FR2962213B1 - Systeme de dosage de debit massique pour applications d'avion - Google Patents
Systeme de dosage de debit massique pour applications d'avion Download PDFInfo
- Publication number
- FR2962213B1 FR2962213B1 FR1155165A FR1155165A FR2962213B1 FR 2962213 B1 FR2962213 B1 FR 2962213B1 FR 1155165 A FR1155165 A FR 1155165A FR 1155165 A FR1155165 A FR 1155165A FR 2962213 B1 FR2962213 B1 FR 2962213B1
- Authority
- FR
- France
- Prior art keywords
- mass flow
- dosing system
- aircraft applications
- flow dosing
- 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.)
- Expired - Fee Related
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
- G01F1/05—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects
- G01F1/34—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects by measuring pressure or differential pressure
- G01F1/36—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects by measuring pressure or differential pressure the pressure or differential pressure being created by the use of flow constriction
- G01F1/363—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects by measuring pressure or differential pressure the pressure or differential pressure being created by the use of flow constriction with electrical or electro-mechanical indication
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Volume Flow (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12815575 | 2010-06-15 | ||
US12/815,575 US20110307192A1 (en) | 2010-06-15 | 2010-06-15 | Mass flow metering system for aircraft applications |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2962213A1 FR2962213A1 (fr) | 2012-01-06 |
FR2962213B1 true FR2962213B1 (fr) | 2018-08-10 |
Family
ID=45096902
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1155165A Expired - Fee Related FR2962213B1 (fr) | 2010-06-15 | 2011-06-14 | Systeme de dosage de debit massique pour applications d'avion |
Country Status (3)
Country | Link |
---|---|
US (1) | US20110307192A1 (fr) |
CA (1) | CA2742333A1 (fr) |
FR (1) | FR2962213B1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9207108B2 (en) | 2012-01-26 | 2015-12-08 | Hamilton Sundstrand Corporation | Fluid mass flow measurement apparatus and method |
DE102014119210A1 (de) * | 2014-12-19 | 2016-06-23 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zur Ermittlung eines Treibstofflecks eines Treibstoffsystems eines wenigstens zwei Triebwerke aufweisenden Flugzeugs |
GB202205347D0 (en) * | 2022-04-12 | 2022-05-25 | Rolls Royce Plc | Propulsion system |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3772915A (en) * | 1970-10-27 | 1973-11-20 | Cons Airborne Systems | Density corrected flowmeter |
GB8907788D0 (en) * | 1989-04-06 | 1989-05-17 | Rolls Royce Plc | Management of heat generated by aircraft gas turbine installations |
GB8911806D0 (en) * | 1989-05-23 | 1989-07-12 | Rolls Royce Plc | Gas turbine engine fuel control system with enhanced relight capability |
US5111653A (en) * | 1990-04-11 | 1992-05-12 | Woodward Governor Company | Fuel delivery system with capacity monitor |
US6487847B1 (en) * | 2000-11-03 | 2002-12-03 | General Electric Company | Gas turbine engine fuel control system |
US6748744B2 (en) * | 2001-11-21 | 2004-06-15 | Pratt & Whitney Canada Corp. | Method and apparatus for the engine control of output shaft speed |
GB0329626D0 (en) * | 2003-12-23 | 2004-01-28 | Goodrich Control Sys Ltd | Fuel system |
US7739004B2 (en) * | 2006-11-29 | 2010-06-15 | The Boeing Company | Automatic engine fuel flow monitoring and alerting fuel leak detection method |
-
2010
- 2010-06-15 US US12/815,575 patent/US20110307192A1/en not_active Abandoned
-
2011
- 2011-06-06 CA CA2742333A patent/CA2742333A1/fr not_active Abandoned
- 2011-06-14 FR FR1155165A patent/FR2962213B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CA2742333A1 (fr) | 2011-12-15 |
FR2962213A1 (fr) | 2012-01-06 |
US20110307192A1 (en) | 2011-12-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 5 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20160429 |
|
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: 10 |
|
ST | Notification of lapse |
Effective date: 20220205 |