DE112016001339A5 - DEVICE FOR STABILIZING THE ENGINE INJECTION FLOW IN ENGINE STANDS AND / OR FOR REDUCING FLOW SAVINGS AND PRESSURE FLUCTURES IN ENGINE ENTRY IN STATIONS, DEVICE FOR SUPPORTING STATIONS FOR AIRCRAFT GEARWAYS, AND USE OF A DEVICE - Google Patents

DEVICE FOR STABILIZING THE ENGINE INJECTION FLOW IN ENGINE STANDS AND / OR FOR REDUCING FLOW SAVINGS AND PRESSURE FLUCTURES IN ENGINE ENTRY IN STATIONS, DEVICE FOR SUPPORTING STATIONS FOR AIRCRAFT GEARWAYS, AND USE OF A DEVICE Download PDF

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Publication number
DE112016001339A5
DE112016001339A5 DE112016001339.6T DE112016001339T DE112016001339A5 DE 112016001339 A5 DE112016001339 A5 DE 112016001339A5 DE 112016001339 T DE112016001339 T DE 112016001339T DE 112016001339 A5 DE112016001339 A5 DE 112016001339A5
Authority
DE
Germany
Prior art keywords
engine
stations
gearways
fluctures
aircraft
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.)
Withdrawn
Application number
DE112016001339.6T
Other languages
German (de)
Inventor
Bernd Konrath
Horst Meessen
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.)
I F I Inst fur Industrieaerodynamik GmbH
Ifi Institut fur Industrieaerodynamik GmbH
Original Assignee
I F I Inst fur Industrieaerodynamik GmbH
Ifi Institut fur Industrieaerodynamik GmbH
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 I F I Inst fur Industrieaerodynamik GmbH, Ifi Institut fur Industrieaerodynamik GmbH filed Critical I F I Inst fur Industrieaerodynamik GmbH
Publication of DE112016001339A5 publication Critical patent/DE112016001339A5/en
Withdrawn legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00—Testing of engines
    • G01M15/14—Testing gas-turbine engines or jet-propulsion engines
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00—Testing of engines
    • G01M15/02—Details or accessories of testing apparatus

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Tires In General (AREA)
  • Testing Of Engines (AREA)
  • Measuring Fluid Pressure (AREA)
DE112016001339.6T 2015-03-23 2016-03-23 DEVICE FOR STABILIZING THE ENGINE INJECTION FLOW IN ENGINE STANDS AND / OR FOR REDUCING FLOW SAVINGS AND PRESSURE FLUCTURES IN ENGINE ENTRY IN STATIONS, DEVICE FOR SUPPORTING STATIONS FOR AIRCRAFT GEARWAYS, AND USE OF A DEVICE Withdrawn DE112016001339A5 (en)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
DE102015003562.2 2015-03-23
DE102015003562 2015-03-23
DE102015009714 2015-08-01
DE102015009714.8 2015-08-01
DE102015010484.5 2015-08-17
DE102015010484.5A DE102015010484A1 (en) 2015-03-23 2015-08-17 Device for stabilizing the engine inlet flow in engine stands and / or to reduce flow separation and pressure fluctuations in the engine entrance to stand runs, apparatus for supporting stands for aircraft engines and use of a device
PCT/DE2016/000127 WO2016150423A2 (en) 2015-03-23 2016-03-23 Device for stabilizing the engine inlet flow in static tests of engines and/or for reducing stall and pressure fluctuations in the engine inlet in static tests, device for supporting static tests for aircraft engines, and use of a device

Publications (1)

Publication Number Publication Date
DE112016001339A5 true DE112016001339A5 (en) 2017-11-30

Family

ID=56889640

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102015010484.5A Withdrawn DE102015010484A1 (en) 2015-03-23 2015-08-17 Device for stabilizing the engine inlet flow in engine stands and / or to reduce flow separation and pressure fluctuations in the engine entrance to stand runs, apparatus for supporting stands for aircraft engines and use of a device
DE112016001339.6T Withdrawn DE112016001339A5 (en) 2015-03-23 2016-03-23 DEVICE FOR STABILIZING THE ENGINE INJECTION FLOW IN ENGINE STANDS AND / OR FOR REDUCING FLOW SAVINGS AND PRESSURE FLUCTURES IN ENGINE ENTRY IN STATIONS, DEVICE FOR SUPPORTING STATIONS FOR AIRCRAFT GEARWAYS, AND USE OF A DEVICE

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102015010484.5A Withdrawn DE102015010484A1 (en) 2015-03-23 2015-08-17 Device for stabilizing the engine inlet flow in engine stands and / or to reduce flow separation and pressure fluctuations in the engine entrance to stand runs, apparatus for supporting stands for aircraft engines and use of a device

Country Status (2)

Country Link
DE (2) DE102015010484A1 (en)
WO (1) WO2016150423A2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3073287B1 (en) * 2017-11-08 2020-10-02 Safran Aircraft Engines IMPROVED GROUND TEST DEVICE FOR TURBOMACHINE

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1582107A (en) * 1968-06-12 1969-09-26
CH518214A (en) * 1970-03-12 1972-01-31 Swissair Soundproofing system for aircraft on the ground
US4258823A (en) * 1979-01-02 1981-03-31 The Boeing Company Inflow turbulence control structure
US4691561A (en) * 1986-06-13 1987-09-08 The Boeing Company Inflow control device for engine testing
FR2683321B1 (en) 1991-11-06 1994-02-11 Boet Sa Andre GROUND TEST INSTALLATION FOR REACTORS OF A LARGE-CARRYING AIRCRAFT.
US5293775A (en) * 1992-11-02 1994-03-15 United Technologies Corporation Gas turbine engine test cell
US5396793A (en) * 1993-09-17 1995-03-14 United Technologies Corporation Altitude gas turbine engine test cell
DE4335872A1 (en) 1993-10-21 1995-04-27 Rheinhold & Mahla Ag Device for weakening intake vortices on turbine engines
DE19743591C2 (en) 1997-10-02 1999-12-16 Daimler Chrysler Aerospace Device for stabilizing the engine inlet flow in engine stationary runs
GB2337301B (en) * 1998-05-14 2000-11-08 Richard Adkins Improved aircraft run-up pen
GB2339242B (en) * 1998-07-06 2001-01-24 Richard Adkins Intake shields
JP2002166896A (en) * 2000-11-29 2002-06-11 Kawasaki Heavy Ind Ltd Ground test method for aircraft and air intake straightening duct used therefor
US6910370B2 (en) * 2002-05-22 2005-06-28 United Technologies Corporation Apparatus and method for preventing inlet vortex
DE10337372B4 (en) 2003-08-13 2005-08-04 Airbus Deutschland Gmbh Device for stabilizing the engine inlet flow in engine stands
US20090100918A1 (en) * 2007-09-26 2009-04-23 United Technologies Corp. Systems and Methods for Testing Gas Turbine Engines

Also Published As

Publication number Publication date
WO2016150423A2 (en) 2016-09-29
WO2016150423A3 (en) 2016-11-10
WO2016150423A9 (en) 2017-03-30
DE102015010484A1 (en) 2016-09-29

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Legal Events

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R082 Change of representative

Representative=s name: FARAGO PATENTANWAELTE, DE

Representative=s name: FARAGO PATENTANWALTS- UND RECHTSANWALTSGESELLS, DE

R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee