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 aircraftInfo
- 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
Links
- 239000012530 fluid Substances 0.000 title 1
- 239000007788 liquid Substances 0.000 abstract 9
- 230000001105 regulatory effect Effects 0.000 abstract 3
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 230000000994 depressogenic effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/16—De-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.
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)
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. |
-
1937
- 1937-11-03 GB GB30072/37A patent/GB505094A/en not_active Expired
Cited By (2)
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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