Device for connecting two tubular pieces of an aircraft...

Pipe joints or couplings – Packed – Flanged pipe

Reexamination Certificate

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Details

C285S047000

Reexamination Certificate

active

06857669

ABSTRACT:
A connecting device for connecting first and second tubular pieces of an aircraft turbine engine may include a rigid ring with an at least approximately S-shaped cross section. The rigid ring is housed in a recess of an acoustic protection cellular core of the first tubular piece and includes: (1) an external branch, which bears against an external skin of the second tubular piece and is secured to the latter by a first fixing device; (2) a back, arranged facing an edge face of the cellular core; (3) a front arranged facing the first tubular piece, after the first and second tubular pieces have been connected; (4) a transverse branch connecting the back to the front; and (5) an internal branch connected to an internal skin of the second tubular piece and secured to the latter.

REFERENCES:
patent: 4293053 (1981-10-01), Shuttleworth et al.
patent: 4506616 (1985-03-01), Nixon
patent: 5658024 (1997-08-01), Bachmann et al.
patent: 6123170 (2000-09-01), Porte et al.
patent: 6328258 (2001-12-01), Porte
patent: 0352993 (1990-01-01), None
patent: 2474099 (1981-07-01), None
patent: 2767560 (1999-02-01), None
patent: 2787509 (2000-06-01), None
patent: 2010434 (1979-06-01), None

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