INJECTABLE CAP ASSEMBLY AND METHOD OF USE
INJECTABLE CAP ASSEMBLY AND METHOD OF USE
- New search for: GRIMM MICHAEL B
- New search for: FLADHAMMER SCOTT T
- New search for: GRIMM MICHAEL B
- New search for: FLADHAMMER SCOTT T
An injectable cap assembly (100) is provided that includes a cap housing (120) with a cover portion (124) having a base (128) that extends substantially therearound, and an inner chamber (130) positioned therein, a sealant flow channel (140) extending along the base (128), a sealant input tube (132) in fluid communication with the sealant flow channel (140) and extending upwards from the base (128), a sealant output tube (142) in fluid communication with the sealant flow channel (140) and extending upwards from the base (128). The assembly (100) further includes a cap insert (122) securable within the inner chamber (130) of the cap housing (120), the insert (122) having a plurality of insert fingers (148) for engagement with a fastener (102), and a plurality of outer walls (154) interconnected with the insert fingers (148), the outer walls (154) securably engageable with the inner chamber (130).
Document information
INJECTABLE CAP ASSEMBLY AND METHOD OF USE
INJIZIERBARE KAPPENANORDNUNG UND VERFAHREN ZUR VERWENDUNG
ENSEMBLE CAPUCHON INJECTABLE ET SON PROCÉDÉ D'UTILISATION
2021-02-17
Patent
Electronic Resource
English
| IPC: | F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |