FR886790A - Remote control of aircraft engines by combined hydraulic and electrical devices - Google Patents

Remote control of aircraft engines by combined hydraulic and electrical devices

Info

Publication number
FR886790A
FR886790A FR886790DA FR886790A FR 886790 A FR886790 A FR 886790A FR 886790D A FR886790D A FR 886790DA FR 886790 A FR886790 A FR 886790A
Authority
FR
France
Prior art keywords
remote control
electrical devices
aircraft engines
combined hydraulic
hydraulic
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.)
BMW Flugmotorenbau GmbH
Original Assignee
BMW Flugmotorenbau GmbH
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 BMW Flugmotorenbau GmbH filed Critical BMW Flugmotorenbau GmbH
Application granted granted Critical
Publication of FR886790A publication Critical patent/FR886790A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B9/00Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/02Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type
    • F15B9/08Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor
    • F15B9/09Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor with electrical control means
FR886790D 1941-10-28 1942-10-15 Remote control of aircraft engines by combined hydraulic and electrical devices Expired FR886790A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE886790X 1941-10-28

Publications (1)

Publication Number Publication Date
FR886790A true FR886790A (en) 1943-10-25

Family

ID=6833502

Family Applications (1)

Application Number Title Priority Date Filing Date
FR886790D Expired FR886790A (en) 1941-10-28 1942-10-15 Remote control of aircraft engines by combined hydraulic and electrical devices

Country Status (1)

Country Link
FR (1) FR886790A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2199069A1 (en) * 1972-09-11 1974-04-05 Applied Power Inc

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2199069A1 (en) * 1972-09-11 1974-04-05 Applied Power Inc

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