<<

Nat’l Highway Traffic Safety Admin., DOT § 572.196

(iv) Lower not less than 32 (b)(3) and (4) of this section, the top of mm and not more than 38 mm; the rib (drawing 180– (2) Peak lateral acceleration of the 3352) orientation in the fore-and-aft di- upper spine (T1) shall not be less than rection is 24.6 ± 2.0 degrees relative to 34 g and not more than 43 g, and the horizontal, as shown in Figure V6–B in lower spine (T12) not less than 29 g and appendix A to this subpart. not more than 37 g; (6) Adjust orientation of the legs (3) Peak impactor acceleration after such that they are symmetrical about 5 ms after time zero shall be not less the mid-, the than 30 g and not more than 36 g. touch the seat pan, the inner part of [71 FR 75370, Dec. 14, 2006, as amended at 74 the right and left legs at the are FR 29895, June 23, 2009] as close as possible to each other, the touch the designated support § 572.196 Thorax without . surface and the feet are vertical and as (a) The thorax is part of the upper close together as possible. assembly shown in drawing 180– (7) The impactor is specified in 49 3000. For this thorax test, the dummy CFR 572.200(a). is tested as a complete assembly (draw- (8) The impactor is guided, if needed, ing 180–0000) with the arm (180–6000) on so that at contact with the thorax, its the impacted side removed. The dum- longitudinal is within 1 degree of a my’s thorax is equipped with T1 and horizontal plane and perpendicular to T12 laterally oriented accelerometers the midsagittal plane of the dummy. as specified in 49 CFR 572.200(d) and The centerpoint of the impactor is with deflection potentiometers for the within 2 mm of the vertical midpoint of thorax as specified in drawing 180–3881, the second thorax rib and coincident installed as shown in drawing 180–0000 with a line parallel to the seat back in- sheet 2 of 5. When subjected to the test cline passing through the center of the procedure specified in paragraph (b) of shoulder yoke assembly arm rotation this section, the thorax shall meet the pivot (drawing 180–3327), as shown in performance requirements set forth in Figure V6–A in appendix A to this sub- paragraph (c) of this section. part. (b) Test procedure. (1) Soak the dummy assembly (180–0000) in a test en- (9) The dummy’s thorax is impacted ± vironment as specified in 49 CFR at 4.3 0.1 m/s. 572.200(j). (10) Allow a period of at least thirty (2) Seat the dummy, outfitted with (30) minutes between successive tests the torso jacket (180–3450) and cotton of the same thorax assembly. underwear pants on a calibration (c) Performance criteria. bench, specified in Figure V3 in appen- (1) While the impactor is in contact dix A to this subpart, the seat pan and with the dummy’s thorax, the the seatback surfaces of which are cov- shall conform to the following range of ered with a 2-mm-thick PTFE (Teflon) deflections: sheet. (i) Upper thorax rib not less than 32 (3) Align the outermost portion of mm and not more than 40 mm; the flesh of the impacted side of (ii) Middle thorax rib not less than 39 the seated dummy tangent to a mm and not more than 45 mm; vertical plane located within 10 mm of (iii) Lower thorax rib not less than 35 the side edge of the bench as shown in mm and not more than 43 mm; Figure V6–A, while the midsagittal (2) Peak acceleration of the upper plane of the dummy is in vertical ori- spine (T1) shall not be less than 13 g entation. and not more than 17 g and the lower (4) Push the dummy at the knees and spine (T12) not less than 7 g and not at mid- of the upper torso with more than 11 g; just sufficient horizontally oriented (3) Peak impactor acceleration shall force towards the seat back until the not be less than 14 g and not more than back of the upper torso is in contact 18 g. with the seat back. (5) While maintaining the dummy’s [71 FR 75370, Dec. 14, 2006, as amended at 74 position as specified in paragraphs FR 29895, June 23, 2009]

145

VerDate Mar<15>2010 10:10 Dec 13, 2010 Jkt 220218 PO 00000 Frm 00155 Fmt 8010 Sfmt 8002 Y:\SGML\220218.XXX 220218 wwoods2 on DSK1DXX6B1PROD with CFR