a fuselage longeron or frame
A deployable structure that may include a slit-tube longeron and a flat panel coupled with the slit-tube longeron.
The slit-tube longeron may include a tubular member having a slit that runs along the longitudinal length of the slit-tube longeron.
An essentially straight longitudinal beam section (3) is assembled with a separate longitudinal beam head (4).
An internally threaded bush which protrudes into the hollow space is welded to one of the sheet metal shells, thus allowing the chassis part to be screwed to the longitudinal beam.
The component carrier (10) has a longitudinal beam (50) with one or more support elements (59) which support one or more components (4) and which project laterally beyond the longitudinal beam (50).
At the intersection of a longitudinal beam and a transverse beam there is provided a plate-like fixing piece (5) separately fastened to both of the intersecting chassis beams and transferring the forces between the beams.
The invention is characterized in that the forward section (7) of the first bottom longitudinal beam (5) is less long than the forward section (7') of the second bottom longitudinal beam (6').
The first upper rail channel and the first lower rail channel are provided at a first depth and the second upper rail channel and the second lower rail channel are provided at a second depth.
A left vertical sidewall is defined between the left bottom rail and the left top rail.
The second vehicle frame rail is disposed a fixed distance from the first frame rail and is generally parallel to the first frame rail.
A right vertical sidewall is defined between the right bottom rail and the right top rail.
The device consists of a Roof-Rail, a Roof-Fitting, and Stirring Implements and where necessary may employ a food receptacle securing method.
tunnel side member closing sill panel
Each side member (1) has an opening (8) in which each end (9) of the crosspiece presses on the side member by means of suspension springs (16).
The device consists of a side member (10), two inclined posts (1).
Each side member is provided with at least one articulated linkage.
The support mount (20) is intended to be mounted at the end of a motor vehicle side member (12), this side member (12) comprising, in the continuation thereof, a mounting plate (14) for a transverse impact beam (16).
Said longitudinal member (7) is respectively formed with a free longitudinal member end (8).
The cross-member preferably extends between a left lateral longitudinal member and a right lateral longitudinal member.
A motor vehicle body according to the present invention has a longitudinal member and a bumper crossmember which is fixed on an end of the longitudinal member.
Between these, a central member (22) is secured to the longitudinal member (16), parallel to the cross-members (18), and a loading opening (46) is formed opposite said longitudinal member (22).
A device for elastically connecting a bumper support to a longitudinal member of a vehicle consists essentially of a spring body supported between the longitudinal member of the vehicle and the bumper support.
The composite material, the foam in the form of the stringer, and the plurality of structural members are cured to form the composite stringer.
The saddles (2) are pinned to the stringer by pins (10) that pass through the saddle skirts (and metal reinforcing of present) and the stringer.
A method and apparatus for manufacturing a composite stringer.
A further element (17) is provided at the lower end of the stringer (25) to mount the stringer on a ground surface and define a support for the lowermost step tread of the flight of steps.
A lap joint is preferably utilized wherein mandrel segments are split at the stringer centerline through the middle of the hat or through the cap of the stringer.
Each roof beam has an upper (5) and a lower (6) longitudinal girder.
An extension feed beam for a rock drill, comprising a lower beam (1), and an upper beam (2) mounted slidably with respect to the lower beam (1).
The seat base (2) extends between a front seat stay (4) on a front stay support (5) and a rear seat stay (6) on a rear stay support (7).
A body frame connection member connects a first side frame portion and a second side frame portion which constitute each side frame.
The torsion beam (23) is provided with front and rear beam wall sections (43, 44).
The arm (20) is composed of upper and lower rods (24, 26) extending parallel to each other.
The spar or preform can be used to provide a tubular main spar for a winglet.
A lower skin (20) of the winglet (5) is joined to the braided spar (10) and the lower front spar cap (18).
The tip section is mounted to a central blade section by mounting the tip spar to a main blade spar.
The upper and lower spar caps extend from the spar web only on the other side of the spar web to the fuel containment area.
An upper skin (19) of the winglet (5) is joined to the braided spar (10) and the upper front spar cap (17).
An upper skin of the winglet is joined to the braided spar and the upper front spar cap.
The spar bridge and the spar section have interlocking shapes by which rotation of the spar bridge in the spar section is prevented thereby preventing rotation of one of the blade sections relative to the other.
The yoke loosely receives the beam.
A lower skin of the winglet is joined to the braided spar and the lower front spar cap.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
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