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An improved support bracket for supporting electronic devices provides improved adjustability and alignment. The support bracket includes a front surface and a rear surface each including a portion having at least one threaded hole and a support portion between the front surface and rear surface for

An improved support bracket for supporting electronic devices provides improved adjustability and alignment. The support bracket includes a front surface and a rear surface each including a portion having at least one threaded hole and a support portion between the front surface and rear surface for supporting an electronic device. The support bracket includes a side portion having a mechanism for coupling the side portion to a structure, a guide portion and a support portion for supporting an electronic device.

대표청구항 ▼

An improved support bracket for supporting electronic devices provides improved adjustability and alignment. The support bracket includes a front surface and a rear surface each including a portion having at least one threaded hole and a support portion between the front surface and rear surface for

An improved support bracket for supporting electronic devices provides improved adjustability and alignment. The support bracket includes a front surface and a rear surface each including a portion having at least one threaded hole and a support portion between the front surface and rear surface for supporting an electronic device. The support bracket includes a side portion having a mechanism for coupling the side portion to a structure, a guide portion and a support portion for supporting an electronic device. surface at other side for cooperating with the coupling grooves to allow the clutch disk to be reversely rotated and a plurality of third coupling projections or concaved grooves formed at the positions facing to the second coupling projections on one side surface of the reel for coupling with the second coupling projections. 2. The pretensioner integrated with the pyrotechnic gas generating apparatus according to claim 1, in which: at least three of the first coupling projections in the second chamber are positioned at different arc angles α, β, γ to be staggered from one another properly dividing the circumferential angle of 360° so that they are respectively inserted into preferable insertion position of the coupling grooves. 3. The pretensioner integrated with the pyrotechnic gas generating apparatus according to claim 1, in which: a small bearing and a pin are used to mount the pulley on the arm to freely rotate the pulley, thereby minimizing the friction of the cable on the pulley. 4. The pretensioner integrated with the pyrotechnic gas generating apparatus according to claim 1, in which: a weight is provided on the pulley to have an eccentricity so that the weight center of the pulley is slightly inclined toward one direction. 5. The pretensioner integrated with the pyrotechnic gas generating apparatus according to claim 1, in which: supporting grooves are formed on both sides of the pulley and supporting bars are fixed to positions corresponding to at least one predetermined length of the cable, thereby securing the exact traveling length of the cable. 6. The pretensioner integrated with the pyrotechnic gas generating apparatus according to claim 1, in which: the safety belt retractor further comprises a guider for guiding the safety belt being wound on or released from the reel, thereby smoothing the webbing due to the reverse-rotating of the reel upon the operating of the pretensioner. rd end of the stabilizer forms a predetermined angle tau with the leading edge for providing a forward sweep angle. When attached to a leading edge of a reaction body such as a leading edge flap or wing, the stabilizer will modify the behavior of a transonic shock. When the magnitude of the leading edge sweep angle is equal to the sweep back angle of the opposite wing, radar signature is minimized. In some applications the modification to the behavior of the transonic shock prevents abrupt wing stall phenomena and optimally minimizes radar detection signature. A vehicle such as an airplane, rocket or water borne ship may incorporate the stabilizer on any of its reaction surfaces including control surfaces and furthermore in any particular location to modify the behavior of the shock.