SU22406A1 - Internal combustion turbine - Google Patents

Internal combustion turbine

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Publication number
SU22406A1
SU22406A1 SU13897A SU13897A SU22406A1 SU 22406 A1 SU22406 A1 SU 22406A1 SU 13897 A SU13897 A SU 13897A SU 13897 A SU13897 A SU 13897A SU 22406 A1 SU22406 A1 SU 22406A1
Authority
SU
USSR - Soviet Union
Prior art keywords
turbine
internal combustion
blades
combustion turbine
chambers
Prior art date
Application number
SU13897A
Other languages
Russian (ru)
Inventor
И.С. Слесаренко
Original Assignee
И.С. Слесаренко
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 И.С. Слесаренко filed Critical И.С. Слесаренко
Priority to SU13897A priority Critical patent/SU22406A1/en
Application granted granted Critical
Publication of SU22406A1 publication Critical patent/SU22406A1/en

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Description

Изобретение имеет в виду использо1вать дл  вращени  турбины как пар так и газы, образованные горючим, дл  чего полушаровые камеры предлагаемой турбины расположены по сторонам венца ее лопаток и снабжены каналами, по которым образующиес  в камере газы, направл ютс  на рабочие лопатки турбины и дальше-в расположенныер дом осевые турбины или под паровой котел.The invention is intended to use both steam and gas generated for rotation of a turbine, for which the hemispherical chambers of the proposed turbine are located on the sides of the crown of its blades and provided with channels through which gases formed in the chamber are directed to the turbine blades and further located axial turbine house or under the steam boiler.

На чертеже фиг. 1 изображает разрез турбины; фиг. 2-вертикальный разрез полушаровых камер, расположенных по сторонам венца лопаток турбины; фиг. 3-поперечный разрез турбины.In FIG. 1 shows a section of a turbine; FIG. 2 is a vertical section of the hemispherical chambers located on the sides of the crown of the turbine blades; FIG. 3-cross section of the turbine.

На валу О установлен турбинный диск с лопатками в, вокруг которого расположены полушаровые камеры с, снабженные крыльчатыми поршн ми d, приводимыми в движение гайками, заключенными в эксцентрик g, установленный на валу О. Камеры с снабженьГ форсунками S дл  подачи в них горючего и окнами « с |томещенными-за ними обратными клапанами, через которые всасываетс  воздух, сжимаемый в камерах поршн ми d, служащими дл  нагнетани  горючей смеси и дл  выпуска образовавшихс  при горении ее газов в каналы т (фиг. 2), направл ющие их на лопатки b турбинного диска. В дальИ . С./ On the shaft O there is a turbine disk with blades in, around which there are hemispherical chambers equipped with wing pistons d, driven by nuts enclosed in an eccentric g mounted on the shaft O. Chambers with a supply of nozzles S for feeding fuel into them and windows "With back-mounted check valves behind them, through which air is compressed, the pistons d are compressed in the chambers, which serve to inject the combustible mixture and to release the gases formed during its combustion into the channels (Fig. 2), which direct them to the blades b turbine about the disk. In the distance. WITH./

нейшем своем движении газы поступают в трубы v (фиг. 1), ведущие их в осевые турбины В, сид щие на валу О. Кроме того, газы через краны и могут быть направлены под паровой котел дл  дальнейшего их использовани . Дл  работы турбины паром последний подводитс  к отверсти м/(фиг. 2), ведущим его в каналы т, из которых он поп; дает на рабочие лопатки b и дальше, проход  осевые турбины В, направл етс  В| конденсатор .In its slowest movement, the gases enter the tubes v (Fig. 1), which drive them into the axial turbines B, which sit on the shaft O. In addition, the gases pass through the taps and can be directed under the steam boiler for their further use. For turbine operation, the steam is supplied to the openings m / (Fig. 2), leading it to the channels t, from which it pops; gives the blades b and farther, the passage axial turbines B, is directed B | capacitor.

Предмет изобретени .The subject matter of the invention.

Турбина внутреннего горени , отличающа с  применением полушаровых камер с, расположенных по сторонам венца лопаток b вокруг него и снабженных крыльчатыми поршн ми d, приводимыми в движение гайками, заключенными в эксцентрик g, каковые поршни предназначены дл  всасывани  воздуха через окна п, за которыми помещаютс  обратные клапаны сжимани  его в камерах с, в которые горючее вводитс  форсунками S и из которых продукты горени  направл ютс  по каналам т на рабочие лопатки Ь, а затем через трубы v- в осевые турбины В или через крацы и под паровой котел дл  - дальнейшего использовани . :;- - с- : ; Internal combustion turbine, characterized with the use of hemispherical chambers c, located on the sides of the crown of blades b around it and provided with winged pistons d, driven by nuts, enclosed in an eccentric g, which pistons are designed to suck air through windows n, behind which are placed back valves are clamped in chambers c into which fuel is injected by nozzles S and from which combustion products are directed through channels t to work blades b, and then through pipes v to axial turbines B or through edges and steam. Boiler for howling - further use. :;- - with- : ;

SU13897A 1927-01-04 1927-01-04 Internal combustion turbine SU22406A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU13897A SU22406A1 (en) 1927-01-04 1927-01-04 Internal combustion turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU13897A SU22406A1 (en) 1927-01-04 1927-01-04 Internal combustion turbine

Related Child Applications (1)

Application Number Title Priority Date Filing Date
SU52823A Addition SU15230A1 (en) 1929-08-12 1929-08-12 Device for determining the depth of indentation of a ball in a Brinel device for determining the hardness of metals

Publications (1)

Publication Number Publication Date
SU22406A1 true SU22406A1 (en) 1931-08-31

Family

ID=48341207

Family Applications (1)

Application Number Title Priority Date Filing Date
SU13897A SU22406A1 (en) 1927-01-04 1927-01-04 Internal combustion turbine

Country Status (1)

Country Link
SU (1) SU22406A1 (en)

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