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2190 results about "Load carrying" patented technology

Load monitoring system and method utilizing transponder tags

A system 10 for monitoring the load on a load carrying vehicle comprises an electronic radio frequency (RF) identification system 22 comprising a reader 24 and a plurality of RF transponders 28.1 to 28.n. Each transponder is associated with a respective load item 36.1 to 36.n, and the items collectively constitute the load located in a load carrying region of the vehicle. The reader is operative in use to interrogate the transponders, to read response data received from the transponders and to generate data relating to a load change event. A controller 34 and a vehicle position data generating device 38 are connected to the controller. The controller is sensitive to a load change event and operative to record vehicle position related data corresponding to the load change event.
Owner:SUPERSENSOR

Load Bearing Bracket for Adjustable Gear Bags

InactiveUS20090014602A1Maximizes adjustabilityPassenger spaceRacks dispositionModularityEngineering
A load bearing bracket for adjustable gear bags comprises a base bracket having a plurality of openings disposed therein. The openings are arranged in columns and rows. A top row consists of uniformly sized openings and alternates with another row of uniformly but different sized openings. This arrangement maximizes adjustability when attaching a variety of holding items such as Modular Lightweight Load-carrying Equipment (MOLLE) bags or other equipment bags or holders. The base bracket is mounted using bolts, rivets or other fasteners to a vehicle. The equipment bags have an attached strap that fits within the openings to secure them therein. A plurality of large adjustment openings are disposed along a bottom portion of the base bracket allowing a user to insert a hand to guide and secure the straps. A snap on the bottom of the strap secures the free end of the strap to the bag.
Owner:FROST ANDREW MEYER

Non-pneumatic tire with annular spoke reinforcing web

A non-pneumatic tire is provided with an annular reinforcing web that reduces the bending of compression spokes formed in the tire and reduces stresses and strains in the tire. The non-pneumatic tire includes an inner hoop member having an inner surface that defines the inner diameter of the tire, and an outer hoop member having a tread groove region that defines the outer diameter of the tire. A disc-shaped central web portion connects the inner and outer hoop members. A plurality of elongated, radially aligned cavities on either side of the central web defines integrally-formed compression spokes which connect the inner and outer hoop members. The annular reinforcing web is located on and affixed to either side of the central web portion and interconnects a mid portion of each spoke to a mid portion of the spokes on either side of it. Preferably, the annular reinforcing web is reinforced with fiber webbings on its outer side for added strength. The annular reinforcing web allows the tire to be made with less polyurethane material with no reduction in load carrying capability.
Owner:CATERPILLAR INC

Shield construction method for three-line parallel under-passing trunk railway tunnel

The invention discloses a shield construction method of digging three parallel tunnels under a trunk railway, which belongs to the field of tunnel construction technology. The construction method of the invention comprises the procedure that: the model analysis on each construction sequence and method is made by a three-dimensional finite element and the shield construction sequence is selected; to select the reinforcement project of the railway bed is selected according to the influence degree of the dynamic stress, the load-carrying structural model is adopted to calculate and decide the shield area reinforcing bars enhancement project under the dynamic load of the railway train; the construction parameters are selected according to the test results and the performance of the shield machine, the front earth pressure is reasonably set , the synchronizing mortar injection is enhanced, the forward digging speed and the axis deviation are strictly controlled, the secondary mortar injection is made, the foam or mud is filled by utilizing a pre-embedded injection hole; the strict monitoring measures to monitor the shield construction process is adopted so that the construction unit can adjust the construction parameters in time and guarantee the construction safety. The invention not only guarantees the construction quality and the construction safety of the project but also creates good economic benefit.
Owner:CHINA RAILWAY NO 2 ENG GRP CO LTD

Main load-carrying structure of spacecraft

The invention discloses a novel aircraft main bearing structure, comprising a pushing cabin structure, a star-shaped truss structure (6) and an electronic cabin main framework structure; the upper part of the propelling cabin structure is connected with the electronic cabin main framework and the lower part thereof is taken as a whole star precision detection benchmark surface and an installation surface used for the propelling cabin instruments; the star-shaped truss structure (6) is a load installation frame supported by a supporting rod and arranged in the electronic cabin main framework structure and used for installing effective loads; the lower end of the supporting rod is fixedly connected with the upper part of the propelling cabin structure; as the main bearing structure adopts an external framework side plate structure and an internal start-shaped truss structure to form a mixed main structure with dual bearing paths (internal bearing path and external bearing path) so as to transmit the whole star load, the force transmission path is short and continuous, the structure is compact, the center of mass is low, and the main bearing structure meets the requirement of the whole satellite of high rigidity and small inertia.
Owner:AEROSPACE DONGFANGHONG SATELLITE

Structural joint connection providing blast resistance and a beam-to-beam connection resistant to moments, tension and torsion across a column

ActiveUS20050204684A1Mitigates likelihood of progressive collapseTremendous tensile pull and vertical moment demandBuilding roofsFloorsGusset plateEngineering
At a beams-to-column joint connection of two beams to a column, in which the joint connection comprises both a gravity load-carrying connection and a moment-resisting connection, there is added a beam-to-beam connection across the column, using two gusset plates, facing each other, on opposite sides of the joint connection. The gusset plates, which are not connected to the column in a moment-resisting connection, connect the two beams, in a tension and moment-resisting connection with respect to each other, by longitudinal welds between the gusset plates and the beams, and provide the capability of withstanding disastrous events, including loss of column support and/or loss of integrity of the beams-to-column joint connection and severe torsional and lateral inelastic deformation due to direct blast pressure. When subjected to such violent conditions and upon loss of column support, and, the likely loss of integrity of the beams-to-column joint connection, the two beams and two gusset plates provide independent beam-to-beam structural continuity, causing the two beams to act as one long beam, or, in other words, a “double-span” condition is created. Such beam-to-beam connection is capable of carrying the tension, torsional and moment loads placed upon the beams, to the ultimate capacity of the beams. Inasmuch as a gusset plate is disposed on each side of the beams-to-column joint connections, substantial shielding of those connections against blast and impact forces is also achieved.
Owner:MITEK HLDG INC

Gas turbine component and a method for producing a gas turbine component

A gas turbine component includes an inner ring, an outer ring, and a plurality of circumferentially spaced struts which are rigidly connected to the inner ring and the outer ring forming a load-carrying structure. The component includes at least one fairing connected to two adjacent struts defining a gas channel between the struts and the fairing.
Owner:VOLVO AERO CORP
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