CPC B64C 1/403 (2013.01) [B64C 1/40 (2013.01); F16B 2/20 (2013.01)] | 20 Claims |
1. An insulation system for an aircraft fuselage having a plurality of stringers extending longitudinally, the system comprising:
an insulation blanket configured for installation on the stringers; and
a plurality of stringer clips attached to and extending from an outboard surface of the insulation blanket, each stringer clip having:
a connecting flange engaged to a cover of the insulation blanket;
a first attachment arm extending outboard from a first end of the connecting flange and terminating in a first hook resiliently engaging a top plate of the stringer; and
a second attachment arm extending outboard from a second end of the connecting flange and terminating in a second hook resiliently engaging a bottom plate of the stringer.
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