US2431885A - Prevention or inhibiting of ice accumulations - Google Patents

Prevention or inhibiting of ice accumulations Download PDF

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Publication number
US2431885A
US2431885A US535202A US53520244A US2431885A US 2431885 A US2431885 A US 2431885A US 535202 A US535202 A US 535202A US 53520244 A US53520244 A US 53520244A US 2431885 A US2431885 A US 2431885A
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compound
glycerine
prevention
inhibiting
coating
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US535202A
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Walter E Palmer
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    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K3/00Materials not provided for elsewhere
    • C09K3/18Materials not provided for elsewhere for application to surfaces to minimize adherence of ice, mist or water thereto; Thawing or antifreeze materials for application to surfaces
    • C09K3/185Thawing materials

Definitions

  • This invention relates to the treatment .of 'surifacestexposed to moisture under freezing conditions and to the prevention .of the accumulation of ice or frost on such surfaces.
  • the surfaces treated may the the windshield of a vehicle such as an automobile, the windows of buildings, vehicles or other structures, the propeller blades of an aircraft or of various other types.
  • compositions have been pro-posed for this purpose, but none with which I am familiar are entirely satisfactory. Some are water-soluble so that they have short life and areoften washed off before the need for de-icing or preventing of ice formation occurs.
  • compositions are translucent rather than transparent and interfere with free vision through the protected glass.
  • To continuously supply a compound to the surface to be protected is wasteful, and uniform distribution is difficult, if not impossible, on a surface which is moving at high speed with a resulting rapid air flow over the surface.
  • Some compounds that have been proposed to lower or depress the freezing point of water contacting therewith are corrosive to metal or the surface coating of the part to be protected.
  • a compound composed of a polyhydric alcohol and a polycarboxylic acid may be formed, which serves admirably for antiicin purposes. It is well known that glycerine, in certain proportions, may be reacted with phthalic anhydride or other polycarboxylic acid to form a hard insoluble resin, but such a resin cannot be readily applied to a surface to be protected, and has little or no anti-icing action. In making my anti-icing compound, the glycerine and phthalic anhydride are reacted under conditions and in such proportions that a somewhat sticky compound is formed in which there are free hydroxyl groups and which has a limited amount of free glycerine.
  • phthalic anhydride and glycerine are mixed in substantially equal molecular proportions and are slowly heated up to about 240 C. in about forty-five minutes to one hour with stirring and until limited gelling occurs. Then an additional amount of glycerine, which is preferably substantially equal to the original amount, is added, and the temperature is brought up to me-Email 231301112 200 and the heatingcontinued with stirring until a test shows that the desired end point has been reached. l liis may beeascertained by placin a :drop iof the compound on .a clean metal surface.
  • the heat is shut off but stirring is continued and the compound allowed to cool to about C., at which point ethyl alcohol or other suitable volatile thinner is added and the stirring continued to effect a uniform dispersion.
  • the amount of thinner added is usually about 40 to 45% by weight of the compound, but should be such that the compound may be readily sprayed or brushed on the surface to be protected from icing. If the compound is applied to the surface in a heated condition, very little, if any, thinner is needed.
  • the temperature of cooking may vary between about 200 C. and 280 C. and the time of cooking may be correspondingly varied. At 200 C. the reaction is slow and requires considerable time, and at 280 C. it is very rapid. A temperature about half way between those extremes is the preferred one. The heating after the additional glycerine is put in, should not be substantially above 200 C. nor for a very long time.
  • I m not prepared to state the definite chemical composition of the compound but it is believed to be mainly a compound of phthalic anhydride and glycerine in the ratio of about 1 mol of the former to 2 mols of the latter, and thus each glycerine radical contains two free or unesterified hydroxyl groups.
  • each glycerine radical contains two free or unesterified hydroxyl groups.
  • the proportions of the polyhydric alcohol and the polycarboxylic acid may be varied and the amount of reaction may be controlled by varying the time and temperature of cooking. It is important that the compound be soluble in a readily volatile thinner or liquid and that after the evaporation of the thinner, the coating be somewhat sticky.
  • the coating acts to depressthe freezing point of water which may contact with the treated surface, as for instance, in the form of rain, fog, mist or snow flakes, and the water having its freezing point depressed or lowered,'drains off or is thrown off if the treated surface be that of an airplane propeller, or is blown off if the surface be some other exposed part of an aircraft.
  • the free glycerine is retained in the coating for a considerable length of time under service conditions, but gradually becomes dissipated or leached out, and then a fresh coating may be applied directly upon the originalcoating or after Washing the latter off by the use of a suitable solvent.
  • the coating contain only a relatively small amount of free glycerine, a very much larger amount of glycerine may be added in preparing the compound and thus a, larger amount will be present in the coating.
  • the amount should not be so large as will permit draining of the glycerine away from the coating or the formation of a coating with is sufiiciently pre-fiowing to drain ofi the surface.

Description

Patented Dec. 2, 1947 UNITED PREVENTION OR INHIBITIING OF "ICE ACCUMULATIONS 'Walter E. Palmer, Eair :Lawmfl.
No Drawing. Application May. 1*1, 1j944, Serial No. 535,202
1 Claim. 1
This invention relates to the treatment .of 'surifacestexposed to moisture under freezing conditions and to the prevention .of the accumulation of ice or frost on such surfaces. The surfaces treated :may the the windshield of a vehicle such as an automobile, the windows of buildings, vehicles or other structures, the propeller blades of an aircraft or of various other types.
Formation of ice on propeller blades is particularly dangerous, as pieces of ice breaking off are projected at high speed like missiles, and leave the propeller out of balance. Ice formations on windows, Windshields, etc., destroy or reduce visibility therethrough.
Many compositions have been pro-posed for this purpose, but none with which I am familiar are entirely satisfactory. Some are water-soluble so that they have short life and areoften washed off before the need for de-icing or preventing of ice formation occurs.
Other compositions are translucent rather than transparent and interfere with free vision through the protected glass. To continuously supply a compound to the surface to be protected is wasteful, and uniform distribution is difficult, if not impossible, on a surface which is moving at high speed with a resulting rapid air flow over the surface. Some compounds that have been proposed to lower or depress the freezing point of water contacting therewith are corrosive to metal or the surface coating of the part to be protected.
I have discovered that a compound composed of a polyhydric alcohol and a polycarboxylic acid may be formed, which serves admirably for antiicin purposes. It is well known that glycerine, in certain proportions, may be reacted with phthalic anhydride or other polycarboxylic acid to form a hard insoluble resin, but such a resin cannot be readily applied to a surface to be protected, and has little or no anti-icing action. In making my anti-icing compound, the glycerine and phthalic anhydride are reacted under conditions and in such proportions that a somewhat sticky compound is formed in which there are free hydroxyl groups and which has a limited amount of free glycerine.
As a preferred procedure for making the coating composition, phthalic anhydride and glycerine are mixed in substantially equal molecular proportions and are slowly heated up to about 240 C. in about forty-five minutes to one hour with stirring and until limited gelling occurs. Then an additional amount of glycerine, which is preferably substantially equal to the original amount, is added, and the temperature is brought up to me-Email 231301112 200 and the heatingcontinued with stirring until a test shows that the desired end point has been reached. l liis may beeascertained by placin a :drop iof the compound on .a clean metal surface. The drop should be somewhat :c'loudy "but =not opaque, and sulfic'iently plastic so that-it can be smeared out with :the finger and without showing long stringy adherence to the finger from the metal plate. It should not be hard or brittle on becoming cold and should remain soft and sticky. When this end point is reached, the heat is shut off but stirring is continued and the compound allowed to cool to about C., at which point ethyl alcohol or other suitable volatile thinner is added and the stirring continued to effect a uniform dispersion. The amount of thinner added is usually about 40 to 45% by weight of the compound, but should be such that the compound may be readily sprayed or brushed on the surface to be protected from icing. If the compound is applied to the surface in a heated condition, very little, if any, thinner is needed.
The temperature of cooking may vary between about 200 C. and 280 C. and the time of cooking may be correspondingly varied. At 200 C. the reaction is slow and requires considerable time, and at 280 C. it is very rapid. A temperature about half way between those extremes is the preferred one. The heating after the additional glycerine is put in, should not be substantially above 200 C. nor for a very long time.
I m not prepared to state the definite chemical composition of the compound but it is believed to be mainly a compound of phthalic anhydride and glycerine in the ratio of about 1 mol of the former to 2 mols of the latter, and thus each glycerine radical contains two free or unesterified hydroxyl groups. There should be a small amount of free glycerine uniformly dispersed throughout the compound, but due to such dispersion, it can be leached out by water only at a very low rate. The proportions of the polyhydric alcohol and the polycarboxylic acid may be varied and the amount of reaction may be controlled by varying the time and temperature of cooking. It is important that the compound be soluble in a readily volatile thinner or liquid and that after the evaporation of the thinner, the coating be somewhat sticky.
The coating acts to depressthe freezing point of water which may contact with the treated surface, as for instance, in the form of rain, fog, mist or snow flakes, and the water having its freezing point depressed or lowered,'drains off or is thrown off if the treated surface be that of an airplane propeller, or is blown off if the surface be some other exposed part of an aircraft. The free glycerine is retained in the coating for a considerable length of time under service conditions, but gradually becomes dissipated or leached out, and then a fresh coating may be applied directly upon the originalcoating or after Washing the latter off by the use of a suitable solvent.
Although it is preferred that the coating contain only a relatively small amount of free glycerine, a very much larger amount of glycerine may be added in preparing the compound and thus a, larger amount will be present in the coating. The amount should not be so large as will permit draining of the glycerine away from the coating or the formation of a coating with is sufiiciently pre-fiowing to drain ofi the surface. In-
stead of using a single polyhydric alcohol such as the solvent.
WALTER E. PALMER.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,341,735 Monsaroff Feb. 15, 1944 2,346,891 Adlington Apr. 18, 1944 FOREIGN PATENTS Number Country Date 337,199 Great Britain Oct. 30, 1930 OTHER REFERENCES Ellis, The Chemistry of Synthetic Resins, vol.
II, 1935, pages 864 to 869.
US535202A 1944-05-11 1944-05-11 Prevention or inhibiting of ice accumulations Expired - Lifetime US2431885A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2918052A (en) * 1957-03-14 1959-12-22 Armour Res Found Heat-releasing anti-icing means
US3157117A (en) * 1957-10-31 1964-11-17 Dick Co Ab Lithographic plates and method for manufacture

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB337199A (en) * 1929-10-31 1930-10-30 Ig Farbenindustrie Ag Improvements in printing inks
US2341735A (en) * 1942-07-13 1944-02-15 Cosmos Imp Mills Ltd Method and composition for treating yarns and fabrics
US2346891A (en) * 1940-12-20 1944-04-18 Adlington George Stuart Prevention of ice accretion

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB337199A (en) * 1929-10-31 1930-10-30 Ig Farbenindustrie Ag Improvements in printing inks
US2346891A (en) * 1940-12-20 1944-04-18 Adlington George Stuart Prevention of ice accretion
US2341735A (en) * 1942-07-13 1944-02-15 Cosmos Imp Mills Ltd Method and composition for treating yarns and fabrics

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2918052A (en) * 1957-03-14 1959-12-22 Armour Res Found Heat-releasing anti-icing means
US3157117A (en) * 1957-10-31 1964-11-17 Dick Co Ab Lithographic plates and method for manufacture

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