Readily changeable isolator and method of assembly thereof

Aeronautics and astronautics – Aircraft power plants – Mounting

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Details

248556, 248557, 248560, 248638, B64D 2700

Patent

active

061130303

ABSTRACT:
An isolator (26) and assembly method therefor. The isolator (26) is particularly useful for aircraft thrust reverser doors, and the like, and includes an outer member (28), and a isolator component (29). The outer member (28) has a central axis (A--A), a generally non-planar inner peripheral surface (32), and first and second axially extending slotted entryways (48, 48'). The isolator component (29) preferably includes a component axis (B--B), an inner member (30) having an external radial peripheral surface (33), and an elastomer or metal mesh member (40) surrounding said external radial peripheral surface (33). The isolator component (29) is assembled and retained within said outer member (28) by insertion endwise through said first and second slotted entryways (48, 48'), and rotating 90.degree. such that the component axis (B--B) is substantially aligned with the central axis (A--A).

REFERENCES:
patent: 3601431 (1971-08-01), Henley
patent: 4514458 (1985-04-01), Thorn et al.
patent: 5031545 (1991-07-01), Bourgeot
patent: 5033722 (1991-07-01), Lammers
patent: 5108045 (1992-04-01), Law et al.
patent: 5397112 (1995-03-01), Roth et al.
patent: 5397113 (1995-03-01), Kojima et al.
patent: 5855069 (1999-01-01), Matsubayashi et al.
patent: 5927407 (1999-07-01), Gwinn et al.
Lord Mechanical Products Publication entitled Vibration, Shock, Noise Control Product Data--Safetied Tube Form Mounts (STA Series) DS-73009; 1980.
Lord Mechanical Products Engineering Guide and Catalog for Vibration, Shock and Noise Control Products, PC2201n, pp. 75-80, Mar. 1996.

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