RU93031249A - POWER POINT - Google Patents

POWER POINT

Info

Publication number
RU93031249A
RU93031249A RU93031249/06A RU93031249A RU93031249A RU 93031249 A RU93031249 A RU 93031249A RU 93031249/06 A RU93031249/06 A RU 93031249/06A RU 93031249 A RU93031249 A RU 93031249A RU 93031249 A RU93031249 A RU 93031249A
Authority
RU
Russia
Prior art keywords
rotation
axis
engines
parallel
main shafts
Prior art date
Application number
RU93031249/06A
Other languages
Russian (ru)
Other versions
RU2070982C1 (en
Inventor
В.Н. Волов А.Н. Осауленко
А.Ю. Волков
V.N. Volov A.N. Osaulenko
A.Ju. Volkov
Original Assignee
Осауленко В.Н.
Osaulenko V.N.
Filing date
Publication date
Application filed by Осауленко В.Н., Osaulenko V.N. filed Critical Осауленко В.Н.
Priority to RU93031249A priority Critical patent/RU2070982C1/en
Priority claimed from RU93031249A external-priority patent/RU2070982C1/en
Publication of RU93031249A publication Critical patent/RU93031249A/en
Application granted granted Critical
Publication of RU2070982C1 publication Critical patent/RU2070982C1/en

Links

Claims (1)

Использование: силовые установки, использующие несколько двигателей внутреннего сгорания с осями симметрии цилиндров, параллельными оси вращения коренного вала. Сущность изобретения: силовая установка содержит первый и второй двигатели внутреннего сгорания с турбокомпрессорами, топливными насосами, цилиндрами, поршнями, связанными с коренными валами. Корпуса двигателей установлены с образованием между наружными боковыми поверхностями промежуточного пространства, в котором размещены турбокомпрессоры и топливные насосы. Плоскости симметрии двигателей, проведенные через наибольшие осевые сечения двигателей и оси вращения коренных валов, образуют угол развала 30-120o, биссектриса которого проходит через ось вращения выходного звена редуктора. Оси вращения коренных валов двигателей могут быть как параллельны, так и не параллельны друг другу.Usage: power plants using multiple internal combustion engines with axes of symmetry of the cylinders parallel to the axis of rotation of the main shaft. The inventive power plant contains the first and second internal combustion engines with turbochargers, fuel pumps, cylinders, pistons associated with the main shafts. The engine housings are installed to form an intermediate space between the outer side surfaces in which the turbo-compressors and fuel pumps are located. The plane of symmetry of the engines, carried out through the largest axial sections of the engines and the axis of rotation of the main shafts, form a camber angle of 30-120 o , whose bisector passes through the axis of rotation of the output link of the gearbox. The axis of rotation of the main shafts of the engines can be both parallel and not parallel to each other.
RU93031249A 1993-06-24 1993-06-24 Power plant RU2070982C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU93031249A RU2070982C1 (en) 1993-06-24 1993-06-24 Power plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU93031249A RU2070982C1 (en) 1993-06-24 1993-06-24 Power plant

Publications (2)

Publication Number Publication Date
RU93031249A true RU93031249A (en) 1996-07-27
RU2070982C1 RU2070982C1 (en) 1996-12-27

Family

ID=20143239

Family Applications (1)

Application Number Title Priority Date Filing Date
RU93031249A RU2070982C1 (en) 1993-06-24 1993-06-24 Power plant

Country Status (1)

Country Link
RU (1) RU2070982C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009047343A1 (en) * 2009-12-01 2011-06-09 Deere & Company, Moline Drive arrangement and method for a work machine with two internal combustion engines

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DALBY et al. CORRESPONDENCE. THE PRESENT POSITION OF THE PRESSURE-CHARGED HEAVY OIL MACHINE.