To broadly provide an aircraft motion control auxiliary power unit suspension system device.
An aircraft motion control auxiliary power unit suspension system device includes a first motion control nonelastomeric member (36) and a second motion control nonelastomeric member (38), a first motion control elastomer member (40) disposed to operatively interconnect the first motion control nonelastomeric member and the second motion control nonelastomeric member. The first motion control elastomer member includes an exterior surface coating formed from an elastomeric polymer dissolved in an organic solvent and the elastomeric polymer dissolved in the solvent is applied to an exterior surface of the first motion control elastomer member, the solvent evaporates, and the elastomeric polymer crosslinks.
KRAKOWSKI FRANK J
JP2000516553A | 2000-12-12 | |||
JP2004025811A | 2004-01-29 | |||
JP2003526713A | 2003-09-09 | |||
JP2005113964A | 2005-04-28 | |||
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JP2005520016A | 2005-07-07 | |||
JP2011502066A | 2011-01-20 | |||
JP2004025811A | 2004-01-29 | |||
JP2000516553A | 2000-12-12 | |||
JP2003526713A | 2003-09-09 | |||
JP2005113964A | 2005-04-28 | |||
JP2002226635A | 2002-08-14 |
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US6328293B1 | 2001-12-11 | |||
US5902050A | 1999-05-11 | |||
US4571936A | 1986-02-25 |