MD2023C2 - Turbomachine (variants) - Google Patents

Turbomachine (variants)

Info

Publication number
MD2023C2
MD2023C2 MDA20010072A MD20010072A MD2023C2 MD 2023 C2 MD2023 C2 MD 2023C2 MD A20010072 A MDA20010072 A MD A20010072A MD 20010072 A MD20010072 A MD 20010072A MD 2023 C2 MD2023 C2 MD 2023C2
Authority
MD
Moldova
Prior art keywords
turbomachine
gear
satellite
blades
rotor
Prior art date
Application number
MDA20010072A
Other languages
Romanian (ro)
Russian (ru)
Other versions
MD2023B2 (en
Inventor
Ион БОСТАН
Валериу ДУЛГЕРУ
Раду ЧУПЕРКЭ
Original Assignee
Технический университет Молдовы
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 Технический университет Молдовы filed Critical Технический университет Молдовы
Priority to MDA20010072A priority Critical patent/MD2023C2/en
Publication of MD2023B2 publication Critical patent/MD2023B2/en
Publication of MD2023C2 publication Critical patent/MD2023C2/en

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The invention relates to the mechanical engineering, in particular to a gas turbomachine.The turbomachine includes a body 1, wherein there are placed a rotor 3 with blades 4, the hub inclined flanges 5 of which are placed between the gear rings 7 and 8 of the satellite gear unit 9, being in engagement with the teeth of the central wheels 10 and 11, the last of which is installed onto the driven shaft 12. The hot gas fed through the nozzle 15 acts upon the blades 4, sets in rotation the rotor 3 and through the hub inclined flanges 5 is transmitted to the satellite unit converting into a precession motion. As a result of engagement of the gear rings 7 and 8 of the satellite unit 9 with the central gear wheels 10 and 11, the driven shaft 12 will rotate with the preset reduction degree.The result consists in expanding the functional possibilities and in reducing the overall dimensions.Fig: 2
MDA20010072A 2001-03-20 2001-03-20 Turbomachine (variants) MD2023C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
MDA20010072A MD2023C2 (en) 2001-03-20 2001-03-20 Turbomachine (variants)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
MDA20010072A MD2023C2 (en) 2001-03-20 2001-03-20 Turbomachine (variants)

Publications (2)

Publication Number Publication Date
MD2023B2 MD2023B2 (en) 2002-10-31
MD2023C2 true MD2023C2 (en) 2003-05-31

Family

ID=19739781

Family Applications (1)

Application Number Title Priority Date Filing Date
MDA20010072A MD2023C2 (en) 2001-03-20 2001-03-20 Turbomachine (variants)

Country Status (1)

Country Link
MD (1) MD2023C2 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1511437A1 (en) * 1988-01-19 1989-09-30 Производственное Объединение Атомного Турбостроения "Харьковский Турбинный Завод" Им.С.М.Кирова Turbomachine stage
US6189311B1 (en) * 1999-03-11 2001-02-20 Alm Development, Inc. Gas turbine engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1511437A1 (en) * 1988-01-19 1989-09-30 Производственное Объединение Атомного Турбостроения "Харьковский Турбинный Завод" Им.С.М.Кирова Turbomachine stage
US6189311B1 (en) * 1999-03-11 2001-02-20 Alm Development, Inc. Gas turbine engine

Also Published As

Publication number Publication date
MD2023B2 (en) 2002-10-31

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Legal Events

Date Code Title Description
KA4A Patent for invention lapsed due to non-payment of fees (with right of restoration)
MM4A Patent for invention definitely lapsed due to non-payment of fees