IT1084621B - Rivelatore di temperatura transistoria di aria specialmente adatto a turbomotori a gas. - Google Patents
Rivelatore di temperatura transistoria di aria specialmente adatto a turbomotori a gas.Info
- Publication number
- IT1084621B IT1084621B IT22856/77A IT2285677A IT1084621B IT 1084621 B IT1084621 B IT 1084621B IT 22856/77 A IT22856/77 A IT 22856/77A IT 2285677 A IT2285677 A IT 2285677A IT 1084621 B IT1084621 B IT 1084621B
- Authority
- IT
- Italy
- Prior art keywords
- air
- temperature detector
- especially suitable
- gas turbo
- transistor temperature
- Prior art date
Links
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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K13/00—Thermometers specially adapted for specific purposes
- G01K13/02—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
- G01K13/028—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow for use in total air temperature [TAT] probes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Measuring Temperature Or Quantity Of Heat (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Measuring Fluid Pressure (AREA)
- Measuring Volume Flow (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/680,909 US4047379A (en) | 1976-04-28 | 1976-04-28 | Transient air temperature sensing system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IT1084621B true IT1084621B (it) | 1985-05-25 |
Family
ID=24733018
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT22856/77A IT1084621B (it) | 1976-04-28 | 1977-04-27 | Rivelatore di temperatura transistoria di aria specialmente adatto a turbomotori a gas. |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4047379A (OSRAM) |
| JP (1) | JPS605776B2 (OSRAM) |
| DE (1) | DE2718663A1 (OSRAM) |
| FR (1) | FR2354449A1 (OSRAM) |
| GB (1) | GB1515499A (OSRAM) |
| IT (1) | IT1084621B (OSRAM) |
Families Citing this family (48)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4351150A (en) * | 1980-02-25 | 1982-09-28 | General Electric Company | Auxiliary air system for gas turbine engine |
| GB2089035B (en) * | 1980-12-06 | 1984-10-24 | Rolls Royce | Temperature sensor |
| GB2124706B (en) * | 1982-08-04 | 1986-05-14 | Gen Electric | Gas turbine engine airflow temperature sensor |
| US4685942A (en) * | 1982-12-27 | 1987-08-11 | General Electric Company | Axial flow inlet particle separator |
| US4608819A (en) * | 1983-12-27 | 1986-09-02 | General Electric Company | Gas turbine engine component cooling system |
| US5018873A (en) * | 1985-04-22 | 1991-05-28 | General Electric Company | Air temperature measurement |
| US4644806A (en) * | 1985-04-22 | 1987-02-24 | General Electric Company | Airstream eductor |
| US4668102A (en) * | 1985-05-08 | 1987-05-26 | Honeywell Inc. | Temperature and flow station |
| US4770544A (en) * | 1985-11-15 | 1988-09-13 | General Electric Company | Temperature sensor |
| US4948264A (en) * | 1986-07-07 | 1990-08-14 | Hook Jr Richard B | Apparatus for indirectly determining the temperature of a fluid |
| US4783026A (en) * | 1987-05-22 | 1988-11-08 | Avco Corporation | Anti-icing management system |
| IL84611A (en) * | 1987-11-26 | 1991-11-21 | Ardon Gador | Apparatus and method for protection against heat |
| US5040380A (en) * | 1988-08-04 | 1991-08-20 | Super S.E.E.R. Systems Inc. | Method and apparatus for the sensing of refrigerant temperatures and the control of refrigerant loading |
| US5182906A (en) * | 1990-10-22 | 1993-02-02 | General Electric Company | Hybrid spinner nose configuration in a gas turbine engine having a bypass duct |
| US5220785A (en) * | 1991-07-15 | 1993-06-22 | United Technologies Corporation | Side discharge anti-ice manifold |
| US5302026A (en) * | 1992-07-16 | 1994-04-12 | Rosemount, Inc. | Temperature probe with fast response time |
| IL109388A0 (en) * | 1993-04-29 | 1994-07-31 | Rosemount Aerospace Inc | Temperature sensor with integral debris guard |
| US5397181A (en) * | 1993-10-21 | 1995-03-14 | General Electric Company | Compressor discharge temperature sensing system |
| US5653538A (en) * | 1995-06-07 | 1997-08-05 | Rosemount Aerospace Inc. | Total temperature probe |
| US5930990A (en) * | 1996-05-14 | 1999-08-03 | The Dow Chemical Company | Method and apparatus for achieving power augmentation in gas turbines via wet compression |
| US5867977A (en) * | 1996-05-14 | 1999-02-09 | The Dow Chemical Company | Method and apparatus for achieving power augmentation in gas turbines via wet compression |
| US6609825B2 (en) * | 2001-09-21 | 2003-08-26 | Rosemount Aerospace Inc. | Total air temperature probe providing improved anti-icing performance and reduced deicing heater error |
| US6827485B2 (en) * | 2002-07-16 | 2004-12-07 | Rosemount Aerospace Inc. | Fast response temperature sensor |
| ITMI20032586A1 (it) * | 2003-12-23 | 2005-06-24 | Nuovo Pignone Spa | Sistema di montaggio di una termocoppia per una turbina a gas |
| USD545227S1 (en) | 2005-09-20 | 2007-06-26 | Rosemount Aerospace Inc. | Total air temperature probe |
| US7357572B2 (en) * | 2005-09-20 | 2008-04-15 | Rosemount Aerospace Inc. | Total air temperature probe having improved deicing heater error performance |
| USD548634S1 (en) | 2005-09-20 | 2007-08-14 | Rosemount Aerospace Inc. | Total air temperature probe |
| JP4672565B2 (ja) * | 2006-02-06 | 2011-04-20 | 三菱重工業株式会社 | 温度計測装置、燃焼監視装置、及び、ガスタービン |
| US7313963B2 (en) * | 2006-02-28 | 2008-01-01 | General Electric Company | Isothermal de-iced sensor |
| US7328623B2 (en) | 2006-03-20 | 2008-02-12 | General Electric Company | Temperature and/or pressure sensor assembly |
| US20080047425A1 (en) * | 2006-08-23 | 2008-02-28 | United Technologies Corporation | Mission adaptable inlet particle separator |
| DE102006040757A1 (de) | 2006-08-31 | 2008-04-30 | Rolls-Royce Deutschland Ltd & Co Kg | Fluidrückführung im Trennkörper von Strömungsarbeitsmaschinen mit Nebenstromkonfiguration |
| US7828477B2 (en) * | 2007-05-14 | 2010-11-09 | Rosemount Aerospace Inc. | Aspirated enhanced total air temperature probe |
| RU2347089C1 (ru) * | 2007-06-13 | 2009-02-20 | Институт теоретической и прикладной механики им. С.А. Христиановича СО РАН (ИТПМ СО РАН) | Сверхзвуковой осесимметричный воздухозаборник (варианты) |
| US8392141B2 (en) * | 2009-11-02 | 2013-03-05 | Rosemount Aerospace Inc. | Total air temperature probe and method for reducing de-icing/anti-icing heater error |
| DE102010014900A1 (de) | 2010-04-14 | 2011-10-20 | Rolls-Royce Deutschland Ltd & Co Kg | Nebenstromkanal eines Turbofantriebwerkes |
| US8945254B2 (en) | 2011-12-21 | 2015-02-03 | General Electric Company | Gas turbine engine particle separator |
| US8452516B1 (en) | 2012-01-31 | 2013-05-28 | United Technologies Corporation | Variable vane scheduling based on flight conditions for inclement weather |
| US10202185B2 (en) | 2014-06-10 | 2019-02-12 | United Technologies Corporation | Geared turbofan with improved spinner |
| GB201416928D0 (en) * | 2014-09-25 | 2014-11-12 | Rolls Royce Plc | A gas turbine and a method of washing a gas turbine engine |
| US20160376010A1 (en) * | 2015-06-26 | 2016-12-29 | Rosemount Aerospace Inc. | Systems and methods for preventing ice accumulation |
| CN105114180A (zh) * | 2015-08-26 | 2015-12-02 | 成都博世德能源科技股份有限公司 | 一种用于燃气轮机的保温式进气系统 |
| US10605675B2 (en) * | 2017-06-22 | 2020-03-31 | Unison Industries, Llc | Air temperature sensor |
| US10578498B2 (en) * | 2017-06-22 | 2020-03-03 | Unison Industries, Llc | Air temperature sensor |
| US11143193B2 (en) * | 2019-01-02 | 2021-10-12 | Danfoss A/S | Unloading device for HVAC compressor with mixed and radial compression stages |
| US11840346B2 (en) * | 2022-03-28 | 2023-12-12 | Pratt & Whitney Canada Corp. | Strut for aircraft engine |
| US11821363B1 (en) * | 2022-05-06 | 2023-11-21 | Pratt & Whitney Canada Corp. | Apparatus for removing particulate matter from bleed gas and gas turbine engine including same |
| US11964223B1 (en) * | 2022-10-15 | 2024-04-23 | Beta Air, Llc | Methods and apparatus for an inertial separation of air in an electric aircraft |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE532567A (OSRAM) * | ||||
| GB734702A (en) * | 1952-12-16 | 1955-08-03 | Rolls Royce | Improvements in measuring gas temperatures |
| GB746596A (en) * | 1953-01-26 | 1956-03-14 | Rolls Royce | Improvements in or relating to gas turbine engines having multi-stage compressors |
| DE951239C (de) * | 1953-11-06 | 1956-10-25 | Sulzer Ag | Temperaturmesseinrichtung |
| US3000213A (en) * | 1955-08-08 | 1961-09-19 | Cook Electric Co | Fluid testing probe |
| CH357885A (de) * | 1960-05-06 | 1961-10-31 | Sulzer Ag | Anordnung zur Temperaturmessung eines durch eine Rohrleitung strömenden Mediums |
| US3167960A (en) * | 1961-08-07 | 1965-02-02 | Holley Carburetor Co | Temperature probe |
| GB1029522A (en) * | 1964-01-22 | 1966-05-11 | Bristol Siddeley Engines Ltd | Apparatus for measuring the temperature of a gas flow |
| US3512414A (en) * | 1968-05-23 | 1970-05-19 | Rosemount Eng Co Ltd | Slotted airfoil sensor housing |
| US3597920A (en) * | 1969-08-21 | 1971-08-10 | Chandler Evans Inc | Turbine inlet temperature sensor and computer |
| US3623367A (en) * | 1969-12-23 | 1971-11-30 | Westinghouse Electric Corp | Apparatus for measuring the average temperature of a gas stream |
| BE791726A (fr) * | 1971-11-23 | 1973-05-22 | Gen Electric | Separateur de particules avec dispositif de balayage en colimacon |
| US3832086A (en) * | 1971-11-23 | 1974-08-27 | Gen Electric | Particle separator with scroll scavenging means |
| US3940988A (en) * | 1974-03-11 | 1976-03-02 | John Zink Company | Velocity thermocouple |
-
1976
- 1976-04-28 US US05/680,909 patent/US4047379A/en not_active Expired - Lifetime
-
1977
- 1977-04-15 GB GB15767/77A patent/GB1515499A/en not_active Expired
- 1977-04-22 FR FR7712164A patent/FR2354449A1/fr active Granted
- 1977-04-26 JP JP52047467A patent/JPS605776B2/ja not_active Expired
- 1977-04-27 DE DE19772718663 patent/DE2718663A1/de active Granted
- 1977-04-27 IT IT22856/77A patent/IT1084621B/it active
Also Published As
| Publication number | Publication date |
|---|---|
| JPS52139815A (en) | 1977-11-22 |
| FR2354449A1 (fr) | 1978-01-06 |
| JPS605776B2 (ja) | 1985-02-14 |
| FR2354449B1 (OSRAM) | 1983-10-28 |
| DE2718663C2 (OSRAM) | 1989-02-09 |
| US4047379A (en) | 1977-09-13 |
| DE2718663A1 (de) | 1977-11-10 |
| GB1515499A (en) | 1978-06-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| IT1084621B (it) | Rivelatore di temperatura transistoria di aria specialmente adatto a turbomotori a gas. | |
| SE434076B (sv) | Gasturbinmotorkylsystem | |
| IT7824102A0 (it) | Turbomotore a gas e mezzi per raffreddare il medesimo. | |
| IT1089112B (it) | Registratore di turbomotori a gas | |
| NO801882L (no) | Pakning for gassturbinmotorer. | |
| SE7513778L (sv) | Anordning for kylning av en gasturbinmotors turbininloppsledskovlar | |
| IT7830214A0 (it) | Impianti di riciclo dei gas di scarico di motori. | |
| SE435415B (sv) | Forbrenningsmotor med avgasturbokompressor | |
| IT7926656A0 (it) | Turbina raffreddata ad aria per motore a turbina a gas. | |
| SE415385B (sv) | Gasturbinmotor | |
| AR211564A1 (es) | Camara de combustion para turbina de gas | |
| NL7502167A (nl) | Koelsysteem voor een gasturbine. | |
| AR213664A1 (es) | Turbina de gas | |
| IT1079420B (it) | Turbocompressore a gas di scarico | |
| BR7706043A (pt) | Meios para calculo da temperatura de entrada da turbina em um motor de turbina a gas | |
| NL7705363A (nl) | Heetgasmotor. | |
| SE421342B (sv) | Ljuddempare for luft- eller gasstromningar | |
| IT1130186B (it) | Sistema di combustione per turbina a gas a doppio stadio/doppio modo di funzionamento | |
| SE392950B (sv) | Gasreglage for forbrenningsmotor, serskilt for motorsag | |
| SE403393B (sv) | Gasturbin | |
| SE429675B (sv) | Vermevexlare for kylning av avgaserna fran en forbrenningsmotor | |
| IT1088161B (it) | Sistema di controllo per motori a turbina a gas | |
| NO144751C (no) | Avgassledning for turboladede forbrenningsmotorer | |
| NL7710880A (nl) | Uitlaatgasleiding. | |
| IT1063518B (it) | Sistema di utilizzazione della perdita di aria di raffreddamento in un turbomotore a gas |