RU93035344A - ENGINE SPRAYER SPRAYER - Google Patents

ENGINE SPRAYER SPRAYER

Info

Publication number
RU93035344A
RU93035344A RU93035344/06A RU93035344A RU93035344A RU 93035344 A RU93035344 A RU 93035344A RU 93035344/06 A RU93035344/06 A RU 93035344/06A RU 93035344 A RU93035344 A RU 93035344A RU 93035344 A RU93035344 A RU 93035344A
Authority
RU
Russia
Prior art keywords
sprayer
needle
nozzle
engine
diesel
Prior art date
Application number
RU93035344/06A
Other languages
Russian (ru)
Other versions
RU2095614C1 (en
Inventor
С.А. Побегалов
Original Assignee
С.А. Побегалов
Filing date
Publication date
Application filed by С.А. Побегалов filed Critical С.А. Побегалов
Priority to RU93035344A priority Critical patent/RU2095614C1/en
Priority claimed from RU93035344A external-priority patent/RU2095614C1/en
Publication of RU93035344A publication Critical patent/RU93035344A/en
Application granted granted Critical
Publication of RU2095614C1 publication Critical patent/RU2095614C1/en

Links

Claims (1)

Изобретение относится к топливным форсункам дизелей и может быть применено для распыливания различных жидкостей. Распылитель форсунки дизеля состоит из корпуса с центральным каналом, иглы распылителя, расточки с подводящими отверстиями седла, соплового конуса с ребрами и поднутренными полостями. При подъеме иглы распылителя топливо по зазору между иглой и коническим седлом, частично соударяясь на пересечении, направляется на сопловой конус с оребрением, на котором в поднутренных полостях образуются стоячие вихри, устраняющие ламинарность течения, смачиваемость поверхности и нагарообразование. Дробление струй, насыщение капель кислородом воздуха, создавая парогазовую смесь, способствует легкому воспламенению.The invention relates to diesel fuel injectors and can be used for spraying various liquids. A diesel nozzle atomizer consists of a body with a central channel, a spray needle, a bore with the supply holes of the seat, a nozzle cone with ribs and undercuts. When the spray needle is lifted, the fuel is directed along the gap between the needle and the conical seat, partially colliding at the intersection, and is directed to a nozzle cone with fins, on which standing vortices are formed in the undercut cavities, eliminating the laminar flow, wettability of the surface and carbon formation. Crushing jets, saturation of droplets with oxygen in the air, creating a vapor-gas mixture, contributes to easy ignition.
RU93035344A 1993-07-07 1993-07-07 Diesel engine nozzle spay tip RU2095614C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU93035344A RU2095614C1 (en) 1993-07-07 1993-07-07 Diesel engine nozzle spay tip

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU93035344A RU2095614C1 (en) 1993-07-07 1993-07-07 Diesel engine nozzle spay tip

Publications (2)

Publication Number Publication Date
RU93035344A true RU93035344A (en) 1996-01-20
RU2095614C1 RU2095614C1 (en) 1997-11-10

Family

ID=20144741

Family Applications (1)

Application Number Title Priority Date Filing Date
RU93035344A RU2095614C1 (en) 1993-07-07 1993-07-07 Diesel engine nozzle spay tip

Country Status (1)

Country Link
RU (1) RU2095614C1 (en)

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