SU65514A1 - Turbocharger for internal combustion engines - Google Patents

Turbocharger for internal combustion engines

Info

Publication number
SU65514A1
SU65514A1 SU9262A SU331510A SU65514A1 SU 65514 A1 SU65514 A1 SU 65514A1 SU 9262 A SU9262 A SU 9262A SU 331510 A SU331510 A SU 331510A SU 65514 A1 SU65514 A1 SU 65514A1
Authority
SU
USSR - Soviet Union
Prior art keywords
internal combustion
turbocharger
compressor
combustion engines
engine
Prior art date
Application number
SU9262A
Other languages
Russian (ru)
Inventor
Б.М. Рыжов
Original Assignee
Б.М. Рыжов
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Б.М. Рыжов filed Critical Б.М. Рыжов
Priority to SU9262A priority Critical patent/SU65514A1/en
Application granted granted Critical
Publication of SU65514A1 publication Critical patent/SU65514A1/en

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  • Supercharger (AREA)

Description

Целью насто щего изобретени   вл етс  использование энергии продуктов горени  дл  сжати  воздуха, предназначаемого дл  наддува двигател  внутреннего горени .The object of the present invention is to utilize the energy of the combustion products for compressing air intended for pressurizing an internal combustion engine.

Отличительна  особенность изобретени  заключаетс  в применении дл  этой цели компрессора со свободными Поршн ми, приводимого в действие продуктами горени , отбираемыми из цилиндра двигател . Свободные поршни компрессора могут быть попарно св заны общим штоком, проход щим через перегородку цилиндра, полости между которой и поршн ми образуют рабочие камеры компрессора.A distinctive feature of the invention is the use for this purpose of a compressor with free pistons driven by combustion products taken from the engine cylinder. The free pistons of the compressor can be pairwise connected by a common rod passing through the cylinder wall, the cavities between which and the pistons form the working chambers of the compressor.

На чертеже фиг. 1 изображает схему работы компрессора дл  двухцилиндрового двигател , ф11г. 2 - схему присоединени  трехцилиндрового компрессора к двеиадцатицилиндровому авиационному двигателю.In FIG. 1 shows a compressor operation scheme for a two-cylinder engine, 11g. 2 is a diagram of the connection of a three-cylinder compressor to a two-twenty-cylinder aircraft engine.

Цилиндры четырехтактного двигател  нар ду с впускными и выхлопными клапанами имеют окна 2.Cylinders of the four-stroke engine, along with intake and exhaust valves, have windows 2.

С приближением поршн  / к нижней мертвой точке продукты горени  поступают из цилиндра двигател  через окно 2 и обратный клапан 11 в камеру А компрессора, свободные поршни которого попарно св заны общим штоком, проход щим через перегородку 10 цилиндра компрессора.As the piston (bottom dead center) approaches, combustion products flow from the engine cylinder through window 2 and check valve 11 into compressor chamber A, the free pistons of which are connected in pairs by a common rod passing through the compressor cylinder 10.

Действием продуктов горени  в KaiMepe А ггоршни 3 и 5 перемещаютс  влево (по чертежу).By the action of the combustion products in KaiMepe A, the horns 3 and 5 are moved to the left (according to the drawing).

При этом поршень 5 сжимает воздух в камере В и нагнетает его через обратный клапан 4 в трубопровод 7 или в рессивер Я (фиг. 2), а поршень 5 засасывает в камеру Б через клапан 6 атмосферный воздух и выталкивает отработавшие газы из Г.At the same time, the piston 5 compresses the air in chamber B and injects it through the check valve 4 into the pipeline 7 or into the receiver I (Fig. 2), and the piston 5 sucks the atmospheric air into valve B through the valve 6 and pushes the exhaust gases out of G.

При движении вниз порщн  S двигател  происходит повторение цикла.When moving down Porshn S engine repeats the cycle.

Дл  предупреждени  ударов поршней 5 и 5 о перегородку 10 предусмотрен демпфер 9.To prevent impacts of the pistons 5 and 5 on the partition 10, a damper 9 is provided.

По достижении самолетом определенной высоты летчик посредством т ги открывает краны Н. Продукты горени  поступают из одновременно работающих цилиндров одного блока двигател , через обратные клапаны О, в присоединенный к ним цилиндр компрессора.When the aircraft reaches a certain height, the pilot opens the cranes H by means of the gun. Combustion products come from simultaneously working cylinders of one engine block, through check valves O, to the compressor cylinder attached to them.

Сжатый воздух из цилиндров компрессора по трубопроводам подаетс  в рессивер И, проходит через радиатор Р и нагнетае-Л  центробежным нагнетателем ДЯ в коллектор /( двигател  Е.Compressed air from compressor cylinders is piped through pipelines into receiver I, passes through radiator P and is pumped by L with a centrifugal supercharger DY to collector / (engine E.

SU9262A 1944-02-18 1944-02-18 Turbocharger for internal combustion engines SU65514A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU9262A SU65514A1 (en) 1944-02-18 1944-02-18 Turbocharger for internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU9262A SU65514A1 (en) 1944-02-18 1944-02-18 Turbocharger for internal combustion engines

Publications (1)

Publication Number Publication Date
SU65514A1 true SU65514A1 (en) 1944-11-30

Family

ID=48245762

Family Applications (1)

Application Number Title Priority Date Filing Date
SU9262A SU65514A1 (en) 1944-02-18 1944-02-18 Turbocharger for internal combustion engines

Country Status (1)

Country Link
SU (1) SU65514A1 (en)

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