GB565463A - Improvements in aircraft fluid pressure remote control systems - Google Patents

Improvements in aircraft fluid pressure remote control systems

Info

Publication number
GB565463A
GB565463A GB10839/41A GB1083941A GB565463A GB 565463 A GB565463 A GB 565463A GB 10839/41 A GB10839/41 A GB 10839/41A GB 1083941 A GB1083941 A GB 1083941A GB 565463 A GB565463 A GB 565463A
Authority
GB
United Kingdom
Prior art keywords
pump
injector
reservoir
control systems
pipe
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
GB10839/41A
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.)
Dowty Equipment Ltd
Original Assignee
Dowty Equipment Ltd
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 Dowty Equipment Ltd filed Critical Dowty Equipment Ltd
Priority to GB10839/41A priority Critical patent/GB565463A/en
Publication of GB565463A publication Critical patent/GB565463A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/22Operating mechanisms fluid

Abstract

565,463. Hydraulic control systems. DOWTY EQUIPMENT, Ltd., and BURKE, P. W. Aug. 25, 1941, No. 10839. [Class 69 (ii)] [Also in Group XXVIII] To ensure correct action without cavitation of a liquid supply system for operating hydraulic motors on aircraft an injector device is arranged between the reservoir 11 of the fluid supply system and the pump 3 which is preferably of the kind described in Specifications 534,847, 524,384, 524,199, [all in Group XXVIII]. As applied to a power system such as described in Specification 531,465 in which jacks 17 are operated from the pump 3 under the control of a valve 16, the outlet pipe 15 of the pump 3 is connected to the injector nozzle 21, which draws fluid from a pipe 10 connected to the reservoir 11 and delivers it to the inlet 4 of the pump 3. The injector thus acts as a booster. The pump is provided with a centrifuge return outlet 14 connected by a pipe 23 to the reservoir which acts to cool the pump. The circuit may include an additional injector 24 which supplies a low pressure hydraulic motor 25 under control of a, valve 26.
GB10839/41A 1941-08-25 1941-08-25 Improvements in aircraft fluid pressure remote control systems Expired GB565463A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB10839/41A GB565463A (en) 1941-08-25 1941-08-25 Improvements in aircraft fluid pressure remote control systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10839/41A GB565463A (en) 1941-08-25 1941-08-25 Improvements in aircraft fluid pressure remote control systems

Publications (1)

Publication Number Publication Date
GB565463A true GB565463A (en) 1944-11-13

Family

ID=9975271

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10839/41A Expired GB565463A (en) 1941-08-25 1941-08-25 Improvements in aircraft fluid pressure remote control systems

Country Status (1)

Country Link
GB (1) GB565463A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2181494A (en) * 1985-10-03 1987-04-23 Draegerwerk Ag Piston dosing pump for a fluid

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2181494A (en) * 1985-10-03 1987-04-23 Draegerwerk Ag Piston dosing pump for a fluid

Similar Documents

Publication Publication Date Title
GB1027973A (en) Plural output pump
GB565463A (en) Improvements in aircraft fluid pressure remote control systems
US2452874A (en) Pumping system
US2315656A (en) Dual pressure pumping system
GB531465A (en) Improvements relating to hydraulic actuating systems, for aircraft and the like
GB1148179A (en) Pumping system for a nuclear reactor
GB1005455A (en) Flow dividing valve means
GB580604A (en) Improvements in or relating to liquid circulating systems
GB879586A (en) Fuel supply systems for aircraft
GB628639A (en) Improvements in or relating to hydraulic systems
GB1072378A (en) Improvements in or relating to hydraulically actuated flexible chamber pumps
GB1059304A (en) Improvements in or relating to lubricating systems
US2361934A (en) Servo mechanism of the hydraulic type
GB551119A (en) Improvements in or relating to fluid pressure supply systems
GB573362A (en) Improvements in or relating to hydraulic systems
GB1334769A (en) Device for the control of a high pressure pump
GB914077A (en) Centrifugal boost pumps for aircraft fuel systems
GB569300A (en) Improvements in or relating to liquid pressure remote control systems
GB565834A (en) Improvements in or relating to hydraulic control systems
GB534054A (en) Improvements in or relating to power transmission systems
GB956921A (en) Oil-burner supply systems
GB1108232A (en) Improvements in or relating to hydraulic control circuits
GB592200A (en) Improvements in hydraulic pump and motor systems
GB1205981A (en) Improvements in two stage reciprocating pump systems
GB617639A (en) Improvements in liquid pumps and liquid supply systems