rectangular shape, and both longitudinal ends thereof are supported by a carriage 6 by a support shaft 4. The support frame 3 can be rotated at any angle around the support shaft 4 and fixed. The carriage 6 is supported so as to be displaceable along a guide 7 in the Y-Y direction.
キヤリツジ6を支持するガイド7はZ−Z方向
に変位可能に支柱8に支持されており、支柱8は
X−X方向にレール10に沿つて走行可能の台車
11に支持されている。キヤリツジ6、ガイド
7、台車11等の変位は適当なモータによりなさ
れる。 A guide 7 supporting the carriage 6 is supported by a column 8 so as to be movable in the Z-Z direction, and the column 8 is supported by a truck 11 that can run along a rail 10 in the XX direction. The carriage 6, guide 7, truck 11, etc. are displaced by appropriate motors.
加工物支持枠3を上下から挟む形状をもつリベ
ツタフレーム13がレール10の一側に設置され
る。このリベツタフレーム13の上方の腕13a
の先端には後述の第1の筒状押圧部材、ロツクピ
ン供給装置等が設けられ、またその下方の腕13
bの先端部には後述の第2の筒状押圧部材、ロツ
クカラー供給装置、ロツクカラー駆動軸等が設け
られる。そして、リベツタフレーム腕13aに設
けた上述の装置およびリベツタフレーム腕13b
に設けた上述の装置が主翼2の上方および下方か
らそれぞれ主翼に対し作用を及ぼすことによつ
て、後述のようにして打鋲作業が行われる。 A riveter frame 13 having a shape that sandwiches the workpiece support frame 3 from above and below is installed on one side of the rail 10. The upper arm 13a of this riveter frame 13
A first cylindrical pressing member, a lock pin supply device, etc., which will be described later, are provided at the tip of the arm 13.
A second cylindrical pressing member, a lock collar supply device, a lock collar drive shaft, etc., which will be described later, are provided at the tip of b. The above-described device provided on the riveter frame arm 13a and the riveter frame arm 13b
The above-mentioned device installed in the main wing 2 acts on the main wing 2 from above and below, respectively, thereby performing the fastening operation as described below.
打鋲は主翼2の全面の無数の位置に対してなさ
れ、その作用は、リベツタ駆動油圧ユニツト1
4、NC制御装置15、シーケンスコントローラ
16により制御される。なお、17は電圧ボツク
スを示す。 The riveting is done at countless positions on the entire surface of the main wing 2, and the action is carried out by the riveter drive hydraulic unit 1.
4. Controlled by NC control device 15 and sequence controller 16. Note that 17 indicates a voltage box.
第2図において、20はリベツタフレームの上
方の腕13aに設けられた第1の筒状押圧部材、
21は下方の腕13bに設けられた第2の筒状押
圧部材であり、これらの両押圧部材20,21は
被連結部材2a,2bに対し接近するように移動
自在にリベツタフレーム13に支持されている。
第2の押圧部材21は円筒状をなし、その内部に
中空のロツクカラー駆動軸22を有している。こ
の駆動軸22は図示しない駆動源に連結されてい
て回転駆動されるものであり、また押圧部材21
内で軸線方向に摺動変位自在となつている。ま
た、ロツクカラー駆動軸22の内面にはその長手
方向に突条23が形成され、突条23の上端に続
いてロツクカラー駆動軸内面24が非円形断面、
たとえば長円形断面に形成されている。 In FIG. 2, 20 is a first cylindrical pressing member provided on the upper arm 13a of the riveter frame;
21 is a second cylindrical pressing member provided on the lower arm 13b, and both of these pressing members 20, 21 are supported by the riveter frame 13 so as to be movable so as to approach the connected members 2a, 2b. has been done.
The second pressing member 21 has a cylindrical shape and has a hollow lock collar drive shaft 22 therein. This drive shaft 22 is connected to a drive source (not shown) and is rotationally driven, and the pressing member 21
It can be slid freely in the axial direction. Further, a protrusion 23 is formed on the inner surface of the lock collar drive shaft 22 in its longitudinal direction, and following the upper end of the protrusion 23, the inner surface 24 of the lock collar drive shaft has a non-circular cross section.
For example, it is formed in an oval cross section.
第2図の状態から第1および第2の筒状押圧部
材20,21は被連結部材2a,2bの面に向か
つて相対的に前進し、両筒状部材20,21の端
面が第3図に示すように被連結部材の面に押しつ
けられ、これにより被連結部材は両押圧部材2
0,21により挟圧保持される。 From the state shown in FIG. 2, the first and second cylindrical pressing members 20, 21 move relatively forward toward the surfaces of the connected members 2a, 2b, and the end surfaces of both cylindrical members 20, 21 are moved forward as shown in FIG. As shown in FIG.
It is held under pressure by 0 and 21.
つぎに、第3図の状態のままで、穿孔ドリル2
6が第4図に示すように下降させられて貫通孔2
7が形成される。貫通孔27は上端側に皿取り部
28を有するようにされ、このために穿孔ドリル
26には皿取り部形成刃29が設けられる。 Next, while maintaining the state shown in Figure 3, drill the drilling drill 2.
6 is lowered to open the through hole 2 as shown in FIG.
7 is formed. The through hole 27 has a countersunk portion 28 on the upper end side, and for this purpose, the drilling drill 26 is provided with a countersunk portion forming blade 29.
このようにして貫通孔27を形成した被連結部
材2a,2bは両押圧部材20,21により挟圧
された状態で、貫通孔27の内面およびその近傍
にシーラントを塗布される。このためには、第5
図に示すようにシーラント塗布ノズル31,32
を貫通孔27の上下開口部内へ前進させる。 A sealant is applied to the inner surface of the through hole 27 and the vicinity thereof while the connected members 2a and 2b having the through hole 27 formed in this manner are pressed by both the pressing members 20 and 21. For this purpose, the fifth
As shown in the figure, sealant application nozzles 31, 32
are advanced into the upper and lower openings of the through hole 27.
第1のシーラント塗布ノズル31は被連結部材
2a,2bの上方に設けられており、シーラント
供給管34の先端部に螺合により固定されてい
る。シーラント塗布ノズル31内へは、ばね35
により弾圧されたボール36からなるバルブを経
てシーラントが供給され、ノズル31の先端部の
ノズル軸線に角度をなすシーラント供給孔37か
ら吹出される。ノズル31の先端面は皿取り部2
8の面に合う円すい面をなしている。シーラント
供給孔37は円周方向に等間隔で例えば4個設け
られる。シーラント供給孔37から供給されたシ
ーラントは貫通孔27の皿取り部28の面に塗布
され、さらにそれより下方の貫通孔27の内面に
も流れる。 The first sealant application nozzle 31 is provided above the connected members 2a, 2b, and is fixed to the tip of the sealant supply pipe 34 by screwing. A spring 35 is inserted into the sealant application nozzle 31.
The sealant is supplied through a valve made up of a ball 36 that is compressed by the sealant, and is blown out from a sealant supply hole 37 formed at an angle to the nozzle axis at the tip of the nozzle 31. The tip surface of the nozzle 31 has a countersunk portion 2
It has a conical surface that fits the surface of 8. For example, four sealant supply holes 37 are provided at equal intervals in the circumferential direction. The sealant supplied from the sealant supply hole 37 is applied to the surface of the countersunk portion 28 of the through hole 27, and also flows to the inner surface of the through hole 27 below it.
本発明の要部をなす第2のシーラント塗布ノズ
ル32はシーラント供給管39の先端部に螺合に
より固定され、塗布ノズル32内へはばね40に
より弾圧されたボール41からなるバルブを経て
シーラントが上方へ供給される。塗布ノズル32
はその先端中央に突部43が形成されており、こ
の突部43は基部へ近づくにつれ断面積(径)が
小さくなつており、また突部43の先端寄り部は
貫通孔27の内径とほぼ等しい外径を有してい
る。したがつて、突部43が貫通孔27へと挿入
されると、突部の基部の外周面と貫通孔内壁との
間に隙間44が形成される。突部43の基部の外
周には等間隔でシーラント供給孔45が形成され
る。ノズル32の先端部の外周には突部43を囲
む環状突起46が設けられ、シーラント供給孔4
5の出口部に環状空間47が形成される。 The second sealant application nozzle 32, which forms the main part of the present invention, is fixed to the tip of the sealant supply pipe 39 by screwing, and the sealant is supplied into the application nozzle 32 through a valve consisting of a ball 41 pressed by a spring 40. Supplied upwards. Application nozzle 32
A protrusion 43 is formed at the center of the tip, and the cross-sectional area (diameter) of this protrusion 43 becomes smaller as it approaches the base, and the tip of the protrusion 43 is approximately the same as the inner diameter of the through hole 27. have equal outer diameters. Therefore, when the protrusion 43 is inserted into the through hole 27, a gap 44 is formed between the outer peripheral surface of the base of the protrusion and the inner wall of the through hole. Sealant supply holes 45 are formed at equal intervals on the outer periphery of the base of the protrusion 43 . An annular protrusion 46 surrounding a protrusion 43 is provided on the outer periphery of the tip of the nozzle 32, and the sealant supply hole 4
An annular space 47 is formed at the exit portion of 5.
シーラントの塗布のために第2の塗布ノズル3
2を第5図の位置へ前進させてシーラントをシー
ラント供給孔45から供給すると、シーラントは
貫通孔27の下部開口周囲の被連結部材の下面に
塗布されるとともに、隙間44の存在によつて貫
通孔27の内壁面にもよく塗布される。これは突
部43の特有の形状により隙間44が下方へ向か
つて広がつていることにより可能となる。 Second application nozzle 3 for application of sealant
2 is advanced to the position shown in FIG. The inner wall surface of the hole 27 is also well coated. This is possible because the gap 44 widens downward due to the unique shape of the protrusion 43.
以上のようにして貫通孔17とその近傍にシー
ラントが良く塗布された後、両塗布ノズル31,
32は後退し、ついで、第6図に示すように貫通
孔27内にロツクピン50が上方から挿通され
る。このロツクピン50は第1の押圧部材20の
内部を経て供給される。ロツクピン50は皿取り
部28に相当する形状の頭51を有し、さらに先
端部におねじ52を、また先端面に非円形係合部
53を有している。非円形係合部53はこの実施
例では非円形穴である。 After the sealant is well applied to the through hole 17 and its vicinity as described above, both application nozzles 31,
32 is retracted, and then, as shown in FIG. 6, the lock pin 50 is inserted into the through hole 27 from above. This locking pin 50 is fed through the interior of the first pressing member 20. The lock pin 50 has a head 51 having a shape corresponding to the countersunk portion 28, and further has a thread 52 at its tip and a non-circular engagement portion 53 at its tip surface. The non-circular engagement portion 53 is a non-circular hole in this embodiment.
つぎに、第7図に示すようにスリーブ55内で
案内されるアンビル56が下降させられてロツク
ピン50の頭の上面を上方から押さえる。 Next, as shown in FIG. 7, an anvil 56 guided within the sleeve 55 is lowered to press the top surface of the head of the lock pin 50 from above.
ついで、第8図に示すようにロツクカラー60
がロツクカラー駆動軸22の内部を通つて下方か
ら押上られてロツクピン50の先端にはめられ
る。ロツクカラー60はめねじ61を有し、途中
部分に薄肉の弱化部62をもつている。図には示
されていないが、ロツクカラー60はロツクカラ
ー駆動軸22の突条23に摺動自在に係合する溝
を外面に有し、突条23に案内されつつロツクカ
ラーフイーダ63によつて上方へ押上げられる。
第8図の位置にまで押上げられたロツクカラー6
0はロツクカラー駆動軸22の非円形断面内面2
4に係合する。このためにはロツクカラー60の
断面形状を非円形断面内面24に密に接する形状
にしておく。 Then, as shown in FIG.
is pushed up from below through the inside of the lock collar drive shaft 22 and fitted onto the tip of the lock pin 50. The lock collar 60 has a female thread 61 and a thin weakened portion 62 in the middle. Although not shown in the figure, the lock collar 60 has a groove on its outer surface that slidably engages with the protrusion 23 of the lock collar drive shaft 22, and is guided by the protrusion 23 while being guided by the lock collar feeder 63. being pushed upwards.
Lock collar 6 pushed up to the position shown in Figure 8
0 is the non-circular cross-sectional inner surface 2 of the lock collar drive shaft 22
4. For this purpose, the cross-sectional shape of the lock collar 60 is made to be in close contact with the non-circular cross-sectional inner surface 24.
一方、ロツクピン固定用マンドレル65をロツ
クカラー60と共に上昇させ。その先端の非円形
係合部66のロツクピン50の非円形係合部53
内にはめ、ロツクピン50の回転を阻止する。 Meanwhile, the lock pin fixing mandrel 65 is raised together with the lock collar 60. Non-circular engaging portion 53 of lock pin 50 of non-circular engaging portion 66 at its tip
the lock pin 50 from rotating.
第8図の状態においてロツクカラー駆動軸22
を同図のAで示す方向に回転駆動すると、ロツク
カラー60がねじ込み方向に回転され、第9図に
示すようにロツクカラー60はその先端面が被連
結部材2bの面に接するまで進む。 In the state shown in Fig. 8, the lock collar drive shaft 22
When the lock collar 60 is rotated in the direction indicated by A in the same figure, the lock collar 60 is rotated in the screwing direction, and the lock collar 60 advances until its distal end surface contacts the surface of the connected member 2b, as shown in FIG.
ロツクカラー60が被連結部材2bの面に接す
るとねじ込みトルクが突然増大するので、弱化部
62においてロツクカラー60は破壊される。し
たがつて、ロツクカラー駆動軸22を後退させる
と、第10図に示すようにロツクカラー60の主
体部がロツクナツト50に螺合した状態で残され
る。この状態では、さきに塗布されたシーラント
は被連結部材2a,2bとロツクピン50、ロツ
クカラー60との間に介在してシール作用を果た
すようになる。 When the lock collar 60 comes into contact with the surface of the connected member 2b, the screwing torque suddenly increases, so that the lock collar 60 is destroyed at the weakened portion 62. Therefore, when the lock collar drive shaft 22 is retracted, the main body of the lock collar 60 remains threaded into the lock nut 50, as shown in FIG. In this state, the previously applied sealant is interposed between the connected members 2a, 2b, the lock pin 50, and the lock collar 60, and performs a sealing action.
以上のようにして締付打鋲が完了した後、他の
位置での締付打鋲のために第11図に示すように
両押圧部材20,21を被締付部材から離し、次
いで被締付部材を移動させる。 After the tightening rivet driving is completed in the above manner, both pressing members 20 and 21 are separated from the member to be tightened, as shown in FIG. Move the attachment member.
本発明では、被連結部材の貫通孔の皿取り部と
反対の側の開口へ挿入される第2のシーラント塗
布ノズルの先端中央の突部をその基部へ至るにつ
れて断面積が減少するようにしたことによつて、
第2のシーラント塗布ノズルを貫通孔に当てた場
合、貫通孔内へ挿入された突部の外周と貫通孔壁
面との間に外側へ向かつて漸次広がる隙間が形成
され、したがつて、突部の周囲のシーラント供給
孔からシーラントを供給すると、シーラントはそ
の隙間の存在により貫通孔内へ導かれ、貫通孔の
内面に十分にシーラントが塗布される。
In the present invention, the cross-sectional area of the protrusion at the center of the tip of the second sealant application nozzle inserted into the opening on the opposite side of the countersunk part of the through hole of the connected member decreases as it reaches the base. By the way,
When the second sealant application nozzle is applied to the through hole, a gap is formed between the outer periphery of the protrusion inserted into the through hole and the wall surface of the through hole, and the gap gradually widens toward the outside. When the sealant is supplied from the sealant supply hole around the through hole, the sealant is guided into the through hole due to the existence of the gap, and the sealant is sufficiently applied to the inner surface of the through hole.
第1図は本発明によるシーラント塗布装置を施
した打鋲装置の全体斜視図、第2図は第1図の要
部の打鋲開始前の状態における縦断面図、第3図
および第4図は第2図の状態より順次進んだ打鋲
工程をそれぞれ示す縦断面図、第5図は本発明の
特徴をなすシーラント塗布装置の塗布状態の縦断
面図、第6図ないし第11図は、シーラント塗布
後における打鋲工程の異なる状態をそれぞれ示す
縦断面図である。
2,2a,2b……被連結部材、13……リベ
ツタフレーム、15……NC制御装置、16……
シーケンスコントローラ、20……第1の筒状押
圧部材、21……第2の筒状押圧部材、22……
ロツクカラー駆動軸、23……突条、24……非
円形断面内面、26……穿孔ドリル、27……貫
通孔、28……皿取り部、31……第1のシーラ
ント塗布ノズル、32……第2のシーラント塗布
ノズル、37……シーラント供給孔、43……突
部、44……隙間、45……シーラント供給孔、
46……環状突起、47……環状空間、50……
ロツクピン、51……頭部、53……非円形係合
部、55……スリーブ、56……アンビル、60
……ロツクカラー、61……めねじ、62……弱
化部、63……ロツクカラーフイーダ、65……
ロツクピン固定用マンドレル、66……非円形係
合部。
FIG. 1 is an overall perspective view of a fastener driving device equipped with a sealant application device according to the present invention, FIG. 2 is a longitudinal cross-sectional view of the main part of FIG. 1 in a state before starting fastener driving, and FIGS. 3 and 4 2 is a longitudinal sectional view showing the fastener driving process that has proceeded sequentially from the state shown in FIG. 2, FIG. 5 is a longitudinal sectional view showing the application state of the sealant application device which is a feature of the present invention, and FIGS. 6 to 11 are: FIG. 6 is a vertical cross-sectional view showing different states of the fastener driving process after applying the sealant. 2, 2a, 2b... Connected member, 13... Riveter frame, 15... NC control device, 16...
Sequence controller, 20... first cylindrical pressing member, 21... second cylindrical pressing member, 22...
Lock collar drive shaft, 23...Protrusion, 24...Non-circular section inner surface, 26...Drilling drill, 27...Through hole, 28...Countersunk portion, 31...First sealant application nozzle, 32... Second sealant application nozzle, 37...Sealant supply hole, 43...Protrusion, 44...Gap, 45...Sealant supply hole,
46... annular projection, 47... annular space, 50...
Lock pin, 51... Head, 53... Non-circular engaging portion, 55... Sleeve, 56... Anvil, 60
...Lock collar, 61...Female thread, 62...Weakened part, 63...Lock collar feeder, 65...
Lock pin fixing mandrel, 66...non-circular engagement part.
Claims (1)
に皿取り部28を一端に有する貫通孔27を形成
する装置20,21,26と、貫通孔の皿取り部
28内に挿入されて皿取り部の面にシーラントを
供給する第1のシーラント塗布ノズル31と、貫
通孔の皿取り部28と反対の側の開口内に挿入さ
れる突部43を先端中央部に有し、突部の基部を
囲む先端面にシーラント供給孔45をもつ第2の
シーラント塗布ノズル32とを備え、前記突部4
3はその基部へ至るにつれて断面積を減少させた
ことを特徴とする打鋲装置におけるシーラント塗
布装置。 2 第2のシーラント塗布ノズル32のシーラン
ト供給孔45のある先端面が周囲に環状突起46
を有するようにしてなる特許請求の範囲第1項記
載の打鋲装置におけるシーラント塗布装置。[Claims] 1. Connected members 2a, 2b to be connected by driving rivets
a device 20, 21, 26 for forming a through hole 27 having a countersunk portion 28 at one end; and a first sealant application device inserted into the countersink portion 28 of the through hole to supply sealant to the surface of the countersunk portion. A second tube having a nozzle 31 and a protrusion 43 inserted into the opening on the side opposite to the countersunk portion 28 of the through hole at the center of the tip, and a sealant supply hole 45 on the tip surface surrounding the base of the protrusion. a sealant application nozzle 32, and the protrusion 4
Reference numeral 3 refers to a sealant application device for a fastener driving device, characterized in that the cross-sectional area decreases as it approaches the base. 2 The tip surface of the second sealant application nozzle 32 where the sealant supply hole 45 is located has an annular protrusion 46 around it.
A sealant application device for a fastener driving device according to claim 1, comprising the following.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10315884A JPS60248254A (en) | 1984-05-22 | 1984-05-22 | Device for coating sealant in riveting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10315884A JPS60248254A (en) | 1984-05-22 | 1984-05-22 | Device for coating sealant in riveting device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS60248254A JPS60248254A (en) | 1985-12-07 |
| JPH0318945B2 true JPH0318945B2 (en) | 1991-03-13 |
Family
ID=14346692
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10315884A Granted JPS60248254A (en) | 1984-05-22 | 1984-05-22 | Device for coating sealant in riveting device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60248254A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9682429B2 (en) * | 2015-04-22 | 2017-06-20 | The Boeing Company | Reaction tool and method for forming openings in an aircraft fuselage joint |
-
1984
- 1984-05-22 JP JP10315884A patent/JPS60248254A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS60248254A (en) | 1985-12-07 |
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