146 results about "Right flank" patented technology

A vertical take-off and landing aircraft includes a fuselage, a left wing, a right wing, at least one forward thruster, a horizontal stabilizer and a vertical stabilizer. The left and right wings extend from substantially a middle of the fuselage on left and right sides, respectively. The at least one forward thruster is preferably mounted to the fuselage, substantially behind the left and right wings. The horizontal stabilizer extends from a rear of the fuselage. The vertical stabilizer extends from a top of the fuselage at a rear thereof. At least two left lift rotors are retained in the left wing and at least two right lift rotors are retained in the right wing. A second embodiment of the VTOL aircraft includes a fuselage truncated behind the left and right wings with a twin tail empennage.

A communication device holder for vehicles includes an upper cover and a lower cover cooperating with the upper cover; a left wing member and a right wing member, which are horizontally displaceable, are disposed in between the upper cover and the lower cover; one end of the left wing member is formed with at least one clamping jaw, and the other end of the left wing member is formed with a horizontal rack; one end of the right wing member is formed with at least one clamping jaw, and the other end of the right wing member is formed with the horizontal rack and at least one raised portion, and the raised portion is connected with a post formed on the upper cover through a spring; the spring pushes the right wing member to displace towards the outside of the upper cover.

A method of and system for moving an agricultural implement between a folded, inoperative system for transport and an extended, field position is provided. The method includes the steps of providing an agricultural implement having a right wing of tools and a left wing of tools each located on opposite sides of a central longitudinal axis of the implement relative to each other; moving one of the right and left wings of tools from an extended position to a folded, inoperative position for transport; and moving the other of the right and left wings of tools from an extended position to a folded, inoperative position for transport after the step of moving one of the right and left wings.

A roof airbag device includes an outer cushion and an inner cushion. The outer cushion includes a left wing part and a right wing part, which are oppositely disposed about the passenger's head, an upper cushion part connecting the left and right wing parts, and an outlet hole through which an inflation gas from an inflator is transferred. The inner cushion is disposed between the left and right wing parts, and has an inlet hole through which the inflation gas is supplied, and a discharge hole through which the inflation gas is discharged.

A forwardly folding agricultural implement frame includes a tongue having a forward section and a rearward section telescopically extendable relative to the forward section. A carriage having support wheels is mounted on the forward tongue section. Left and right wings are pivotally connected to the rearward tongue section and foldable between a field position wherein the wings are generally perpendicular to the tongue and a transport position wherein the wings are generally parallel to the tongue. During the folding process, the carriage remains generally centered under the frame such that the majority of the weight of the implement is carried by the wheels and not shifted forwardly to the tractor drawbar.

The invention discloses a backlash-free double rollers enveloping worm gear, a worm wheel of the transmission mechanism comprises two half worm wheels, the rollers are uniformly distributed in circumferential direction of each half worm wheel, the rollers rotate on the rotation axes; the two rows of rollers are arranged alternatively, wherein, one row of the rollers are engaged with left flank of the worm, the other row of rollers contact the right flank of the worm; the left and right flanks of the worm are respectively enveloped by rollers which are arranged at appropriate positions on the top and bottom of the main plane; through the adjustment of the mounting positions of the two half worm wheels, the rollers can always be in contact with the flank of the worm ,so as to achieve no backlash transmission. The transmission mechanism eliminates the return error of the transmission, makes the transmission smooth and improves the accuracy of transmission. The invention has the advantages of simple structure, easy manufacture, low cost and good economy, is a novel worm transmission device combining precision transmission and power transmission, is capable of being used for precision indexing, precision transmission and precision power transmission.

The invention relates to an electric double-track wheel type flaw detection car. The electric double-track wheel type flaw detection car comprises a car frame, a detection device, a power supply device, a left scanning device, a right scanning device, a left driving wheel, a left driven wheel, a right driving wheel, a right driven wheel, a left coupling device and a right coupling device. The car frame comprises a car body, a left wing, a right wing, a motor assembly, a left extension coupler, a right extension coupler, a left guiding shaft, a left guiding sleeve, a right guiding shaft, a right guiding sleeve, a left guiding device and a right guiding device. The detection device, the power supply device, the motor assembly, the left guiding sleeve and the right guiding sleeve are arranged on the car body; the left driving wheel, the left scanning device, the left coupling device, the left driven wheel, the left guiding device, the right driving wheel, the right scanning device, the right coupling device, the right driven wheel and the right guiding device are arranged on the left wing and the right wing. The flaw detection car is convenient to arrange, disassemble and convey, and can be manually put away and extended, the detection accuracy is improved and the cost is low.

Infant and preemie swaddling wraps including a kite-shaped body defining head and body supporting portions, a bottom flap and opposing right and left wings configured to be folded around the infants torso, a plurality of hook-and-loop fasteners attached to the body at a plurality of positions for releasably engaging with other positions on the kite-shaped body to maintain the folded configuration, and padding in the head and body portions.

A foldable pedal assembly includes: a pedal frame formed with left and right studs opposite to each other in an axial direction; a crank-connecting part including left and right wing units that define left and right recesses, respectively, the left and right studs extending into the left and right recesses and being pivoted to the left and right wing units, respectively; left and right urging members disposed in the left and right recesses to urge the pedal frame in a first direction transverse to the axial direction, and to urge the crank-connecting part in a second direction opposite to the first direction; a first limiting unit abutting against at least one of the left and right studs by urging action of the urging members; and a second limiting unit abutting against at least one of the left and right wing units by urging action of the urging members.

Poultry wings are suspended by their tip segments and oriented so that their outside surfaces face one side of the processing path, with right wings oriented with their elbows leading, and left wings oriented with their elbows trailing. The lower, primary segments are bent at the elbow joints by a bending guide, laterally and upwardly about an elbow guide, opening the elbow joints. The open joints are cut so as to release the primary segments. The mid-wing segments are compressed and the bone ends are moved laterally from the wing tip segments, causing the bone ends of the mid-wing segments to pop out of the tip segments. In both instances, the bones of the segments are exposed in the final products, so when the products are cooked, the exposed bone ends are free of grease, etc. and are suitable for grasping by the fingers of the hand for eating as finger food.

Poultry wings are suspended by their tip segments and oriented so that their outside surfaces face one side of the processing path, with right wings oriented with their elbows leading, and left wings oriented with their elbows trailing. The lower, primary segments are bent at the elbow joints by a bending guide, laterally and upwardly about an elbow guide, opening the elbow joints. The open joints are cut so as to release the primary segments. The mid-wing segments are compressed and the bone ends are moved laterally from the wing tip segments, causing the bone ends of the mid-wing segments to pop out of the tip segments. In both instances, the bones of the segments are exposed in the final products, so when the products are cooked, the exposed bone ends are free of grease, etc. and are suitable for grasping by the fingers of the hand for eating as finger food.

A roll-up patient-evacuation mattress has a bottom sheet having a head end and a foot end. A mattress is disposed above the bottom sheet. A patient support sheet is disposed above the mattress, and has a left wing and a right wing which are dimensioned to respectively enclose at least portions of left and right sides of a patient lying on the patient support sheet. A foot section is coupled to the bottom sheet and is dimensioned to substantially enclose the patient-evacuation mattress when the bottom sheet, the mattress, and the patient support sheet are rolled from the head end to the foot end in a direction substantially parallel to a longitudinal axis of the patient-evacuation mattress into said foot section.

A forwardly folding tool bar which may be moved between field and transport positions. The tool bar includes a center tool bar section having a hinged telescopic tongue extending forwardly therefrom for connection to a tractor. Right and left wrap-around winglet tool bar sections are pivotally secured to the right and left ends of the center tool bar section and are pivotally movable between field and transport positions. Right and left wing hinges are also pivotally secured to the center tool bar section. Right and left intermediate hinge sections are pivotally secured to the outer ends of the right and left hinge sections, respectively. Right and left outer hinge sections are pivotally secured to the outer ends of the right and left intermediate hinge sections. Inner, intermediate and outer tool bar sections are secured to each of the inner, intermediate and outer hinge sections.

An external frame backpack comprising two spaced-apart substantially rigid frame side posts, a substantially rigid cargo shelf integrally connected to the side posts, a substantially rigid upper cross member secured between the side posts, a substantially rigid lower hip plate secured between the side posts, and a flexible hip belt rigidly fastened to the hip plate. In another aspect disclosed herein, the hip belt comprises left and right wings, each wing fastened to the hip plate through at least two vertically separated apertures defined by the hip plate.

An aircraft that is enable to turn in a desired direction, and a method for controlling the flight direction of an aircraft, by employing differential drag on the respective wings. A control means that receives a control signal indicating a left turn increases the incidence angle on the left wing and reduces it on the right wing. For a right turn the opposite action is performed. The aircraft comprises airfoils that have increased drag as the incidence angle increases but have a generally constant lift.

Quadribalanced digital time displays and methods comprising increasing digital minutes displayed on the right flank of centrally positioned digital present hours, in relatively upper and lower positions during the first and second quarter hours, followed by decreasing digital minutes displayed on the left flank of digital next hours, in relatively lower and upper positions during the third and fourth quarter hours, are enhanced by simultaneously displaying markers in one or more of the three quarter hour minute positions not containing digital minutes at any one time to inform the viewer that such marked positions are functional elements of the display but not activated due to the current time being displayed in another of said minute positions at that time.

A method of and system for moving an agricultural implement between a folded inoperative system for transport and an extended, field position is provided. The method includes the steps of providing an agricultural implement having a right wing of tools and a left wing of tools each located on opposite sides of a central longitudinal axis of the implement relative to each other; moving one of the right and left wings of tools from an extended position to a folded, inoperative position for transport; and moving the other of the right and left wings of tools from an extended position to a folded, inoperative position for transport after the step of moving one of the right and left wings.

The invention relates to the technical field of layout design of unmanned plane systems, specifically to an unmanned plane system combined with all-wing oblique wing planes by using a wingtip connecting / towing technology. The unmanned plane system is composed of the plural identical all-wing unmanned planes which are connected in parallel through a wingtip-coupling mode. Wings and an engine of each unmanned plane can rotate relative to each other around a rotating shaft in the horizontal direction. The wingtip-coupling mode is that the left and right wingtips of each all-wing unmanned plane are provided with corresponding wingtip coupling and towing mechanisms, and every two coupled all-wing unmanned planes are only capable of doing relative movements of rotating around a coupling shaft. The system can increase the lift-drag ratio effectively and enable each unmanned plane to achieve a longer flying range and better endurance. Moreover, the flight capabilities in a middle-low speed zone, a subsonic speed zone, and an ultrasonic speed zone are all taken into account. When necessary, the in-flight detachment or recombination of the planes can be realized according to the actual situations, such as task requirements or atmospheric conditions.

The invention provides a post-rolling control cooling process for hot-rolled H-shape steel. The hot-rolled H-shape steel enters a cooling device after the rolling is finished, an upper nozzle and a lower nozzle are respectively aligned with upper / lower R parts of the hot-rolled H-shape steel to carry out water spray cooling, and a left nozzle and a right nozzle are respectively aligned with left / right flank centers of the hot-rolled H-shape steel to carry out water spray cooling. The invention is characterized in that the pressure of cooling water is within 0.7 to 1.2MPa, the water quantity is within 1,200 to 2,000m3 / hour, the cooling rate is within 75 to 150 DEG C / s and the cooling time is within 3 to 5 seconds; and the hot-rolled H-shape steel is cooled to 20 to 30 DEG C above the martensitic phase transformation point of the corresponding steel grade after the rolling under the temperature of 850 to 1,000 DEG C is finished. By adopting the cooling process in the invention, the actual grain size of ferrite at the core part of the hot-rolled H-shape steel can be refined from 8-10 grades to 10-12 grades, and a tissue of bainite plus sorbite can be formed on the surface of the hot-rolled H-shape steel, thereby obviously improving the strength and toughness of the hot-rolled H-shape steel and improving the yield strength of the hot-rolled H-shape steel by more than 70MPa.

A body worn hosiery / shaper uplifts the rear buttocks in an expandable thin material region, by virtue of respective left and right flank members, which cause the uplifting of the rear buttocks region. The flank members are supported from above by an annular upper waist knitted in welt, that extends circumferentially around the upper rib area. Upper thigh ring cuff portions also help with the uplifting of rear buttocks region from below while the high waisted control top control stomach and back side bulge. The body worn hosiery / shaper also optionally provides sheer leg portions that end just before the toes leaving the toe portion open. An extra wide open crotch double gusset is also provided allowing the user to utilize the restroom when nature calls.

A head and neck restraint device controls the motion of the head and forces exerted upon the neck of a seated occupant in a decelerating vehicle. A body defines a collar, right and left legs and right and left wings. The collar is tethered to the helmet. Each leg has belt interaction surfaces that provide a friction action on the shoulder straps. Left and right extensions or wings residing under the shoulder strap rearward of the legs provide a restriction of rotation of the body and thus a binding action on the shoulder straps. A cantilever action is induced in generally forward impact by the tethers pulling on the collar of the body and the binding action on the shoulder straps reducing the forward motion of the body. The present restraint device does not attach to the structure of the vehicle, allows travel thereof with respect to the seated occupant, yet controls the motion of the occupant's head in order to substantially reduce neck loads on the occupant. Moreover present restraint device is not in contact with the occupant during normal operation and thus does not induce discomfort or fatigue. Under general forward impact conditions, the occupant's head motion is controlled with respect to the torso, yet the device will restrictively move with the driver's head and torso along shoulder straps of a seat harness of the vehicle.

A writing instrument comprising a tubular body having an upper end, a lower end having left and right sides, and a point end; left and right wings, each wing among the left and right wings having proximal and distal ends; hinges interconnecting the left and right wings and the tubular body, the hinges respectively positioning the left and right wings' proximal ends at the left and right sides of the tubular body's lower end, and the hinges being adapted for respectively leftwardly and rightwardly extending the left and right wings' distal ends; and a ballpoint pen assembly operatively associated with the tubular body's point end.

An electromagnetic driven micro ornithopter comprises a body, a piston cylinder, an AC power supply, upper and lower electromagnetic coils, a permanent magnet, left and wing motion bars, left wing and right wing rotation shafts, left wing and right wing frameworks and left wing and right wing fins, wherein the piston cylinder and the AC power supply are internally arranged in the frame of the body; the upper and lower electromagnetic coils are arranged at the upper and lower ends of the piston cylinder respectively; the AC power supply is connected with the upper and lower electromagnetic coils; a permanent magnet sleeve is positioned in the middle part of the piston cylinder; the permanent magnet is internally arranged in the permanent magnet sleeve; one end of the left motion pole and one end of the right motion pole are fixed to the left side and the right side of the permanent magnet sleeve and the other end of the left motion pole and the other end of the right motion pole are fixedly to the left wing rotation shaft and the right wing rotation shaft; the left wing rotation shaft and the right wing rotation shaft are fixed to the ends of the left wing framework and the right wing framework; and the right ends of the left wing fins and the left ends of the right wing fins are fixed to the left wing framework and the right wing framework respectively. According to the invention, the upper and lower electromagnetic coils are used for providing magnetic force, so that the flapping power output is doubled. The defect that the magnetic force of a single coil may be influenced by the travel distance is made up and the power output becomes more stable.

A urine bag, which is folded flat so that it is compact and ready for use, has a water impermeable bag portion and a flexible mouse portion secured at an upper opening of the bag portion. The flexible mouse portion surrounds at least a portion of the upper opening of the mouse portion and has shape preserving capability. The mouse portion includes left and right wings which can be displaced around a first central folding line to open or close the upper opening, and left and right tongues. The tongues can be displaced together with the wings around a second central folding line which is an extension of the first central folding line. The mouse portion also has a pair of symmetrical folding lines extending diagonally from the intersection of the contour of tongues and the upper edges of the wings to the first central folding line.

A flying toy capable of moving by flapping of wings includes an actuation mechanism, for the wings, comprising a crank drive rotated by a means providing the driving force, two flexible wings arranged symmetrically with respect to the vertical plane of symmetry of the toy and connected, at the wing bases, to the actuation mechanism. The wing bases are mounted oscillating about axes arranged on both sides of the vertical plane of symmetry of the toy. The toy includes a control means, that receives a control signal indicating a left turn, increases the tension on the right wing and reduces it on the left wing. For a right turn, the opposite action is performed.

A horseshoe with splaying and flexibility features has a U shaped compliant metallic unitary body having left and right wings and a central toe area integral with the body, and a compliant leaf-spring formation disposed proximate to or as part of the toe area. The leaf spring is arch shaped and resiliently deforms and exerts horizontal pressure sideways on the left and right wings thus splaying the left and right wings. The arch shape forms a cavity which is optionally filled with a resilient material, e.g., polyurethane, to prevent accumulation of debris in the cavity. Contiguous serrations on the left and right wings provide relative vertical flexibility of the left and right wings. The splaying and flexibility enhance horse-hoof comfort and hoof-structure re-generation. The horseshoe may be cast / forged, blanked, or welded or produced by mechanical joining. Hardened stainless steel or Titanium, or other material may be used for the horseshoe.

The spacecraft structure is provide, the spacecraft structure for the spacecraft includes, a center fuselage, right wing side fuselage, left wing side fuselage, front wings, and rear wings of Arch-Wings, vertical winglets, and the first levels, the fuselage has a cross-section of substantially flat floor fuselage shape, being is wide enough to provide lifting force.The front wings of the Arch-Wings are disposed horizontally in rear portions of the fuselage the vertical winglets are disposed the top of the rear fuselage the first level disposed fuel tank storage, plurality of landing gear bays, cockpit with control panel, various avionic instruments, cabin doors.The top of the rear fuselage disposed jet-power plants and further more at compartment of the Arch-Wings disposed rocket power plants.The fuselage provide lifting force and the wings provides lifting force and steering force, he whole structure of spacecraft comprises carbon fiber honey comb composite molded structure which is makes the spacecraft lighter weight and shear strong.At the front portion of wing body compartment of the Arch-Wings comprises retro rocket power plant with covered door, and under belly of the Arch-Wings disposed pontoon systems which could provide float at sea port.