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262results about How to "Slide freely" patented technology

Universal stand for vehicle engines and gearboxes

A stand holding virtually any vehicle engine and gearbox respectively during repair and renovation allowing clear access to every side of thereof, carrying a base structure (1) an immovable column (7), a horizontal immovable tube (9), includes a movable support assembly (12) and a pair of rotatable adjustable carrier assemblies (20) being distanced from one another. The support assembly is capable of varying the distance between a pair of carrier assemblies to correspond with the size of engine and of gearbox respectively. Each of the pair of carrier assemblies including an arm and a carrying plate connected by way of the connecting member; rather two handles adjustably coupled to corresponding carrying plate by first ends and having bolts threaded through second ends and corresponding adapters for receipt within corresponding holes of engine and gearbox respectively. The arms rotatably and adjustably threaded through horizontal tube (9) and horizontal support member (18) respectively such that carrier assemblies being positioned inside of the device between column (7) and vertical support member (17) to hold engine and gearbox respectively to allow clear access to every side of engine and gearbox, respectively. The arms have a plurality of holes to adjust the distance between column (7) and vertical support member (17) respectively and engine and gearbox respectively.
Owner:NIKOLIC LJUBOMIR

Continuously variable belt drive system

A belt-type continuously variable transfer system (15) includes a driving pulley assembly (20), a driven pulley assembly (22) and a V-shaped belt (24) engaged to transfer rotary power therebetween. The driven pulley assembly (22) can include a ratio adjustment mechanism (46) that adjusts the position of a rear sheave (40) relative to a forward sheave (42). The adjustment mechanism (46) includes a motor (170) and a worm gear mechanism (171, 172) that rotates an actuation screw (154). Rotation of the actuation screw (154) is reacted by a split nut (158) so that as the screw (154) rotates is translated along the axis (B) of the driven pulley assembly (22). Translation of the actuation screw (154) exerts pressure against the rear sheave (40) to push it toward the forward sheave (42), thereby altering the drive ratio of the pulley assembly. In one feature, the driven pulley assembly (22) includes a fail-safe mechanism (48) that operates when power is supplied to the motor (170) to hold the split nut (158) together. Once power is disrupted, the fail-safe mechanism (48) allows the components (1 58a-c) of the split nut (158) to be separated, disrupting the threaded engagement with the actuation screw (154). At this point, the actuation screw (154) is driven forward by a compression spring (190), thereby driving the rear sheave (40) forward to a predetermined drive ratio position. In another aspect of the invention, the driving pulley assembly (20) includes an idler pulley portion (65) radially inboard from the normal driving sheave surface (29, 31). As the belt speed decreases, the belt (24) migrates downward within the driving pulley assembly (20) until it falls within the idler pulley portion (65). At this point, the belt (24) is isolated from the rotation of the driving pulley assembly (20). The driving pulley assembly (20) also includes a belt tensioning mechanism (32) that maintains proper belt tension at all speeds and drive ratios. The tensioning mechanism (32) relies upon a pivotably mounted centrifugal weight arm (101) to provide tensioning as a function of speed. A compression spring (80) provides axial pressure to maintain belt tension over all drive ratios. The spring (80) acts against a specially curved cam edge (92) on a pivoting lever arm (90), which arm (90) transfers an axial force to the rear sheave (28) of the driven pulley assembly (20).
Owner:BORGWARNER INC

Satellite navigation and inertial measurement combined orbit measuring system and method

The invention discloses a satellite navigation and inertial measurement combined orbit measuring system and method. The satellite navigation and inertial measurement combined orbit measuring system comprises a measuring unit and a data post-processing unit. The measuring unit comprises two satellite navigation and inertial measurement combined orbit measuring devices which are placed on two monorails. A drawing device draws a satellite navigation and inertial measurement combined system to perform real-time online measurement, record original data of a dual-rail geometrical state and an equipment running state and perform offline processing through the data post-processing unit. The satellite navigation and inertial measurement combined orbit measuring method comprises performing preprocessing on original measurement data; establishing a directional mileage measurement curve and an ideal curve; calculating absolute and relative irregularity of a rail direction; establishing a slope angle mileage measurement curve and a slope angle ideal curve; and calculating absolute and relative irregularity of the height. According to online data collection, an offline data processing mode and a dual-rail parallel measuring mode, external geometrical information and internal geometrical irregularity of orbits are determined.
Owner:SAFEWAY XIAN NAVIGATION TECH
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