GB567970A - Improvements in or relating to the prevention of ice formation on aircraft - Google Patents

Improvements in or relating to the prevention of ice formation on aircraft

Info

Publication number
GB567970A
GB567970A GB2179/42A GB217942A GB567970A GB 567970 A GB567970 A GB 567970A GB 2179/42 A GB2179/42 A GB 2179/42A GB 217942 A GB217942 A GB 217942A GB 567970 A GB567970 A GB 567970A
Authority
GB
United Kingdom
Prior art keywords
tube
porous
channel
metal
holes
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
GB2179/42A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB2179/42A priority Critical patent/GB567970A/en
Publication of GB567970A publication Critical patent/GB567970A/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)
  • Materials Applied To Surfaces To Minimize Adherence Of Mist Or Water (AREA)

Abstract

567,970. De-icing windows &c. JONES, W. D., HALBERT, J., RAWSON, R. R., and LENNOX, J. W. Feb. 18, 1942, Nos. 2179/42 and 861/43. [Class 29] [Also in Groups II, X, XXII, XXVIII and XXXIII] A tube for distributing de-icing liquid to aircraft wings and windows, the windscreens of cars, the look-out windows of locomotives, gun.- turrets, refrigerating apparatus, railway points and wireless aerials, has at least part of a wall or walls thereof, which is in communication with the interior of the tube, made of porous metal formed by sintering powdered metals. Fig. 2 shows a channel-shaped metal member 5 having its open side filled with a porous mass 4 formed by sintering powdered metal which in the process becomes bonded to the member 5. Fig. 4 shows a double-walled channel member having the inner channel filled with porous metal 4, holes 2 being formed in the base of the inner channel to lead liquid from a space 1. In another form, the porous block does not completely fill the channel, but leaves a space above the holes 2. In other forms, a separately formed porous strip is soldered or brazed to a square section tube having holes beneath the porous strip. Alternatively, the porous strip may be riveted to the tube with interposed packing. In another form, a channel member filled with porous metal with access holes in the base of the channel, is secured in a deeper channel member by screws with interposed rubber packing. Fig. 8 shows another form of tube. Various examples are given of the composition, grain size, and the duration and temperature of the sintering process for making the porous metal, copper, tin, nickel, aluminium, antimony and stainless steel powders being used, mixed in some cases with small quantities of salicylic acid or " Steratex " which volatilizes during the sintering. Alternatively, metallic oxides may be used, followed by reduction. The rest of the tube in the examples given is of the metal known under the Registered Trade Mark " Monel." As applied to aircraft, lengths of such tube are let into the parts to be protected, particularly the leading edges of the wings and tail planes, and supplied with deicing liquid under pressure from a pump as required. Ethylene glycol, glycerine or sugar solution may be used. For preventing the frosting of refrigerator parts, such tubes are disposed immediately over the parts to be treated so that the liquid spreads over such parts.
GB2179/42A 1942-02-18 1942-02-18 Improvements in or relating to the prevention of ice formation on aircraft Expired GB567970A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2179/42A GB567970A (en) 1942-02-18 1942-02-18 Improvements in or relating to the prevention of ice formation on aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2179/42A GB567970A (en) 1942-02-18 1942-02-18 Improvements in or relating to the prevention of ice formation on aircraft

Publications (1)

Publication Number Publication Date
GB567970A true GB567970A (en) 1945-03-12

Family

ID=9734965

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2179/42A Expired GB567970A (en) 1942-02-18 1942-02-18 Improvements in or relating to the prevention of ice formation on aircraft

Country Status (1)

Country Link
GB (1) GB567970A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2528384A1 (en) * 1982-06-09 1983-12-16 Snecma DEVICE FOR DETECTING AND PREVENTING ICE FORMATION ON PROFILE SURFACES

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2528384A1 (en) * 1982-06-09 1983-12-16 Snecma DEVICE FOR DETECTING AND PREVENTING ICE FORMATION ON PROFILE SURFACES
EP0098182A1 (en) * 1982-06-09 1984-01-11 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Device for sensing and preventing ice accretion on stream-lined surfaces
US4508295A (en) * 1982-06-09 1985-04-02 S.N.E.C.M.A. Device for detecting and preventing the formation of ice on contoured surfaces

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