FR1134891A - Regulator - Google Patents

Regulator

Info

Publication number
FR1134891A
FR1134891A FR1134891DA FR1134891A FR 1134891 A FR1134891 A FR 1134891A FR 1134891D A FR1134891D A FR 1134891DA FR 1134891 A FR1134891 A FR 1134891A
Authority
FR
France
Prior art keywords
regulator
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
Application number
Other languages
French (fr)
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Application granted granted Critical
Publication of FR1134891A publication Critical patent/FR1134891A/en
Expired legal-status Critical Current

Links

FR1134891D 1954-07-28 1955-07-27 Regulator Expired FR1134891A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1134891XA 1954-07-28 1954-07-28

Publications (1)

Publication Number Publication Date
FR1134891A true FR1134891A (en) 1957-04-18

Family

ID=22349747

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1134891D Expired FR1134891A (en) 1954-07-28 1955-07-27 Regulator

Country Status (1)

Country Link
FR (1) FR1134891A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3076310A (en) * 1958-09-01 1963-02-05 Rolls Royce Gas turbine engine fuel system
FR2126937A1 (en) * 1971-02-04 1972-10-13 Bronzavia Sa
FR2610040A1 (en) * 1987-01-28 1988-07-29 Snecma MODULAR REGULATION SUB-ASSEMBLY WITH LOAD LOSS DETECTOR AND INTEGRATED OVERSPEED LIMITER
FR2610041A1 (en) * 1987-01-28 1988-07-29 Snecma ENHANCED FUEL ASSAY REGULATING ASSEMBLY, IN PARTICULAR FOR TURBOMACHINES

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3076310A (en) * 1958-09-01 1963-02-05 Rolls Royce Gas turbine engine fuel system
FR2126937A1 (en) * 1971-02-04 1972-10-13 Bronzavia Sa
FR2610040A1 (en) * 1987-01-28 1988-07-29 Snecma MODULAR REGULATION SUB-ASSEMBLY WITH LOAD LOSS DETECTOR AND INTEGRATED OVERSPEED LIMITER
FR2610041A1 (en) * 1987-01-28 1988-07-29 Snecma ENHANCED FUEL ASSAY REGULATING ASSEMBLY, IN PARTICULAR FOR TURBOMACHINES
EP0278814A1 (en) * 1987-01-28 1988-08-17 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Fuel dose regulating device for turbo machines
EP0278833A1 (en) * 1987-01-28 1988-08-17 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Pressure-drop regulating device with an integrated speed limiter
US4817376A (en) * 1987-01-28 1989-04-04 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Modular sub-assembly for turbine engine fuel control systems

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