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147 results about "Gravity assist" patented technology

In orbital mechanics and aerospace engineering, a gravitational slingshot, gravity assist maneuver, or swing-by is the use of the relative movement (e.g. orbit around the Sun) and gravity of a planet or other astronomical object to alter the path and speed of a spacecraft, typically to save propellant and reduce expense.

Gravity-assisted steam flooding exploitation method for heavy laver common heavy oil reservoir

The invention relates to a gravity-assisted steam flooding mining method for exploiting thick-bed ordinary heavy oil reservoirs. In the thick-bed ordinary heavy oil reservoirs, the methods of steam injection in vertical wells and production in horizontal wells or steam injection in horizontal wells and production in horizontal wells are adopted . For the oil reservoir blocks that have been developed by vertical wells, the combination of vertical wells and horizontal wells can be used to drill horizontal production wells along the lower part of the oil layer in the known oil reservoir blocks, so that the vertical steam injection wells are obliquely above the horizontal wells, and the production wells and injection wells Simultaneous huff and puff of steam wells for 2-4 cycles or thermal communication between steam injection wells and production wells or formation of reservoir pressure down to 3-4MPa, transfer to steam injection wells and steam injection production wells for production and production; or steam injection wells and production wells have formed thermal communication , After the newly drilled horizontal production well huffs and puffs for one cycle and removes the pollution near the wellbore, the steam injection production well is transferred to the steam injection well for production and production. The invention can exert the sweeping effect of the displacement fluid in both vertical and horizontal directions, increase the sweeping range of the driving fluid, and increase the crude oil recovery rate of the thick common heavy oil reservoir.
Owner:PETROCHINA CO LTD

Modified type unidirectional gravity force hot pipe

InactiveCN101338986ABack passWith one-way thermal conductivityIndirect heat exchangersWorking fluidEvaporation
The invention discloses an improved unidirectional gravity assisted heat pipe which comprises a sealed chamber (4), and proper quantity of heat pipe working fluid (5) sealed in the sealed chamber (4). The pipe body is divided into a condensation section (1), an evaporation section (3) and an insulation section (2) arranged between the condensation section (1) and the evaporation section (3). The condensation section (1) is arranged on the top of the gravity assisted heat pipe, and the evaporation section (3) is arranged at the bottom of the gravity assisted heat pipe. The enclosers of the condensation section (1) and the evaporation section (3) are made of materials with high coefficient of heat conductivity; the insulation section (2) is made of insulant different from the condensation section (1) and the evaporation section (3). When the temperature of the evaporation section (3) is higher than the temperature of the condensation section (1), heat is transferred to the condensation section (1) of lower temperature under the action of the gravity assisted heat pipe. When the temperature of the evaporation section (3) is lower than the temperature of the condensation section (1), heat can not be transferred to the evaporation section (1) along the shell of the gravity assisted heat pipe, thus preventing heat from being transferred inversely along the shell of the gravity assisted heat pipe and achieving the unidirectional thermal conduction of the gravity assisted heat pipe. The improved unidirectional gravity assisted heat pipe is applicable for unidirectional transfer of heat of gravity assisted heat pipes which are strictly required.
Owner:SHANDONG UNIV OF SCI & TECH

Preparation of uneven humid efficient phase changing coating and gravity assisted heat pipe device

The invention discloses an uneven humid efficient phase changing coating preparation and a gravity assisted heat pipe device. The gravity assisted heat pipe device comprises a pipe body with two sealed ends; liquid working medium is poured into the pipe body; the upper portion of the pipe body is a condensation section, and the lower portion of the pipe body is an evaporation section; the inner top wall of the condensation section is a zigzag-shaped structure face; the uneven humid coating covers the inner side wall of the condensation section, the zigzag-shaped structure face and the inner bottom face of the evaporation section; the uneven humid coating comprises dewatering areas and hydrophilic areas; the uneven humid coating covering the zigzag-shaped structure face of the condensation section is of the structure that the straight stripes of the dewatering areas and the hydrophilic areas are distributed alternately; and the direction of the straight stripes is perpendicular to the zigzag grooves of the zigzag-shaped structure face. The gravity assisted heat pipe device can improve heat flux of an evaporation process and a condensation process remarkably. According to gravity assisted heat pipe device, depending on the operation rules of gravity assisted heat pipes, drawbacks existing in current gravity assisted heat pipes are overcome; working medium cycling speed is improved; and heat transfer load of the heat pipes is strengthened.
Owner:SOUTH CHINA UNIV OF TECH

Refrigerator with heat preservation drying mechanism

ActiveCN103836865AThe temperature will not exceed the appropriateNo reverse heat conductionLighting and heating apparatusDomestic refrigeratorsEvaporationGravity assist
The invention relates to a refrigerator with a heat preservation drying mechanism. The refrigerator comprises a refrigeration chamber and a refrigeration mechanism. A heat preservation chamber is arranged on the bottom on the outer side of the refrigeration chamber, phase change heat storage blocks are arranged in the heat preservation chamber, the condensation sections of five or more gravity assisted heat pipes are inserted into the corresponding phase change heat storage blocks, the evaporation sections of the gravity assisted heat pipes extend out of the heat preservation chamber and are respectively inserted into a condensing coil of a condenser, a thin ventilation pipe is arranged in the refrigeration chamber, the two ends of the thin ventilation pipe respectively extend into the heat preservation chamber, one end of the thin ventilation pipe is an air inlet, the other end of the thin ventilation pipe is an air outlet, a micro fan is arranged on the air inlet, the thin ventilation pipe located inside the refrigeration chamber is communicated with a water drainage pipe through a T-branch pipe, and a water outlet of the water drainage pipe extends out of the refrigeration chamber. According to the refrigerator with the heat preservation drying mechanism, the temperature of the heat preservation chamber is kept from 40 DEG C to 50 DEG C. When the temperature of a working medium inside the condensing coil is larger than the temperature of phase change heat storage materials in the heat preservation chamber, the gravity assisted heat pipes work and transfer waste heat to the phase change heat storage materials in the heat preservation chamber; otherwise, the gravity assisted heat pipes are closed.
Owner:UNIV OF SCI & TECH OF CHINA

Natural gas acquiring device and method

InactiveCN105275436AReduce development costsEliminate the risk of external contaminationConstructionsFluid removalLiquid waterGravity assist
The invention discloses a natural gas acquiring device comprising a casing and a gravity assisted heat pipe. The outer wall of the heat dissipation section of the casing and the outer wall of the heating section of the casing are provided with perforations. The upper part of the gravity assisted heat pipe is arranged inside the heat dissipation section of the casing. The lower part of the gravity assisted heat pipe is arranged inside the heating section of the casing. In this way, the heat is absorbed by the lower part of the gravity assisted heat pipe and then the absorbed heat is transferred to the gravity assisted heat pipe. After the upper part of the gravity assisted heat pipe is heated, the natural gas hydrate is heated to be decomposed into methane gas and liquid water. Along with the increasing of the content of the decomposed natural gas hydrate, the pressure inside a natural gas hydrate storage layer is increased. When the pressure is increased to a certain degree, the pressure is automatically ejected to the top of the casing. Therefore, the development of the natural gas hydrate is realized. The invention also discloses a natural gas acquiring method, wherein the bottom of the gravity assisted heat pipe is heated by means of a high temperature layer at the bottom of the natural gas hydrate storage layer. As a result, the potential risk of external contamination is eliminated and the development cost is effectively reduced.
Owner:QINGDAO INST OF MARINE GEOLOGY

Adaptive rescue trajectory planning method based on numerical optimization algorithm

ActiveCN109491246AOptimize the rescue trackImprove efficiencyAdaptive controlCarrying capacityAerogravity assist
The invention provides an adaptive rescue trajectory planning method based on a numerical optimization algorithm. According to the method, after a launch vehicle fails, it is judged whether or not therescue trajectory needs gravity-assisted taxiing after a fault; if no, remaining fuel and thrust are used for looking for an optimal rescue trajectory in the current orbital plane and a rescue orbitwhich the launch vehicle can send payload into; if yes, it is considered that the situation of the orbital plane is changed, taxiing is assisted by introducing gravity, the orbital transfer time is adjusted, and the utilization rate of the remaining fuel is increased, thereby obtaining the optimal rescue trajectory and the rescue orbit which the launch vehicle can send payload into through optimization. According to the evaluation of the remaining carrying capacity, the initial value of the trajectory planning numerical optimization algorithm is adaptively generated, and according to the initial value of the state of the rescue trajectory, the numerical optimization algorithm is used for determining the rescue trajectory, improving the solution convergence and efficiency of the rescue trajectory, and reducing the solution difficulty of the problems.
Owner:BEIJING AEROSPACE AUTOMATIC CONTROL RES INST +1

Hybrid vertical energy storage system

A hybrid vertical energy storage system is invented wherein the components responsible for the conversion, storage and production of energy are used as the weighted component of a gravitationally aided energy storage device. The present invention allows gravity to operate mechanical devices which may help move a volume of fluid in order to compress a gas and store potential energy. The present invention utilizes the attributes of pumped hydro by using gravity assisted fluid transfer, and also combines Compressed Air Energy Storage (CAES) functionality by powering hydraulic pumps and motors to transfer fluid from one vessel to another vessel. This feature allows conventional, inexpensive, market proven components to make the capture, conversion, storage and production of energy more effective and affordable while eliminating the placement issues associated with such large scale pumped hydro and CAES systems while extending battery service life. Ideally, combining the positive attributes of some or all of the existing technologies into one energy storage system would provide a real and meaningful improvement, especially if the improvement reduced or eliminated economic, environmental and operational flaws associated with the individual technologies. This invention also provides a method of combining the output of individual, combined attribute energy storage systems to provide user definable and expandable electrical energy production. The vertical aspect of the invention allows operational attribute that separates and makes independent the capture and storage of energy being placed into the energy storage system and the hydro-pneumatic production of energy exiting the system.
Owner:HUGHEY CHARLES E

Gravity-assisted geomagnetic generator

A geomagnetic power generating apparatus 100 has a guide means 20, one or more moving permanent magnets 10, a plurality of coils 40 and a battery 50 or series of batteries. The one or more moving permanent magnets 10, each permanent magnet 10 has a north polarity N at a first end 11 and a south polarity S at the opposite second end 12. The one or more magnets 10 are located and guided along a guide path GP by the guide means 20. The plurality of coils 40 has each coil 40 positioned around the guide means 20, encircling both the guide means 20 and the guide path GP along which one or more permanent magnets 10 move. Each coil 40 has a cross section having an increasing number of windings extending from a minimal winding first end 44 to a maximum winding second end 45. The battery 50 or a series of batteries is connected to the plurality of coils 40. When the one or more permanent magnets 10 are moved, with one magnet 10 approaching toward each coil 40 and as the N or S end of the magnet 10 approaches inside the coil 40 an electric current is created along with a magnetic field having an opposite polarity at the narrow end 44 of the coil 40 relative to the entering end of the magnet 10. As the movement of the one or more permanent magnets 10 generates an electric current in the coils 40 to charge the battery 50 and as the magnet 10 leaves the thick end 45 of the coil 40 a similar or like pole S to S or N to N polarity exists causing the magnetic field of each of the coils 40 to push the similar polarity second end 12 of the magnet 10 out of the coil 40, propelling the magnet 10 to the next coil 40. The moving magnets 10 generate electric currents within the coils 40 causing a major propulsive magnetic field to act on the magnet 10 augmenting its momentum along the guide path GP.
Owner:RAGHUPRASAD PUTHALATH KOROTH
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