IT1228547B - APPARATUS AND METHOD FOR CHECKING THE RELEASE LIMITS OF TURBINE ENGINES - Google Patents
APPARATUS AND METHOD FOR CHECKING THE RELEASE LIMITS OF TURBINE ENGINESInfo
- Publication number
- IT1228547B IT1228547B IT8721567A IT2156787A IT1228547B IT 1228547 B IT1228547 B IT 1228547B IT 8721567 A IT8721567 A IT 8721567A IT 2156787 A IT2156787 A IT 2156787A IT 1228547 B IT1228547 B IT 1228547B
- Authority
- IT
- Italy
- Prior art keywords
- checking
- turbine engines
- release limits
- limits
- release
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/02—Purpose of the control system to control rotational speed (n)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/05—Purpose of the control system to affect the output of the engine
- F05D2270/052—Torque
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/11—Purpose of the control system to prolong engine life
- F05D2270/112—Purpose of the control system to prolong engine life by limiting temperatures
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Control Of Eletrric Generators (AREA)
- Controls For Constant Speed Travelling (AREA)
- Catching Or Destruction (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US89268986A | 1986-08-04 | 1986-08-04 |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8721567A0 IT8721567A0 (en) | 1987-08-03 |
IT1228547B true IT1228547B (en) | 1991-06-20 |
Family
ID=25400361
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT8721567A IT1228547B (en) | 1986-08-04 | 1987-08-03 | APPARATUS AND METHOD FOR CHECKING THE RELEASE LIMITS OF TURBINE ENGINES |
Country Status (6)
Country | Link |
---|---|
JP (1) | JPS6345429A (en) |
BR (1) | BR8701672A (en) |
DE (1) | DE3725687A1 (en) |
FR (1) | FR2602270A1 (en) |
GB (1) | GB2193535A (en) |
IT (1) | IT1228547B (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8730187D0 (en) * | 1987-12-24 | 1988-02-03 | Rolls Royce Plc | Overspeed limiter for gas turbine aeroengine |
US5258505A (en) * | 1991-07-26 | 1993-11-02 | Canon Kabushiki Kaisha | Trisazo compounds, and dye compositions containing same |
GB2262623B (en) * | 1991-12-17 | 1995-04-26 | Rolls Royce Plc | Aircraft engine management system |
US6012676A (en) * | 1998-03-31 | 2000-01-11 | Sikorsky Aircraft Corporation | Integrated fire and flight control system with automatic engine torque limiting |
FR2878288B1 (en) * | 2004-11-25 | 2007-01-19 | Eurocopter France | METHOD AND DEVICE FOR OPTIMIZING THE PERFORMANCE ENVELOPE OF A TURBOMOTEUR |
FR2888287B1 (en) | 2005-07-07 | 2011-04-08 | Eurocopter France | METHOD OF OPTIMIZING THE PERFOMANCE ENVELOPE OF A TURBOMOTEUR |
DE102009016106A1 (en) * | 2009-02-20 | 2010-08-26 | Rolls-Royce Deutschland Ltd & Co Kg | Method for determining rotational speed of e.g. low pressure shaft of aircraft engine, involves producing rotational speed signals for rotary shaft by magnetic coding of shaft and recognizing and evaluating signals by two signal sensors |
DE102009016105B4 (en) * | 2009-02-20 | 2017-11-16 | Rolls-Royce Deutschland Ltd & Co Kg | Method and device for measuring the load of rotating shafts |
FR2966881B1 (en) | 2010-10-29 | 2013-08-30 | Eurocopter France | MOTOR INSTALLATION OF AN AIRCRAFT, AIRCRAFT AND METHOD FOR CONTROLLING SAID AIRCRAFT. |
FR2985715B1 (en) | 2012-01-12 | 2013-12-27 | Eurocopter France | AIRCRAFT AIRCRAFT INSTALLATION, AIRCRAFT AND METHOD FOR CONTROLLING SAID AIRCRAFT |
US9771167B2 (en) | 2013-01-16 | 2017-09-26 | Airbus Helicopters | Monitor system for monitoring the starting of a rotary wing aircraft, an aircraft, and a method using the system |
FR3000989A1 (en) | 2013-01-16 | 2014-07-18 | Eurocopter France | SYSTEM FOR MONITORING THE STARTING OF AN AIRCRAFT WITH A TURNING SAIL, AIRCRAFT AND METHOD IMPLEMENTING SAID SYSTEM |
FR3034403B1 (en) | 2015-03-31 | 2017-03-31 | Airbus Helicopters | METHOD AND DEVICE FOR STOPPING A TURBOMOTER IN NOMINAL OPERATION |
-
1987
- 1987-04-09 BR BR8701672A patent/BR8701672A/en unknown
- 1987-07-31 FR FR8710936A patent/FR2602270A1/en not_active Withdrawn
- 1987-08-03 IT IT8721567A patent/IT1228547B/en active
- 1987-08-03 DE DE3725687A patent/DE3725687A1/en not_active Withdrawn
- 1987-08-03 GB GB08718303A patent/GB2193535A/en not_active Withdrawn
- 1987-08-04 JP JP62195137A patent/JPS6345429A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
JPS6345429A (en) | 1988-02-26 |
BR8701672A (en) | 1988-01-05 |
GB2193535A (en) | 1988-02-10 |
FR2602270A1 (en) | 1988-02-05 |
DE3725687A1 (en) | 1988-02-18 |
IT8721567A0 (en) | 1987-08-03 |
GB8718303D0 (en) | 1987-09-09 |
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