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66results about How to "Small frontal area" patented technology

Accessory gearbox

InactiveUS20060248900A1Contributes minimally to engine weight and complexityImproving engine fuel burnEfficient propulsion technologiesGas turbine plantsEngineeringGas turbines
Provided is an accessory gearbox for a gas turbine engine that contributes minimally to engine weight and complexity. An accessory gearbox comprises a stationary frame that is circumferentially disposed about a central longitudinal axis of the engine. The frame includes a forward-directed axial face and a rearward-directed axial face for fastening the frame to the engine. A central bore accepts a rotational driving means and an outermost rim circumscribes the outer diameter of the frame. A compartment is located between the bore and the rim. At least one primary accessory is mounted to a face and proximate the compartment, remotely engaging the driving means and able to be driven concurrently therewith.
Owner:RAYTHEON TECH CORP

Intravascular stent

A medical device for use in the interior of a body lumen includes a balloon catheter and a radially expandable stent. The stent includes a plurality of zig-zags of a low memory metal formed into a hollow, open-ended cylindrical shape. The individual zig-zags have a curved portion forming a reversing bend which allows the zig-zags to expand and deform as the balloon radially expands the stent. The curved portions of the zig-zags are aligned along the length of the stent in a spaced-apart arrangement with some curved portions attached and others unattached to adjacent zig-zags. The resulting stent is longitudinally flexible throughout its length when unexpanded and is also capable of conforming to a bend in the body lumen when expanded.
Owner:MEDTRONIC INC

Flat paddle square tube propeller for ship crafts

The invention relates to a plate paddle square tube propeller for vessels, which is composed of a crank, a connecting bar, a connecting bar guide, plate paddles, an inner side fixing plate, an outer side fixing plate and two baffle plates. Motor drive is transmitted to the crank by a reducer casing, one end of the connecting bar does circular motion under traction of the crank, the other end does closed curvilinear motion similar to the profile of 'human ears', the middle of the connecting bar slides reciprocally in the connecting bar guide, the plate paddles do motion constantly and reciprocally 'flap and unfolding' similar to an insect in a square tube surrounded by the inner side fixing plate, the outer side fixing plate and two baffle plates under drive of the connecting bar, thereby Weis-Fogh effect is produced to propel a vessel to navigate. The plate paddle square tube propeller for vessels has simple structure, high efficiency and safety.
Owner:王志成

Special purpose small arms ammunition

A multi-piece projectile for a small arms cartridge includes a metal cup that has a bore, a plastic sheath having a through hole and a high-density core. The cup is a cylindrical metal structure having a bore. The sheath is a cylindrical end and a conical end and a through hole. The core is a cylindrical structure having conical end and a blunt end. The projectile is assembled by placing the core in the through hole of the sheath and then pressing the sheath into the bore of the cup. The assembled projectile is attached to the cartridge by crimping the cup to the orifice in the end of the cartridge casing after it is filled with the propellant. When the projectile is fired all of the components remain coupled together but break apart upon impact with a target. Because the core has a higher mass than the other components the components separate very easily, the majority of the kinetic energy remains in the core. Once separated from the other components, the core is able to penetrate through various protective materials.
Owner:XTEK

Special purpose small arms ammunition

A multi-piece projectile for a small arms cartridge includes a metal cup that has a bore, a plastic sheath having a through hole and a high-density core. The cup is a cylindrical metal structure having a bore. The sheath is a cylindrical end and a conical end and a through hole. The core is a cylindrical structure having conical end and a blunt end. The projectile is assembled by placing the core in the through hole of the sheath and then pressing the sheath into the bore of the cup. The assembled projectile is attached to the cartridge by crimping the cup to the orifice in the end of the cartridge casing after it is filled with the propellant. When the projectile is fired all of the components remain coupled together but break apart upon impact with a target. Because the core has a higher mass than the other components the components separate very easily, the majority of the kinetic energy remains in the core. Once separated from the other components, the core is able to penetrate through various protective materials.
Owner:XTEK

Low profile paintball loader mount

The invention is an improvement to an active paintball loader used to feed a supply of paintballs to the breech of a paintball marker wherein the loader is located remote from the marker breech to reduce the target profile of the paintball game player. The loader includes a conventional reservoir for storing a quantity of paintballs, a drive mechanism for moving individual paintballs out of the loader reservoir and into a feed tube where they are forced to the breech inlet of the marker. Locating the loader on the compressed gas storage cylinder reduces the frontal area of the marker / loader combination thereby reducing the target area of a competitor using the LRL during a paintball competition. The location also improves the balance of the combination marker, loader, gas cylinder apparatus making it easier for the player to handle during evasive maneuvers during paintball game play. The improved location of the loader relative to the breech inlet also allows use of a substantially straight feed tube which reduces the propensity for paintball rupture which reduces the chance that a paintball game player will be taken out of competition due to a paintball feed jam.
Owner:KULP DONALD LEE

Turbine wheel

A wind driven energy source is providing utilizing a turbine wheel comprising a peripheral rim attached to a central hub via a series of spokes. A plurality of airfoil blades are assembled to the wheel, each blade being secured to a pair of spokes and positioned proximate an interior edge of the rim and extend only partially down the length of the spoke. This provides a central opening allowing airflow through the innermost region of the wheel. The blades are pivotally assembled to the spokes and can include an incident angle adjusting mechanism as well as a breakaway feature.
Owner:FINNELL ALFRED W

Expansive soil slope and construction method

The invention discloses an expansive soil slope and a construction method. The slope toe angle of the slope is increased to steepen the slope, so that the slope surface water is mainly runoff when rain falls or water flows through to reduce seepage, and the moisture content in the expansive soil of the slope is controlled to be within a lower range to prevent the loss of stability due to expansion of the expansive soil after water absorption of the slope. According to the slope and the method, the varying slope of the expansive soil slope is 45-60 degrees to quicken the surface runoff of the rainwater; the surface of the slope is covered by a clay layer with thickness of 10 cm; fiber reinforcements with length of 20-25 cm are uniformly implanted into the surface of the slope and are exposed out of the clay layer for 3-5 cm; turfs of which roots develop well in the transverse direction but develop poorly in the longitudinal direction are planted on the clay layer.
Owner:宏盛建业投资集团有限公司

Alignment mark, making method and detection device thereof

The present invention discloses a method for making alignment mark, comprising: 1) etching an alignment mark on the back side of a silicon chip; and 2) deposing a layer of oxide-film on the alignmentmark. The invention also discloses an alignment mark made by the method, which is arranged on the back side of a silicon chip. In addition, the invention further discloses a detection device for alignment mark, which comprises a light source, the light emitted by the light source passes through a half transparent and half reflecting mirror, is focused by a first convex lens, passes through a holeon a carrier corresponding to the alignment mark on the back side of a silicon chip, is focused to the alignment mark on the back side of the silicon chip, and is reflected by the alignment mark, signal light sent by the alignment mark passes through the half transparent and half reflecting mirror, and is focused by a second convex lens, and finally an imaged is formed on the plane of the detection device. An alignment mark made by the method is on the back side of a silicon chip, occupying no use area of the front side of the silicon chip, and the method for detecting an alignment mark can beused for detecting the alignment mark.
Owner:SHANGHAI HUA HONG NEC ELECTRONICS

Compact high current, high efficiency laser diode driver

A device includes a u-channel shaped member and a printed circuit board including a plurality of capacitors. Each of the plurality of capacitors has a mounting surface mounted to the printed circuit board and an opposing heat transfer surface thermally coupled to the u-channel shaped member. The device also includes an output cable coupled to the printed circuit board and a return cable coupled to the printed circuit board. The device further includes a control transistor disposed inside the u-channel shaped member and a current sensing resistor disposed inside the u-channel shaped member.
Owner:LAWRENCE LIVERMORE NAT SECURITY LLC

Variable geometry lift fan mechanism

A vertical takeoff and landing aircraft includes rotors that provide vertical and horizontal thrust. During forward motion, the vertical lift system is inactive. A lift fan mechanism positions the fan blades of the aircraft in a collapsed configuration when the vertical lift system is inactive and positions the fan blades of the aircraft in a deployed configuration when the vertical lift system is active.
Owner:WISK AERO LLC

Special purpose small arms ammunition

A multi-piece projectile for a small arms cartridge includes a metal cup that has a bore, a plastic sheath having a through hole and a high-density core. The cup is a cylindrical metal structure having a bore. The sheath is a cylindrical end and a conical end and a through hole. The core is a cylindrical structure having conical end and a blunt end. The projectile is assembled by placing the core in the through hole of the sheath and then pressing the sheath into the bore of the cup. The assembled projectile is attached to the cartridge by crimping the cup to the orifice in the end of the cartridge casing after it is filled with the propellant. When the projectile is fired all of the components remain coupled together but break apart upon impact with a target. Because the core has a higher mass than the other components the components separate very easily, the majority of the kinetic energy remains in the core. Once separated from the other components, the core is able to penetrate through various protective materials.
Owner:XTEK

Variable incidence scramjet engine outboard cowl

The invention relates to a variable incidence scramjet engine outboard cowl, which comprises side walls and a fixed lower wall surface; two sides of the fixed lower wall surface are provided with the side walls; a turning axle arranged on a lip of the fixed lower wall surface is hinged with an adjustable lower wall surface under the fixed lower wall surface; and the adjustable lower wall surface deflects around the turning axle by the driving of a drive mechanism, and the deflection position of the adjustable lower wall surface is limited by a limiting and locking mechanism. In the variable incidence scramjet engine outboard cowl, the adjustable lower wall surface deflecting around the lip of the fixed lower wall surface is arranged under the fixed lower wall surface, and the change of aeroperformance of an aerocraft is realized by adjusting the incidence of the adjustable lower wall surface, so that the aerocraft obtains the optimal aeroperformance under different flight regimes.
Owner:INST OF MECHANICS - CHINESE ACAD OF SCI

Throwing material for lightening interception difficulty and protecting dikes of rivers

InactiveCN102330434AGood interception effectStrong underwater impact resistanceCoastlines protectionFoundation engineeringCofferdamEngineering
The invention discloses a throwing material for lightening interception difficulty and protecting dikes of rivers. The throwing material is a cylindrical line throwing material, the throwing material is provided with a lateral punched hole, rough ribs are arranged at the outer side of the cylinder, the incident flow end of the solid cylindrical line throwing material is provided with a streamline conical head, and the incident flow end of the hollow cylindrical line throwing material is provided with a thin-wall sharp edge. After the cylindrical line throwing material is thrown along the flow from the dike head at the difficult interception section of a cofferdam, the throwing material rolls around a shaft to the bottom of a slope; the throwing material reaches the deep groove part of a closure gap more easily compared with other bulk materials for intercepting the flow by means of sliding; the material has strong underwater impact resistance and low loss, can protect the dike from collapsing, and has the effect of obviously reducing the interception difficulty; and the throwing material can also be used for dike protection of rivers and slope protection and dike protection of reservoir earth and rockfill dams.
Owner:CHANGJIANG RIVER SCI RES INST CHANGJIANG WATER RESOURCES COMMISSION

Location grid rack provided with streamline low pressure drop runner, and fuel assembly

The invention discloses a location grid rack provided with a streamline low pressure drop runner. The location grid rack comprises a plurality of inner strip bands, and an outer strip band, wherein the plurality of inner strip bands intersect with one another, so that a latticed grid structure and a plurality of hollow grid units are formed; the outer strip band is arranged at the periphery of the grid structure in a surrounding way and is fixed together with the inner strip bands; rigid bulges are respectively fixedly arranged on the inner strip bands and extend towards the interiors of the grid units in a convex way; each rigid bulge comprises a plane and a side surface, wherein each plane is contacted with a fuel rod, and each side surface is smoothly connected between the plane and the corresponding inner strip band in a sealing way; a downward corner angle is formed at the lowermost end of each side surface; the at least one pair of rigid bulges which are arranged in an opposite way are arranged in each grid unit. According to the location grid rack, due to the ship-shaped structures of the rigid bulges, an incident flow area and fluid eddies are reduced, the pressure drop is reduced, and the fuel rod is prevented from being scratched. Correspondingly, the invention also discloses a fuel assembly provided with the location grid rack.
Owner:LINGAO NUCLEAR POWER +3

Cross-medium aircraft based on common rotor and cycloidal propeller

The invention discloses a cross-medium aircraft based on a common rotor and a cycloidal propeller. The aircraft comprises an aircraft body, a horizontal support frame and a cross-medium propeller. Anend part of the horizontal support frame is connected with the cross-medium propeller through a propeller tilting device, and the propeller tilting device is used for driving the cross-medium propeller to rotate in a vertical plane around an axis of the horizontal support frame; and the cross-medium propeller is provided with a plurality of blades evenly distributed around the axis of the cross-medium propeller, and the cross-medium propeller is connected with the roots of the blades through a blade turnover device. According to a deformation propeller considering performance characteristics of an aerial fluid and a underwater fluid, one set of propeller can be used for achieving omnidirectional maneuvering navigation and fixed-point hovering in the air and under the water, and a underwater slamming force and a storage space are reduced through composite deformation.
Owner:DALIAN UNIV OF TECH

Wave rotor apparatus

A wave rotor apparatus is provided. In another aspect of the present invention, a radial wave rotor includes fluid passageways oriented in a direction offset from its rotational axis. A further aspect of the present invention employs stacked layers of generally radial channels in a wave rotor. Moreover, turbomachinery is located internal to a wave rotor in yet another aspect of the present invention. In yet another aspect of the present invention, a radial wave rotor has an igniter and fuel injector. Correctional passages are employed in still another aspect of the present invention wave rotor.
Owner:BOARD OF TRUSTEES OPERATING MICHIGAN STATE UNIV

Low pressure drop holding grid and fuel component with holding grid

The invention discloses a low pressure drop holding grid which comprises a plurality of inner strips and outer strips, wherein the plurality of inner strips are intersected with one another to form a net-shaped grid structure and are formed into a plurality of hollow grid units; the outer strips are arranged at the periphery of the grid structure in an enclosure manner and are fixed with the inner strips; a plurality of first guide wings which are arranged at intervals are formed on the upper edges of the outer strips; a plurality of second guide wings and third guide wings which are arranged alternatively are formed on the lower edges of the outer strips; each third guide wing is positioned between two adjacent second guide wings; the interval between each second guide wing and each third guide wing is smaller than the width of each first guide wing; the first guide wings, the second guide wings and the third guide wings all extend into the grid structure in an inclined and convex manner. By adopting the low pressure drop holding grid disclosed by the invention, hooking in hoisting is effectively prevented, and moreover through cooperation of three guide wings, the amplitude that the guide wings extend into the grid structure in the inclined and convex manner can be very small, so that the incident flow area is small, and the pressure loss of a coolant is small.
Owner:CHINA NUCLEAR POWER TECH RES INST CO LTD +1

Vertical Take-Off and Landing Unmanned Aerial Vehicle Having Foldable Fixed Wing and Based on Twin-Ducted Fan Power System

ActiveUS20220081111A1Reduce power lossHigh lift-to-weight ratioFuselage framesPropellersSuction forceLevel flight
A vertical take-off and landing (VTOL) unmanned aerial vehicle having a foldable fixed wing and a twin-ducted fan power system (7) arranged at a tail portion of a fuselage in a transverse and tail propulsion arrangement provides lift for vertical take-off and landing and propulsion for horizontal flight. By means of deflection of a control servo plane arranged at a duct exit, a vectored thrust is provided to enable a fast attitude change. When the aerial vehicle takes off and lands vertically / flies at a low speed, the wing is folded to reduce the frontal area exposure to crosswind. When the aerial vehicle is flying horizontally, the wing is expanded to obtain larger lift. A Coanda effect is created at a trailing edge of the wing by suction of the duct to improve performance.
Owner:SOUTH CHINA UNIV OF TECH

Umbrella rib type underwater vehicle depth and posture adjusting device and control method thereof

The invention discloses an umbrella rib type underwater vehicle depth and posture adjusting device which comprises a buoyancy adjusting system A, an information acquisition and control system B and abattery pack. The buoyancy adjusting system A comprises a head end adjusting subsystem and a tail end adjusting subsystem; the head end adjusting subsystem and the tail end adjusting subsystem comprise main shaft stepping motors, main gears and six groups of buoyancy adjusting units; each buoyancy adjusting unit comprises a buoyancy adjusting cabin, a push rod, a conversion cylinder, a relay shaftlimiter, a coupling type electromagnetic clutch, a branch gear and a transition gear; the information acquisition and control system B comprises a depth meter, a temperature-salinity-depth meter, aninertia measuring instrument, a displacement sensor, a processor and a control assembly. The control method comprises the steps that the underwater vehicle dives; the underwater vehicle floats upwards; and the heeling posture of the underwater vehicle is adjusted. The buoyancy state is adjusted by changing the drainage volume, the longitudinal and transverse inclination postures of the underwatervehicle are adjusted by changing the position of the buoyancy center, and the device and method are suitable for large-range depth adjustment and high-precision buoyancy compensation of the underwatervehicle.
Owner:TIANJIN UNIV
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