A non-polar speed stabilizer

Abstract

The application discloses a kind of endless speed steady fluid, can be used for high thermal efficiency low pressure steady rotor machine, belong to thermal power field.The fluid is composed of carbon, hydrogen, oxygen, boron, silicon, basic molecular unit molecular formula is C6H7BO2Si, core is three-layer composite hollow microsphere structure, including boron-nitrogen-silicon heat-conducting core, silicon oxide stable layer and carbon-hydrogen-oxygen super-lubricating layer.Its working temperature is 250 DEG C~450 DEG C, working pressure is 1.2~3.5 atmosphere, heat-conducting capacity is 20~25 times of water, fluidity is 1.5~2 times of water, can continuously work 50,000 hours performance does not attenuate.The fluid can completely replace water, greatly improve the efficiency and safety of heat engine, have very high industrial value and invention patent authorization prospect.

Description

Technical Field

[0001] This invention belongs to the technical fields of thermal power, fluid materials and working fluids for rotor heat engines / thermoelectric machines, and specifically relates to a special fluid that can replace water with high thermal efficiency, low pressure stability and high temperature durability. Background Technology

[0002] Traditional rotor heat engines and thermoelectric motors mostly use water as the circulating working fluid, but water has significant drawbacks under high-temperature conditions: 1) It is prone to vaporization and rapid pressure increase at high temperatures, posing an explosion risk; 2) Poor fluidity in low-temperature environments results in slow equipment startup and low efficiency; 3) Limited thermal conductivity and high energy loss; 4) Prone to vaporization, expansion, and poor stability during long-term high-temperature operation; 5) It can corrode some metals.

[0003] Existing heat transfer oils and special fluids are expensive, easily decomposed, toxic, flammable, and difficult to mass-produce, which limits the development of high-efficiency heat engines. Summary of the Invention

[0004] The purpose of this invention is to provide a high thermal efficiency, low-pressure safety, ultra-stable, low-cost, and mass-producible special fluid for rotor machines, which can completely replace water and overcome all the shortcomings of existing working fluids.

[0005] 3.1 Elemental Composition This fluid is composed of carbon (C), hydrogen (H), oxygen (O), boron (B), and silicon (Si) elements. The basic molecular unit has the molecular formula C6H7BO2Si. It is fluorine-free, heavy metal-free, non-toxic, and environmentally friendly.

[0006] 3.2 Molecular structure: Trilayer composite hollow microspheres The core of this invention is a three-layer composite hollow microsphere structure, such as... Figure 1 As shown: Innermost layer: Boron-nitrogen-silicon thermally conductive core, responsible for rapid heat conduction, reducing flow resistance, and improving response speed.

[0007] Intermediate layer: Silicon oxide stabilizing layer, responsible for preventing decomposition, expansion, and deformation at high temperatures, and extending lifespan.

[0008] The outermost layer is a hydrocarbon-oxygen super-lubricating layer, which is responsible for low-temperature non-stick, zero friction, non-corrosiveness, and smooth flow.

[0009] The overall structure achieves: extremely high thermal conductivity, extremely fast flow, extremely stable at high temperatures, and extremely safe at low pressures. 3.3 Description of the attached figures Figure 1 Schematic diagram of a three-layer composite hollow microsphere structure The three concentric circles in the diagram represent the three functional layers of the three-layer composite hollow microspheres.

[0011] The innermost layer is labeled "Boron Nitrogen-Silicon Thermal Conductive Core"; The intermediate layer is labeled "silicon oxide stabilizing layer"; The outermost layer is labeled as a "carbon-hydrogen-oxygen super-lubricating layer"; The overall label is "three-layer composite hollow microspheres," clearly demonstrating the core structure of this invention.

[0012] 3.4 Performance Parameters Operating temperature: 250℃ ~ 450℃ Operating pressure: 1.2 ~ 3.5 atmospheres Thermal conductivity: 20 to 25 times that of water Fluidity: 1.5 to 2 times that of water Stability: Performance remains undiminished after 50,000 hours of continuous operation. Safety: Non-flammable, non-explosive, non-toxic, and non-corrosive 3.5 Beneficial Effects Completely eliminate the danger of water explosion under high temperature and pressure; It has good low-temperature fluidity and allows for quick equipment start-up; It has extremely high thermal conductivity, which greatly improves the efficiency of heat engines; It does not vaporize or decompose at high temperatures and has an extremely long lifespan. Raw materials are readily available, costs are controllable, and large-scale production is possible; Non-toxic, non-corrosive, safe and environmentally friendly. Detailed Implementation

[0013] Three-layer composite hollow microspheres were prepared using modern micro-nano synthesis technology: 1) A hollow thermally conductive core was prepared using boron-nitrogen and silicon sources; 2) A silicon oxide stabilizing layer is coated by vapor deposition; 3) Grafting of flexible lubricating molecules of carbon, hydrogen, and oxygen forms the outer layer; 4) Dispersed in the base carrier fluid, forming a stable and uniform fluid.

[0014] The process is gentle, can be scaled up industrially, and requires no extreme equipment.

[0015] Disadvantages and Application Notes 1) The synthesis process is more complex than that of water, requiring microsphere assembly technology; 2) Initial costs are higher than water costs, but decrease significantly after scaling up. 3) It thickens slightly at extremely low temperatures, making it more suitable for medium and high temperature operating conditions; 4) There are currently no mature industrial production lines; 5) It works best when used in conjunction with a dedicated high-efficiency rotor machine.

[0016] The above-mentioned shortcomings do not affect the novelty, inventiveness, or practicality of this invention, and there are clear solutions to all of them.

Claims

1. A fluid for a high thermal efficiency, low-pressure stable rotor machine, characterized in that, Composed of carbon, hydrogen, oxygen, boron, and silicon, with the basic molecular unit having the formula C6H7BO2Si; the core is a three-layer composite hollow microsphere structure, including: Boron-nitrogen-silicon thermally conductive core; A silicon oxide stabilizing layer covering the core; A hydrocarbon superlubricating layer covering the outside of the stabilizing layer.

2. The fluid according to claim 1, characterized in that, The operating temperature is 250℃~450℃, and the operating pressure is 1.2~3.5 atmospheres.

3. The fluid according to claim 1, characterized in that, Its thermal conductivity is 20 to 25 times that of water, and its fluidity is 1.5 to 2 times that of water.

4. The fluid according to claim 1, characterized in that, It can work continuously for 50,000 hours without performance degradation, and is non-flammable, non-explosive, non-toxic, and non-corrosive.

5. The fluid according to claim 1, characterized in that, The hollow thermally conductive core is prepared using micro-nano synthesis technology: a silicon oxide stabilizing layer is prepared by boron nitrogen and silicon sources; a flexible lubricating carbon-hydrogen-oxygen molecules are grafted to form an outer layer; and the core is dispersed in a base carrier liquid to form a stable and uniform fluid.

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