Vehicle-mounted missile launching single-side flow director and launching vehicle with same
A missile launch and deflector technology, applied in the direction of the launch device, etc., can solve the problems of reducing the impact force of the gas flow on the deflector, damage, weak shear resistance of the hydraulic outriggers, etc., so as to reduce the risk of damage and reduce the Shear force, the effect of improving reliability
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Embodiment 1
[0033] see figure 1 As shown, the embodiment of the present invention provides a vehicle-mounted missile launching single-sided deflector, including:
[0034] The flow guide part 1, the flow guide part 1 includes a downwardly concave arc-shaped main profile 11, and connecting surfaces 12 respectively connected to both sides of the head and tail of the main profile 11, the main profile 11 A plurality of convex lines 13 are arranged at intervals on the upper surface of the upper surface, and the plurality of convex lines 13 run through the entire main surface 11 in a transverse direction;
[0035] A bracket 2 for supporting the deflector 1, and the bracket 2 is detachably connected with the launching platform.
[0036] The vehicle-mounted missile launch single-sided deflector of the present invention adopts a plurality of convex lines 13 on the downwardly concave arc-shaped main profile 11. When the vehicle-mounted missile is launched, a part of the missile gas flow injected do...
Embodiment 2
[0043] see figure 1 and figure 2 As shown, the embodiment of the present invention provides a vehicle-mounted missile launching single-sided deflector, including:
[0044] The flow guide part 1, the flow guide part 1 includes a downwardly concave arc-shaped main profile 11, and connecting surfaces 12 respectively connected to both sides of the head and tail of the main profile 11, the main profile 11 A plurality of convex lines 13 are arranged at intervals on the upper surface of the upper surface, and the plurality of convex lines 13 run through the entire main surface 11 in a transverse direction;
[0045] A bracket 2 for supporting the deflector 1, and the bracket 2 is detachably connected with the launching platform.
[0046] The vehicle-mounted missile launch single-sided deflector of the present invention adopts a plurality of convex lines 13 on the downwardly concave arc-shaped main profile 11, and the direction of the arrow in the figure is the gas flow injection di...
Embodiment 3
[0049] see figure 1 and image 3 As shown, the embodiment of the present invention provides a vehicle-mounted missile launching single-sided deflector, including:
[0050] The flow guide part 1, the flow guide part 1 includes a downwardly concave arc-shaped main profile 11, and connecting surfaces 12 respectively connected to both sides of the head and tail of the main profile 11, the main profile 11 A plurality of convex lines 13 are arranged at intervals on the upper surface of the upper surface, and the plurality of convex lines 13 run through the entire main surface 11 in a transverse direction;
[0051] A bracket 2 for supporting the deflector 1, and the bracket 2 is detachably connected with the launching platform.
[0052] The vehicle-mounted missile launch single-sided deflector of the present invention adopts a plurality of convex lines 13 on the downwardly concave arc-shaped main profile 11. When the vehicle-mounted missile is launched, a part of the missile gas fl...
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