FR3023584B1 - Turbomachine a double flux equipee de moyens de mesure d'un parametre - Google Patents

Turbomachine a double flux equipee de moyens de mesure d'un parametre

Info

Publication number
FR3023584B1
FR3023584B1 FR1456563A FR1456563A FR3023584B1 FR 3023584 B1 FR3023584 B1 FR 3023584B1 FR 1456563 A FR1456563 A FR 1456563A FR 1456563 A FR1456563 A FR 1456563A FR 3023584 B1 FR3023584 B1 FR 3023584B1
Authority
FR
France
Prior art keywords
parameter
measuring
double flow
flow turbomachine
turbomachine equipped
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.)
Active
Application number
FR1456563A
Other languages
English (en)
Other versions
FR3023584A1 (fr
Inventor
Thierry Kohn
Ceulen Sylvain Van
Nicolas Aussedat
Yann Linee
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1456563A priority Critical patent/FR3023584B1/fr
Publication of FR3023584A1 publication Critical patent/FR3023584A1/fr
Application granted granted Critical
Publication of FR3023584B1 publication Critical patent/FR3023584B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/02—Arrangement of sensing elements
    • F01D17/08—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure
    • F01D17/085—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure to temperature
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling combustion
    • F23N5/02—Systems for controlling combustion using devices responsive to thermal changes or to thermal expansion of a medium
    • F23N5/10—Systems for controlling combustion using devices responsive to thermal changes or to thermal expansion of a medium using thermocouples
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2241/00—Applications
    • F23N2241/20—Gas turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2900/00—Special features of, or arrangements for controlling combustion
    • F23N2900/05005—Mounting arrangements for sensing, detecting or measuring devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Measuring Temperature Or Quantity Of Heat (AREA)
FR1456563A 2014-07-08 2014-07-08 Turbomachine a double flux equipee de moyens de mesure d'un parametre Active FR3023584B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1456563A FR3023584B1 (fr) 2014-07-08 2014-07-08 Turbomachine a double flux equipee de moyens de mesure d'un parametre

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1456563A FR3023584B1 (fr) 2014-07-08 2014-07-08 Turbomachine a double flux equipee de moyens de mesure d'un parametre

Publications (2)

Publication Number Publication Date
FR3023584A1 FR3023584A1 (fr) 2016-01-15
FR3023584B1 true FR3023584B1 (fr) 2016-08-12

Family

ID=51726691

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1456563A Active FR3023584B1 (fr) 2014-07-08 2014-07-08 Turbomachine a double flux equipee de moyens de mesure d'un parametre

Country Status (1)

Country Link
FR (1) FR3023584B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
PT3809829T (pt) * 2018-06-21 2022-10-06 Univ Amsterdam Uso de microalgas verdes para melhorar o crescimento de plantas
CN112576409A (zh) * 2020-12-03 2021-03-30 上海新力动力设备研究所 一种固体火箭发动机的燃烧室壳体

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6094904A (en) * 1998-07-16 2000-08-01 United Technologies Corporation Fuel injector with a replaceable sensor
US7128818B2 (en) * 2002-01-09 2006-10-31 General Electric Company Method and apparatus for monitoring gases in a combustion system
US8794005B2 (en) * 2006-12-21 2014-08-05 Pratt & Whitney Canada Corp. Combustor construction
US8018590B2 (en) * 2008-10-23 2011-09-13 General Electric Company Three-dimensional optical sensor and system for combustion sensing and control
EP2357339A1 (fr) * 2010-02-12 2011-08-17 Siemens Aktiengesellschaft Procédé de détermination de la température de sortie d'une chambre de combustion et procédé de commande de turbine à gaz

Also Published As

Publication number Publication date
FR3023584A1 (fr) 2016-01-15

Similar Documents

Publication Publication Date Title
DK3734236T3 (da) Flowmåler med en målekanal
GB2522581B (en) Turbine fluid velocity field measurement
PL2971609T3 (pl) Pierścień turbiny do maszyny wirowej
GB2532142B (en) Turbine wheel for a turbine engine
FR3011888B1 (fr) Piece de turbomachine a surface non-axisymetrique
GB2532585B (en) Turbine fluid velocity field measurement
GB2541605B (en) Lubrication device for a turbine engine
GB201500257D0 (en) A flow meter
IL260838B (en) Probe with no moving parts for a tank
GB201817897D0 (en) Flow measurement device for a structure
GB2558072B (en) Turbine for a turbine engine
PL2992183T3 (pl) Zawór do maszyny przepływowej
FR3001037B1 (fr) Calorimetre differentiel a mesure de flux
GB2534268B (en) Turbine wheel for a turbine engine
FR3005992B1 (fr) Dispositif de passage de servitudes pour une turbomachine
GB2530669B (en) Turbine wheel for a turbine engine
GB2533223B (en) Impeller having spoilers for a turbine engine turbine
GB2531521B (en) A fluid conduit for a gas turbine engine
FR3028315B1 (fr) Systeme ameliore de mesure du taux de gaz dans un ecoulement fluide
FR3018849B1 (fr) Piece de revolution pour un rotor de turbomachine
BR112015018886A2 (pt) método para medir a taxa de perda óssea.
FR3023584B1 (fr) Turbomachine a double flux equipee de moyens de mesure d'un parametre
DK3259472T3 (da) Styring for en vindmølle
EP3783200C0 (fr) Conduit de transition pour turbine à gaz
EP2954167A4 (fr) Film amovible pour surfaces de profil aérodynamique

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20160115

RM Correction of a material error

Effective date: 20160404

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11