GB505094A - Method of and means for distributing fluid to prevent the accretion of ice on the wings and other exposed parts or surfaces of aircraft - Google Patents

Method of and means for distributing fluid to prevent the accretion of ice on the wings and other exposed parts or surfaces of aircraft

Info

Publication number
GB505094A
GB505094A GB30072/37A GB3007237A GB505094A GB 505094 A GB505094 A GB 505094A GB 30072/37 A GB30072/37 A GB 30072/37A GB 3007237 A GB3007237 A GB 3007237A GB 505094 A GB505094 A GB 505094A
Authority
GB
United Kingdom
Prior art keywords
liquid
unit
chamber
valve
spring
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
GB30072/37A
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.)
Dunlop Rubber Co Ltd
Original Assignee
Dunlop Rubber Co 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 Dunlop Rubber Co Ltd filed Critical Dunlop Rubber Co Ltd
Priority to GB30072/37A priority Critical patent/GB505094A/en
Publication of GB505094A publication Critical patent/GB505094A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/16De-icing or preventing icing on exterior surfaces of aircraft by mechanical means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Loading And Unloading Of Fuel Tanks Or Ships (AREA)
  • Devices For Dispensing Beverages (AREA)

Abstract

505,094. Means for preventing the formation of ice on aircraft surfaces. DUNLOP RUBBER CO., Ltd., WRIGHT, J., and TREVASKIS, H. Nov. 3, 1937, No. 30072. [Class 4] In means for distributing liquid to prevent ice-accretion on the wings and other exposed parts of aircraft, liquid is fed under pressure to a device or a number of devices incorporating a valve for regulating the amount of liquid flowing to a particular part, and means are provided by which the regulated flow may be byepassed and an unrestricted or flooding flow delivered to the part or simultaneously to a plurality of parts. As shown in Fig. 1, liquid stored in containers 1, la is fed under pressure, by means of air from an air bottle supplied to the container 1 through n control valve and pipe 3, to a flooding unit 6, provided with a gauge 7 indicating the pressure in the whole system, and a plurality of regulating devices 8, connected to pipes f<1> leading to the parts to be treated and provided with flow-registering gauges. A trap valve 5 is provided to prevent air entering the system if the liquid is exhausted. The regulators 8 and unit 6 are secured together by bolts 45 provided with conduits 46, sealed at both ends and communicating with passages in the regulators and unit by diametrical holes and circumferential recesses provided at intervals along the bolts. During normal working, liquid fed to the unit 6, Fig. 2, flows along the c,onduit in the lower bolt, the part 46a of which communicates with the gauge 7 through a passage 13, and enters a chamber 16 in each regulator, Figs: 4 and 5, through passages 14, 15 controlled by a manually adjustable needle valve 17, the liquid then flows from the base of the chamber 16 and through a hole in a spring-pressed plunger 20, connected to a flexible diaphragm 22 and the " movement " 18 of the registering gauge, to a union 29 connected to one of the pipes f<1>. To flood the various parts simultaneously, a lever 35, Fig. 2, is depressed to raise a plunger 34 against the action of a torsion spring 39 and lift a spring- pressed ball 31. Liquid can then flow through the passage 13, a chamber 30 and passages 41, 42 to the part 46b of the conduit in the upper bolt and enter the chamber 16, Fig. 5, through a passage 43 controlled by a spring-loaded valve 44. According to the Provisional Specification the liquid may be fed to the unit 6 by a hand pump supplying a pressure accumulator.
GB30072/37A 1937-11-03 1937-11-03 Method of and means for distributing fluid to prevent the accretion of ice on the wings and other exposed parts or surfaces of aircraft Expired GB505094A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB30072/37A GB505094A (en) 1937-11-03 1937-11-03 Method of and means for distributing fluid to prevent the accretion of ice on the wings and other exposed parts or surfaces of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB30072/37A GB505094A (en) 1937-11-03 1937-11-03 Method of and means for distributing fluid to prevent the accretion of ice on the wings and other exposed parts or surfaces of aircraft

Publications (1)

Publication Number Publication Date
GB505094A true GB505094A (en) 1939-05-03

Family

ID=10301822

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30072/37A Expired GB505094A (en) 1937-11-03 1937-11-03 Method of and means for distributing fluid to prevent the accretion of ice on the wings and other exposed parts or surfaces of aircraft

Country Status (1)

Country Link
GB (1) GB505094A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422746A (en) * 1941-09-13 1947-06-24 Patterson Ind Inc Airplane wing deicer
US2435003A (en) * 1943-12-06 1948-01-27 Cook Electric Co System of deicing for aircraft, vessels, etc.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422746A (en) * 1941-09-13 1947-06-24 Patterson Ind Inc Airplane wing deicer
US2435003A (en) * 1943-12-06 1948-01-27 Cook Electric Co System of deicing for aircraft, vessels, etc.

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