AU2706699A - Multi-stage axial compressor for aircraft engines - Google Patents

Multi-stage axial compressor for aircraft engines

Info

Publication number
AU2706699A
AU2706699A AU27066/99A AU2706699A AU2706699A AU 2706699 A AU2706699 A AU 2706699A AU 27066/99 A AU27066/99 A AU 27066/99A AU 2706699 A AU2706699 A AU 2706699A AU 2706699 A AU2706699 A AU 2706699A
Authority
AU
Australia
Prior art keywords
aircraft engines
axial compressor
stage axial
stage
compressor
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
AU27066/99A
Inventor
Vladimir Iosifovich Belous
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of AU2706699A publication Critical patent/AU2706699A/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Feedback Control In General (AREA)
AU27066/99A 1998-03-17 1999-03-11 Multi-stage axial compressor for aircraft engines Abandoned AU2706699A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
BY19980250 1998-03-17
BY19980250 1998-03-17
PCT/BY1999/000003 WO1999047815A1 (en) 1998-03-17 1999-03-11 Multi-stage axial compressor for aircraft engines

Publications (1)

Publication Number Publication Date
AU2706699A true AU2706699A (en) 1999-10-11

Family

ID=4083719

Family Applications (1)

Application Number Title Priority Date Filing Date
AU27066/99A Abandoned AU2706699A (en) 1998-03-17 1999-03-11 Multi-stage axial compressor for aircraft engines

Country Status (4)

Country Link
AU (1) AU2706699A (en)
RU (1) RU2165547C2 (en)
UA (1) UA40584C2 (en)
WO (1) WO1999047815A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013109159A1 (en) * 2012-01-19 2013-07-25 Panchenko Vladimir Mitrofanovich Rotary screw engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1389347A (en) * 1972-05-25 1975-04-03 Rolls Royce Gas turbine power plant
GB1415679A (en) * 1972-11-17 1975-11-26 Rolls Royce Gas turbine engine powerplant
US4587803A (en) * 1983-08-15 1986-05-13 Rolls-Royce Inc. Valve for diverting fluid flows in turbomachines
SU1394790A1 (en) * 1986-06-06 1996-03-10 В.П. Абруков Method of control of gas-turbine engine multi-stage compressor

Also Published As

Publication number Publication date
UA40584C2 (en) 2001-08-15
RU2165547C2 (en) 2001-04-20
WO1999047815A1 (en) 1999-09-23

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase