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A gas turbine engine fuel injector conduit includes a single feed strip having a single bonded together pair of lengthwise extending plates. Each of the plates has a single row of widthwise spaced apart and lengthwise extending parallel grooves. Opposing grooves in each of the plates are aligned for

A gas turbine engine fuel injector conduit includes a single feed strip having a single bonded together pair of lengthwise extending plates. Each of the plates has a single row of widthwise spaced apart and lengthwise extending parallel grooves. Opposing grooves in each of the plates are aligned forming internal fuel flow passages through the strip from an inlet end to an outlet end. The feed strip includes a substantially straight middle portion between the inlet end and the outlet end. In one alternative, the middle portion has a radius of curvature greater than a length of the middle portion. The feed strip has at least one acute bend between the inlet end and the middle portion and a bend between the outlet end and the middle portion. The feed strip has fuel inlet holes in the inlet end connected to the internal fuel flow passages.

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A gas turbine engine fuel injector conduit includes a single feed strip having a single bonded together pair of lengthwise extending plates. Each of the plates has a single row of widthwise spaced apart and lengthwise extending parallel grooves. Opposing grooves in each of the plates are aligned for

A gas turbine engine fuel injector conduit includes a single feed strip having a single bonded together pair of lengthwise extending plates. Each of the plates has a single row of widthwise spaced apart and lengthwise extending parallel grooves. Opposing grooves in each of the plates are aligned forming internal fuel flow passages through the strip from an inlet end to an outlet end. The feed strip includes a substantially straight middle portion between the inlet end and the outlet end. In one alternative, the middle portion has a radius of curvature greater than a length of the middle portion. The feed strip has at least one acute bend between the inlet end and the middle portion and a bend between the outlet end and the middle portion. The feed strip has fuel inlet holes in the inlet end connected to the internal fuel flow passages. rst and second belt pulleys; a conditioner drive shaft being coupled to said first stub shaft; said second stub shaft forming an input shaft of a hydraulic pump; and first and second hydraulic motors being respectively mounted for driving said third converging drum shafts at the opposite sides of said platform and being hydraulically coupled for receiving working fluid from said hydraulic pump. 4. The crop harvesting platform as defined in claim 3 and further including a control element for selectively controlling the speed of said motors whereby the speed of operation of said second and third converging drums at each side of said platform may be selected. et al.; US-5781981, 19980700, Weder et al.; US-5782062, 19980700, Weder et al.; US-5813194, 19980900, Weder, 053/399; US-5813198, 19980900, Weder et al.; US-5839256, 19981100, Weder et al.; US-D404684, 19990100, Shea, D11/164; US-5890343, 19990400, Weder et al.; US-5913799, 19990600, Weder et al.; US-5921060, 19990700, Straeter; US-5924241, 19990700, Hodge, 047/072; US-5941020, 19990800, Weder, 047/072; US-5966866, 19991000, Ferguson, 047/041.01; US-5974730, 19991100, Chien, 047/041.01; US-5974765, 19991100, Weder et al.; US-5991999, 19991100, Weder; US-D419436, 20000100, Celtorius et al., D09/305; US-6009665, 20000100, Weder; US-6009687, 20000100, Weder, 053/399; US-6014852, 20000100, Weder et al.; US-6047524, 20000400, Weder, 053/399; US-D424972, 20000500, Ferguson, D11/143; US-6080453, 20000600, Weder et al.; US-6082045, 20000700, Weder et al.; US-6098336, 20000800, Ferguson, 206/423; US-6101788, 20000800, Weder et al.; US-6101789, 20000800, Weder et al.; US-6112500, 2000090