Patents
Literature
Hiro is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Hiro

40 results about "Avgas" patented technology

Avgas (aviation gasoline, also known as aviation spirit in the UK) is an aviation fuel used in spark-ignited internal-combustion engines to propel aircraft. Avgas is distinguished from mogas (motor gasoline), which is the everyday gasoline used in motor vehicles and some light aircraft. Unlike mogas, which has been formulated since the 1970s to allow the use of platinum-content catalytic converters for pollution reduction, the most commonly used grades of avgas still contain tetraethyllead (TEL), a toxic substance used to prevent engine knocking (detonation), with ongoing experiments aimed at eventually reducing or eliminating the use of TEL in aviation gasoline.

Shaft part double-wheel symmetrical grinding device and process

The invention relates to a shaft part double-wheel symmetrical grinding device and process. The process includes: machining a workpiece on an excircle grinder to Ra0.40, leaving a machining allowance of 0.008-0.12mm, fixing a fixing piece during grinding, screwing a pressure-adjusting bolt compression spring, enabling grinding wheels to contact a workpiece surface to be ground, winding a lead screw, and enabling two grinding wheels to generate transverse feed; when the pressure of the spring on the workpiece is 2-3kg, stopping the transverse feed, starting a lathe, enabling the workpiece to rotate at the speed of 80-150 turns / minute, driving the two grinding wheels to rotate, starting a large carriage, enabling the large carriage to move vertically along a lathe track and drive the grinding wheels to move vertically together, controlling the moving quantity in the way that the grinding wheels move 2-3 mm vertically when the workpiece rotates a circle, washing through aviation gasoline till the workpiece surface roughness parameter meets the technical requirement, detaching the workpiece, and finishing grinding. The shaft part double-wheel symmetrical grinding device and process has the advantage that the process is simple, the roughness can be lower than Ra0.012, and efficiency is high.
Owner:江西铜业集团(德兴)铸造有限公司

Antioxidant for sintering neodymium iron boron jet mill, and use method of antioxidant

InactiveCN104449740AReduced oxidation resistanceLoss is good for compensationInorganic material magnetismChemical inhibitorsMetallurgyStearic acid
The invention discloses an antioxidant for a sintering neodymium iron boron jet mill, and a use method of the antioxidant. The antioxidant consists of an antioxidation agent and an antioxidation assistant, wherein the antioxidation agent consists of one or several of 1-cetyl alcohol, trityl alcohol and zinc stearate and alcohol; and the antioxidation assistant is a mixture of aviation gasoline and petroleum ether. The use method comprises the following steps that (1) 30-65% of the total amount of the antioxidation agent and neodymium iron boron magnetic powder are uniformly mixed and then crushed via the jet mill; (2) fine mixing is performed, and the antioxidation assistant and the rest antioxidation agent are added and uniformly mixed; and (3) compression molding is performed and then antioxidant removal treatment is performed. The antioxidant can improve the antioxidation property of the sintering neodymium iron boron magnetic powder, greatly improve the lubricating property and the orientation degree of the magnetic powder, and improve the magnet property. The use method can reduce loss of the antioxidation agent caused by volatilization, and can ensure continuous antioxidation property of the neodymium iron boron magnetic powder in each production stage.
Owner:HUNAN AEROSPACE MAGNET & MAGNETO

A kind of electro-injection aviation gasoline engine

The invention discloses an electric injection type aviation gasoline engine, which comprises a crankcase and four cylinders. The four cylinders are installed on both sides of the crankcase in pairs horizontally opposed to each other, and the air inlets of the four cylinders are all facing upwards. The air inlet of each cylinder block is connected with an EFI mechanism, and the EFI mechanism includes an intake pipe, a throttle shaft, a driving crank arm, a fuel injector, and an oil inlet pipe, and the throttle shaft passes through the radial direction of the intake pipe. Located in the middle of the intake pipe, the part where the throttle shaft is located in the inner hole of the intake pipe is fixedly connected to the throttle valve, and the end outside the intake pipe is fixedly connected to the driving crank arm, and the fuel injector is installed on the side of the intake pipe inclined to the axis of the intake pipe , the lower part of the fuel injector is equipped with a nozzle, the middle part is equipped with an electromagnetic switch valve, and the upper part is connected to the oil inlet pipe. The nozzle is located in the inner hole of the intake pipe and is located at the lower part of the throttle valve; An air filter is connected; the present invention has wide adaptability and good fuel economy.
Owner:厦门林巴赫航空发动机有限公司

Lettering and paint embedding method for thin plate disc-shaped duralumin bottom plate part

PendingCN114054968AProblems Affecting FlatnessAdditional drying stepsPretreated surfacesLaser beam welding apparatusDuraluminLettering
The invention relates to a lettering and paint embedding method for a thin plate disc-shaped duralumin bottom plate part. The bottom plate part comprises an annular edge plate and a circular truncated cone, and an open bottom hole is formed in the bottom face of the annular edge plate; a plurality of lettering areas are arranged on the plane of the bottom hole; and line carving is performed on the bottom surface of the annular edge plate. The lettering and paint embedding method comprises the following steps that: S1, lettering and line carving are conducted, specifically, the bottom plate part is clamped, lettering contents of different lettering areas are edited, and lettering is conducted on the lettering areas through lettering equipment, line carving is performed on the bottom surface of the annular edge plate, the depth of the lettering and line carving is 0.2-0.3 mm, and the width of the lettering and line carving is 0.3 mm; S2, inspection is performed, specifically, a laser lettering font inspection template is adopted to compare and inspect lettering fonts, and a vernier caliper is adopted to inspect the depth and width of the lettering and line carving; S3, paint embedding is conducted, specifically, a part to be subjected to paint embedding is wiped with aviation gasoline, paint embedding is carried out by adopting C04-42 black alkyd enamel paint, after paint embedding, the part is naturally aired, after being aired, the paint at a non-paint-embedded part is cleaned, and the part is placed in a constant-temperature drying oven to be dried.
Owner:GUIZHOU AEROSPACE ELECTRONICS TECH CO LTD
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products