FIELD: aircraft manufacture; riveting. SUBSTANCE: blind rivet has body 1 with concave starting chamfer on outer surface having taper section at angle of 6 to 10 deg on one side and manufactured head on other side and with axial hole where core 6 is fitted at negative allowance; core has head at one and technological knurled end-piece 8 at other end. Working portion of core (6) is provided with circular recess and deformable bush (13); bush (13) is mounted between head of core and end of body with starting chamfer. Locking ring (14) of shaped profile is located between body and core; removable thrust plate (15) is located on side of outer surface of manufactured head of rivet. EFFECT: improved quality; reduced overall dimensions and facilitated manufacture. 3 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| RIVET FOR UNILATERAL RIVETING | 0 | 
 | SU1760195A1 | 
| RIVET FOR SINGLE-SIDE RIVETING | 2000 | 
 | RU2178533C1 | 
| RIVET FOR ONE-SIDED RIVETING | 1992 | 
 | RU2006692C1 | 
| RIVET | 1989 | 
 | RU2054584C1 | 
| BLIND RIVET | 1999 | 
 | RU2156895C1 | 
| RIVET FOR ONE-SIDE RIVETING | 2008 | 
 | RU2394174C1 | 
| RIVET | 0 | 
 | SU1490328A1 | 
| RIVET FOR JOINING COMPONENTS | 0 | 
 | SU1163062A1 | 
| RIVET | 0 | 
 | SU1516637A1 | 
| IMPULSE RIVETING METHOD | 1994 | 
 | RU2076014C1 | 
Authors
Dates
1999-08-10—Published
1994-09-21—Filed