Energy absorbing landing gear/tail skid including means for indicating the magnitude of impact loads

A landing gear/tail skid (10) for protecting and limiting the impact loads acting on the tail section of an aircraft, including:

• a mounting fixture (16) for securing the landing/gear tail skid (10) to the aircraft tail section;
• a contact arm (18) disposed in pivotable combination with the mounting fixture (16) about a fulcrum axis (19), the contact arm (18) rotating about the fulcrum axis (19) in response to impact loads acting on the landing gear/tail skid (10);
• the mounting fixture (16) and contact arm (18) defining pivot axes (22, 24) which are subject to relative motion in response to rotational displacement of the contact arm (18);
• and
• a cartridge assembly (20) including:
• a housing member (30) having an internal chamber (38), a reference surface (36rs), and an end portion (30e) disposed in combination with one of the pivot axes (22, or 24);
• a telescoping piston assembly (40) mounted within the internal chamber (38) of the housing member (30) and having an end portion (40e) disposed in combination with the other of the pivot axes (22, or 24);
• the housing member (30) and telescoping piston assembly (40), in combination, defining opposed bearing surfaces (36s, 46s);
• the landing gear/tail skid (10) being further characterized by:
• energy absorbing means (50) having a critical dimension (L.sub.c) and disposed within the internal chamber (38) intermediate the opposed bearing surfaces (36s, 46s);
• the energy absorbing means (50) operative, in response to impact loads coupled thereto by the opposed bearing surfaces (36s, 46s), for reacting impact loads below a threshold value without change in said critical dimension (L.sub.c);
• said energy absorbing means (50) being further operative, in response to impact loads coupled thereto by the opposed bearing surfaces (36s, 46s), for absorbing and dissipating energy of impact loads at least equal to said threshold value by changes in said critical dimension (L.sub.c);
• the housing member (30) and the energy absorbing means (50) including aligned apertures (52, 70);
• and
• indication means (60) including an elongate stem (62) and an integrally formed flange (64), said elongate stem (62) being disposed through said aligned apertures (52, 70) and said flange (64) being disposed in combination with said energy absorbing means (50), said elongate stem (62) protruding beyond said reference surface (36rs) of the housing member (30) in response to said changes in critical dimension (L.sub.c) of said energy absorbing means (50);
• said changes in said critical dimension (L.sub.c) being indicative of the magnitude of the impact loads imposed on the landing gear/tail skid (10).

A cartridge assembly (20) for use in combination with a landing gear/tail skid (10) having at least two pivot axes, (22, 24) which are subject to relative motion in response to impact loads acting on the landing gear/tail skid (10), the cartridge assembly (20) including:

• a housing member (30) having an internal chamber (38) and an end portion (30e) disposed in combination with one of the pivot axes (22, or 24);
• a telescoping piston assembly (40) mounted within said internal chamber (38) of said housing member (30) and having an end portion (40e) disposed in combination with the other of the pivot axes (22, or 24);
• said housing member (30) and telescoping piston assembly (40), in combination, defining opposed bearing surfaces (36s, 46s);
• the cartridge assembly (2) being characterized by:
• energy absorbing means (50) having a critical dimension (L.sub.c) and disposed within the internal chamber (38) intermediate the opposed bearing surfaces (36s, 46s);
• said energy absorbing means (50) operative, in response to impact loads coupled thereto by the opposed bearing surfaces (36s, 46s), for reacting impact loads below a threshold value without change in said critical dimension (L.sub.c);
• said energy absorbing means (50) being further operative, in response to impact loads coupled thereto by the opposed bearing surfaces (36s, 46s), for absorbing and dissipating energy of impact loads at least equal to said threshold value by changes in said critical dimension (L.sub.c);
• and
• indication means (60) for visually indicating changes in said critical dimension (L.sub.c) of said energy absorbing means (50);
• said changes in said critical dimension (L.sub.c) being indicative of the magnitude of the impact loads acting on the landing gear/tail skid (10)
• wherein the housing member (30) includes a reference surface (36rs), and wherein the housing member (30) and said energy absorbing means (50) include aligned apertures (52, 70), and wherein said indication means (60) includes an elongate stem (62) and an integrally formed flange (64), said elongate stem (62) being disposed through said aligned apertures (52, 70) and said flange (64) being disposed in combination with said energy absorbing means (50), said elongate stem (62) protruding beyond said reference surface (36rs) of said housing member (30) in response to said change in critical dimension (L.sub.c) of said energy absorbing means (50).