"Structural Provision For Ingress And Shock Absorbing Support Of Waveguide Through Aircraft Skin"

Abstract: Structural provision for Ingress and Shock absorbing support of waveguide through aircraft skin" is related to arrangement of components enabling vibration damped passage for entry of waveguide inside the aircraft through aircraft skin. The box assembly(2) of shock absorber assembly(!) contain hat(12) having cutout( 14) and recess(13) for Rubber pad(16) & (17), plurality of inbuilt flange(15) plurality of hole(23) on (15) through these hole box assembly (2) integrated with aircraft skin by. Screw and ,anchor nut(25). Wave Guide passed through opening (19) of Rubber pad (16) & (17) to achieve shock absorbent affect. At outside, Aircraft skin(28), arrangement of Doubler(4), Rubber filler(?) with plurality of hole(22), Outer rubber Gasket(S), cut-out doubler(6), Rubber filler(?) , outer plate(9) & (10) and Outer rubber Gasket(5) gives required support and sealing at waveguide ingress.

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