CA1110607A - Pneumatic deicer - Google Patents
Pneumatic deicerInfo
- Publication number
- CA1110607A CA1110607A CA320,038A CA320038A CA1110607A CA 1110607 A CA1110607 A CA 1110607A CA 320038 A CA320038 A CA 320038A CA 1110607 A CA1110607 A CA 1110607A
- Authority
- CA
- Canada
- Prior art keywords
- ply
- tubular members
- deicer
- manifold
- boot
- 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
- 150000001875 compounds Chemical class 0.000 claims abstract description 14
- 238000000034 method Methods 0.000 claims abstract description 10
- 238000004073 vulcanization Methods 0.000 claims abstract description 8
- 239000004744 fabric Substances 0.000 claims description 28
- 239000000463 material Substances 0.000 claims description 22
- 238000004519 manufacturing process Methods 0.000 claims description 11
- 229920001971 elastomer Polymers 0.000 claims description 7
- 230000002093 peripheral effect Effects 0.000 claims description 7
- 244000043261 Hevea brasiliensis Species 0.000 claims description 6
- 239000004677 Nylon Substances 0.000 claims description 6
- 229920003052 natural elastomer Polymers 0.000 claims description 6
- 229920001194 natural rubber Polymers 0.000 claims description 6
- 229920001778 nylon Polymers 0.000 claims description 6
- 238000007789 sealing Methods 0.000 claims description 5
- 230000015572 biosynthetic process Effects 0.000 claims description 2
- 239000002759 woven fabric Substances 0.000 claims description 2
- 239000013536 elastomeric material Substances 0.000 claims 2
- 238000009825 accumulation Methods 0.000 abstract description 2
- LNUFLCYMSVYYNW-ZPJMAFJPSA-N [(2r,3r,4s,5r,6r)-2-[(2r,3r,4s,5r,6r)-6-[(2r,3r,4s,5r,6r)-6-[(2r,3r,4s,5r,6r)-6-[[(3s,5s,8r,9s,10s,13r,14s,17r)-10,13-dimethyl-17-[(2r)-6-methylheptan-2-yl]-2,3,4,5,6,7,8,9,11,12,14,15,16,17-tetradecahydro-1h-cyclopenta[a]phenanthren-3-yl]oxy]-4,5-disulfo Chemical compound O([C@@H]1[C@@H](COS(O)(=O)=O)O[C@@H]([C@@H]([C@H]1OS(O)(=O)=O)OS(O)(=O)=O)O[C@@H]1[C@@H](COS(O)(=O)=O)O[C@@H]([C@@H]([C@H]1OS(O)(=O)=O)OS(O)(=O)=O)O[C@@H]1[C@@H](COS(O)(=O)=O)O[C@H]([C@@H]([C@H]1OS(O)(=O)=O)OS(O)(=O)=O)O[C@@H]1C[C@@H]2CC[C@H]3[C@@H]4CC[C@@H]([C@]4(CC[C@@H]3[C@@]2(C)CC1)C)[C@H](C)CCCC(C)C)[C@H]1O[C@H](COS(O)(=O)=O)[C@@H](OS(O)(=O)=O)[C@H](OS(O)(=O)=O)[C@H]1OS(O)(=O)=O LNUFLCYMSVYYNW-ZPJMAFJPSA-N 0.000 description 5
- 238000012986 modification Methods 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 230000002411 adverse Effects 0.000 description 2
- 230000000740 bleeding effect Effects 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 239000011888 foil Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 239000000806 elastomer Substances 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 229920001084 poly(chloroprene) Polymers 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 239000012858 resilient material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000011800 void material Substances 0.000 description 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
- B64D15/166—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means using pneumatic boots
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Heating, Cooling, Or Curing Plastics Or The Like In General (AREA)
- Defrosting Systems (AREA)
Abstract
PNEUMATIC DEICER
ABSTRACT OF THE DISCLOSURE
A pneumatic deicer and a method for making such deicer having a plurality of inflatable tubes which are capable of being distended by inflation to break up the accumulation of ice. The tubes are constructed with a nonflowing elastomeric compound leaving a passageway therein after vulcanization of the deicer by external heat.
ABSTRACT OF THE DISCLOSURE
A pneumatic deicer and a method for making such deicer having a plurality of inflatable tubes which are capable of being distended by inflation to break up the accumulation of ice. The tubes are constructed with a nonflowing elastomeric compound leaving a passageway therein after vulcanization of the deicer by external heat.
Description
~1106~)7 This invention relates to pneumatic deicers and more particularly to a pneumatic deicer and the method of making a pneumatic deicer of the type employing a boot of resilient material attached to the leading edge of an airfoil wherein the boot has a plurality of inflatable tubes which are selectively distended as by inflation pressure to break up ice accumulation which tends to form on the surface of the boot. The inflatable tubes are generally disposed in a direction parallel to each other in the spanwise direction of the leading edge of the airfoil. The tubes, however, may be disposed to extend in the direction of the airfoil or in any other angular position. The deicer is vulcanized by steam which also I5 passes through the inflation tubes assuring that the tubular passageway remains open so that the inner peripheral surfaces of such passageway do not adhere to each other. The inflation of the tube is performed through a manifold that extends transversely of and over-lies the tubes. In the manufacture of the boot assemblies,various modifications in tube construction have been tried to facilitate the inflating and evacuation process of the tubes since it is desirable to so construct the boot assembly to provide an unencumbered flow of air to and from the tubes. To insure such flow additional materials r such as flocked liners or fabrics, have been integrated into the tube structure; however;j such finally constructed boots would present ripples and objectionable thickness thereby rendering such boot objectionable for aesthetic reasons as well as for aerodynamic reasons.
The present invention provides a simple structure and method of constructing a deicer to provide for the adequate bleeding of the inflation tubes during the deflation cycle, eliminating the need for building in additional separating devices that add to the manufacturing ,~
~ 7 11~06Q7 cost and adversely affect aerodynamic conditions of the airfoils. The present invention substantially eliminates the causes of erosion of the skin of the deicers and mate-rially improves the aerodynamics of the air foils by keep-ing the airfoils smooth externally.
The pneumatic deicer and method of the present invention provides a boot which is smooth and of uniform thickness, wherein the inflating tubes are formed using fabric coated with a nonflowing rubberized compound on the one side thereby leaving the fabric with uncoated portion on the other side in cooperation with the non-flowing com-pound on the inside of the tube, allowing the bleeding off of the inflation air directly to the manifold or via a channel and the manifold. The cross communication of the tubes with the manifold is maintained easily and in an economic manner.
The non-flowing rubberized compound is more parti-cularly an elastomer which is an in-cure, nonflowing rubberized compound.
Thus in accordance with one aspect of the invention there is provided an inflatable deicer boot for mounting on an air foil comprising a series of tubular members selectively inflated and deflated for breaking up the formation of ice on said airfoil; a manifold ply of rubberized material extending transversely across said series of tubular memhers; the mani-fold ply having a passageway therethrough for the flow of air to pressurize or exhaust air from said tubular members;
each of the tubular members having a port communicating with the passageway in the manifold ply; each of the tubular members hac an inner peripheral surface of fabric, each tubular member being covered with in-cure, nonflowing rubberized compound; a layer of a vulcanizable material impervious to air overlaying the manifold ply and the tubular members and at least another layer of a vulcanizable mate-rial impervious to air underlaying the tubular members.
In particular overlaying and underlaying layers are sealing layers, the various layers and the nonflowing rubberized compound being vulcanized to form a unitary integral deicer boot.
C
.
.
, . ' ,.
- -11~06~7 `` ` In another aspect of the invention there is pro-vided a method of fabricating a deicer boot of the invention which comprises the steps of disposing a plurality of the tubular members in a laterally spaced relationship on the under layer of vulcanizable material, laying the manifold ply across the tubular members so that the passageway in the manifold ply communicates with the ports in the tubular members, laying overlayer of vul-canizable material over the tubular members, forming a vacuum on the manifold and vulcanizing the assembly into a unitary structure.
The invention is illustrated in a particular and preferred embodiment by reference to the accompanying drawings in which:
Fig. 1 is a plan view of the deicer boot with the inflation tubes being shown in dotted lines, Fig. 2 is an enlarged section of the deicer boot taken along line 2-2 of Fig. 1 with a portion broken away;
Fig. 3 is an enlarged section of the deicer boot taken along line 3-3 of Fig. 1 with a portion broken away.
With further reference to the drawings wherein like reference numerals designate like or corresponding parts throughout the several views, there is shown in Fig. 1 a laminated inflatable deicer boot 10 in the condition prior to installation on an airfoil with the leading edge of the airfoil to be covered by the leading edge portion of the boot indicated by the dot-dash line L-L. Trailing edges 11 : ~.
111~6~7 and 12 of the boot extend toward the rear of the airfoil on the upper and under side thereof. The bottom ply 15 which may be fabric coated with rubber or other resilient rubber-like material extends over a series of longitudinal tubular members or inflation tubes 16 as shown in dotted lines in Fig. 1.
The inflation tubes 16 are made of a nylon or other similar fabric 17 which has a nonflowing, during curing, rubberized compound 18 containing cross-linked natural rubber greater than 1% by weight on one side and with the other side (inward side) being uncoated due to the non-flowing nature of such compound 18 to provide an inner tubular surface that has fabric and an outer tubular surface coated with the nonflowing compound 18. The fabric 17 of the inflation tubes 16 is tricot knit fabric or woven fabric coated with the rubberized compound 18 in such a manner that the tubes 16 may expand during inflation but are not exten-sible in the longitudinal direction. A top ply 20 of resi-lient rubber or rubberlike materials is disposed on top of the inflation tubes 16. A sheet of resilient rubberlike material 21 such as neoprene covers the top ply 20. Side fill gum 23 is positioned adjacent to the outermost tube 16 between top ply 20 and the bottom ply 15. Fill gum 23A is interposed between the respective tubes 16 and the bottom ply 15 and top ply 20. A variation of such invention contemplates the elimination of the fill gum 23A.
As shown in Fig. 3, extending traversely across the inflation tubes 16 of the deicer boot 10 is a manifold ply 25 having a plurality of closely spaced elements such as stiff fibers 26 projecting outwardly and downwardly from the fabric to provide interstices and a passageway 40 through which the inflating medium can flow. The re~pective tubes 16 all have channels 28 (Fig. 2) on their back side of the boot lo that run the full length of the tube and communicate with the space provided by C
" .
. .
` ` 111(96!~7 the interstices of the fibers 26 of manifold ply 25 to provide for the inflation and deflation of the tubes 16.
In lieu of such channels 28, a single port may be located directly in the tubes 16 at the juncture with manifold ply 25 to exhaust the pressurized air from the tubes 16 to the manifold. The interstices 26 of the manifold ply 25 communicate with a central bore 29 on frustoconical annular supporting member or air connecting means 30 which is made of resilient rubber or other rubberlike materials which may contain a hollow body of steel or other suitable material for the supply of inflating medium from the aircraft supply. Gum plies 32, 33, and reinforcing fabric material 34 encompass the supporting member 30 which supporting member 30 is cemented to the bottom-ply 15.
The above described plies of resilient rubberized materials are impervious to the inflating medium.
Manifold ply 25 may have a central passageway therethrough that communicates with the respective ports or channels 2 in the tubular members 16.
In the manufacture of the deicer boot 10 described above, the various plies, parts, and tubes are assembled and cemented together with tube 16 being compounded to include cross-linked natural rubber greater than 1% by weight, which cross-linked rubber prevents flow during cure. Ordinarily the deicer is cured by steam, having the steam enter the respective tubes during the actual cure to maintain the tubes 16 in a distended condition to prevent adhesion of the inner sur~aces. In curing the deicer pad by this method, the steam can penetrate voids or pockets of material that were not properly sealed or cemented and adversely affect the quality of the end product. In the instant invention the deicer pad in its assembled condition without the air connecting means 30 is covered by a bleeder material such as heavy-duty paper. The paper and deicer are then ~J
, ,,: . -.
10~i~7 covered with a suitable cover ply that overlaps both to assure a positive seal around the edges. The cover ply has a small bore in it such that all air can be withdrawn from under the cover. In this instance a vacuum is drawn on the bore to evacuate the air from underneath the cover, with the paper acting as a wick to facilitate the removal of the air. The assembled deicer boot and cover are then subjected to vulcanization heat and vulcanized to provide a unitary structure with the nonflowing rubberized compound 18 assuring that the inner peripheral wall surface of the tubes 16 which have fabric therein retain their form and upon receiving pressurized air will inflate.
Upon completion of vulcanization, the cover and paper are removed and a port or bore is cut into the deicer pad to communicate with the central passageway in the manifold 40.
The air connecting means 30 is then cemented onto the deicer pad and vulcanized so that the central bore 29 thereof communicates directly with the cut port to the manifold 40.
A modification of the above process is to place a thin mesh nylon fabric onto the bottom ply 15 of the unvulcanized assembled deicer pad (containing the top ply 20, sheet material 21, tubes 16, manifold ply 25, and bottom ply 15) and then cover such pad with a bleeder pad such as a layer of porous paper. The deicer pad, nylon fabric, and paper are then covered completely with a suitable cover that overlaps all edges of the deicer pad and paper. In this condition the parts as assembled are flat and void of air. However, to assure a complete absence of air, the cover is pierced to provide a port or bore and suitable means are connected to this pierced hole to withdraw all air from the deicer assembly, afterwhich the pierced hole is immediately covered and sealed. The entire deicer assembly and cover are then vulcanized.
Thereafter, the cover, paper, and nylon fabric are removed.
C
.
~ ', ,' ,' :
.. .. .
- ' ' ' -'.............. ,..... . .- : ~ ' .. ~
lllQ~i~7 The nylon fabric gives the bottom surface of the deicer pad a textured fabric finish thus acting as an impression cover or an impression fabric finish cover. The paper facilitates the removal of air and acts as a wick means for the removal of trapped air. The vulcanized deicer pad then has a hole cut into its bottom ply 15 on the manifold section 40 so as to communicate therewith. An air connecting means or valve 30 is then secured and vulcanized to the bottom ply 15 to have its bore 29 register with the hole cut in the ply 15. A further modification is to omit evacuation of the air from under-neath the cover prior to vulcanization since careful assemblying will substantially eliminate trapping of air;
and since no steam is introduced into the tubes 16 themselves, the subsequent vulcanization process provides a more economical means for manufacturing quality deicers.
The present invention also provides a flat, nonripple surface. When pressurized air is communicated to tubes 16 during deicing process, all tubes will be in full communication with the central passageway in the manifold 'ply 40 which in turn communicates with the central bore 29 of the air connecting means 30. Such deicer boot may be mounted on any airfoil of an aircraft in a manner old and well-known in the art.
It will be apparent that, although a specific emhodiment and certain modifications of the invention have been described in detail, the invention is not limited to the specifically illustrated and described constructions since variations may be made without departing from the principles of the invention.
-.: .
- ' ~ ,, .
The present invention provides a simple structure and method of constructing a deicer to provide for the adequate bleeding of the inflation tubes during the deflation cycle, eliminating the need for building in additional separating devices that add to the manufacturing ,~
~ 7 11~06Q7 cost and adversely affect aerodynamic conditions of the airfoils. The present invention substantially eliminates the causes of erosion of the skin of the deicers and mate-rially improves the aerodynamics of the air foils by keep-ing the airfoils smooth externally.
The pneumatic deicer and method of the present invention provides a boot which is smooth and of uniform thickness, wherein the inflating tubes are formed using fabric coated with a nonflowing rubberized compound on the one side thereby leaving the fabric with uncoated portion on the other side in cooperation with the non-flowing com-pound on the inside of the tube, allowing the bleeding off of the inflation air directly to the manifold or via a channel and the manifold. The cross communication of the tubes with the manifold is maintained easily and in an economic manner.
The non-flowing rubberized compound is more parti-cularly an elastomer which is an in-cure, nonflowing rubberized compound.
Thus in accordance with one aspect of the invention there is provided an inflatable deicer boot for mounting on an air foil comprising a series of tubular members selectively inflated and deflated for breaking up the formation of ice on said airfoil; a manifold ply of rubberized material extending transversely across said series of tubular memhers; the mani-fold ply having a passageway therethrough for the flow of air to pressurize or exhaust air from said tubular members;
each of the tubular members having a port communicating with the passageway in the manifold ply; each of the tubular members hac an inner peripheral surface of fabric, each tubular member being covered with in-cure, nonflowing rubberized compound; a layer of a vulcanizable material impervious to air overlaying the manifold ply and the tubular members and at least another layer of a vulcanizable mate-rial impervious to air underlaying the tubular members.
In particular overlaying and underlaying layers are sealing layers, the various layers and the nonflowing rubberized compound being vulcanized to form a unitary integral deicer boot.
C
.
.
, . ' ,.
- -11~06~7 `` ` In another aspect of the invention there is pro-vided a method of fabricating a deicer boot of the invention which comprises the steps of disposing a plurality of the tubular members in a laterally spaced relationship on the under layer of vulcanizable material, laying the manifold ply across the tubular members so that the passageway in the manifold ply communicates with the ports in the tubular members, laying overlayer of vul-canizable material over the tubular members, forming a vacuum on the manifold and vulcanizing the assembly into a unitary structure.
The invention is illustrated in a particular and preferred embodiment by reference to the accompanying drawings in which:
Fig. 1 is a plan view of the deicer boot with the inflation tubes being shown in dotted lines, Fig. 2 is an enlarged section of the deicer boot taken along line 2-2 of Fig. 1 with a portion broken away;
Fig. 3 is an enlarged section of the deicer boot taken along line 3-3 of Fig. 1 with a portion broken away.
With further reference to the drawings wherein like reference numerals designate like or corresponding parts throughout the several views, there is shown in Fig. 1 a laminated inflatable deicer boot 10 in the condition prior to installation on an airfoil with the leading edge of the airfoil to be covered by the leading edge portion of the boot indicated by the dot-dash line L-L. Trailing edges 11 : ~.
111~6~7 and 12 of the boot extend toward the rear of the airfoil on the upper and under side thereof. The bottom ply 15 which may be fabric coated with rubber or other resilient rubber-like material extends over a series of longitudinal tubular members or inflation tubes 16 as shown in dotted lines in Fig. 1.
The inflation tubes 16 are made of a nylon or other similar fabric 17 which has a nonflowing, during curing, rubberized compound 18 containing cross-linked natural rubber greater than 1% by weight on one side and with the other side (inward side) being uncoated due to the non-flowing nature of such compound 18 to provide an inner tubular surface that has fabric and an outer tubular surface coated with the nonflowing compound 18. The fabric 17 of the inflation tubes 16 is tricot knit fabric or woven fabric coated with the rubberized compound 18 in such a manner that the tubes 16 may expand during inflation but are not exten-sible in the longitudinal direction. A top ply 20 of resi-lient rubber or rubberlike materials is disposed on top of the inflation tubes 16. A sheet of resilient rubberlike material 21 such as neoprene covers the top ply 20. Side fill gum 23 is positioned adjacent to the outermost tube 16 between top ply 20 and the bottom ply 15. Fill gum 23A is interposed between the respective tubes 16 and the bottom ply 15 and top ply 20. A variation of such invention contemplates the elimination of the fill gum 23A.
As shown in Fig. 3, extending traversely across the inflation tubes 16 of the deicer boot 10 is a manifold ply 25 having a plurality of closely spaced elements such as stiff fibers 26 projecting outwardly and downwardly from the fabric to provide interstices and a passageway 40 through which the inflating medium can flow. The re~pective tubes 16 all have channels 28 (Fig. 2) on their back side of the boot lo that run the full length of the tube and communicate with the space provided by C
" .
. .
` ` 111(96!~7 the interstices of the fibers 26 of manifold ply 25 to provide for the inflation and deflation of the tubes 16.
In lieu of such channels 28, a single port may be located directly in the tubes 16 at the juncture with manifold ply 25 to exhaust the pressurized air from the tubes 16 to the manifold. The interstices 26 of the manifold ply 25 communicate with a central bore 29 on frustoconical annular supporting member or air connecting means 30 which is made of resilient rubber or other rubberlike materials which may contain a hollow body of steel or other suitable material for the supply of inflating medium from the aircraft supply. Gum plies 32, 33, and reinforcing fabric material 34 encompass the supporting member 30 which supporting member 30 is cemented to the bottom-ply 15.
The above described plies of resilient rubberized materials are impervious to the inflating medium.
Manifold ply 25 may have a central passageway therethrough that communicates with the respective ports or channels 2 in the tubular members 16.
In the manufacture of the deicer boot 10 described above, the various plies, parts, and tubes are assembled and cemented together with tube 16 being compounded to include cross-linked natural rubber greater than 1% by weight, which cross-linked rubber prevents flow during cure. Ordinarily the deicer is cured by steam, having the steam enter the respective tubes during the actual cure to maintain the tubes 16 in a distended condition to prevent adhesion of the inner sur~aces. In curing the deicer pad by this method, the steam can penetrate voids or pockets of material that were not properly sealed or cemented and adversely affect the quality of the end product. In the instant invention the deicer pad in its assembled condition without the air connecting means 30 is covered by a bleeder material such as heavy-duty paper. The paper and deicer are then ~J
, ,,: . -.
10~i~7 covered with a suitable cover ply that overlaps both to assure a positive seal around the edges. The cover ply has a small bore in it such that all air can be withdrawn from under the cover. In this instance a vacuum is drawn on the bore to evacuate the air from underneath the cover, with the paper acting as a wick to facilitate the removal of the air. The assembled deicer boot and cover are then subjected to vulcanization heat and vulcanized to provide a unitary structure with the nonflowing rubberized compound 18 assuring that the inner peripheral wall surface of the tubes 16 which have fabric therein retain their form and upon receiving pressurized air will inflate.
Upon completion of vulcanization, the cover and paper are removed and a port or bore is cut into the deicer pad to communicate with the central passageway in the manifold 40.
The air connecting means 30 is then cemented onto the deicer pad and vulcanized so that the central bore 29 thereof communicates directly with the cut port to the manifold 40.
A modification of the above process is to place a thin mesh nylon fabric onto the bottom ply 15 of the unvulcanized assembled deicer pad (containing the top ply 20, sheet material 21, tubes 16, manifold ply 25, and bottom ply 15) and then cover such pad with a bleeder pad such as a layer of porous paper. The deicer pad, nylon fabric, and paper are then covered completely with a suitable cover that overlaps all edges of the deicer pad and paper. In this condition the parts as assembled are flat and void of air. However, to assure a complete absence of air, the cover is pierced to provide a port or bore and suitable means are connected to this pierced hole to withdraw all air from the deicer assembly, afterwhich the pierced hole is immediately covered and sealed. The entire deicer assembly and cover are then vulcanized.
Thereafter, the cover, paper, and nylon fabric are removed.
C
.
~ ', ,' ,' :
.. .. .
- ' ' ' -'.............. ,..... . .- : ~ ' .. ~
lllQ~i~7 The nylon fabric gives the bottom surface of the deicer pad a textured fabric finish thus acting as an impression cover or an impression fabric finish cover. The paper facilitates the removal of air and acts as a wick means for the removal of trapped air. The vulcanized deicer pad then has a hole cut into its bottom ply 15 on the manifold section 40 so as to communicate therewith. An air connecting means or valve 30 is then secured and vulcanized to the bottom ply 15 to have its bore 29 register with the hole cut in the ply 15. A further modification is to omit evacuation of the air from under-neath the cover prior to vulcanization since careful assemblying will substantially eliminate trapping of air;
and since no steam is introduced into the tubes 16 themselves, the subsequent vulcanization process provides a more economical means for manufacturing quality deicers.
The present invention also provides a flat, nonripple surface. When pressurized air is communicated to tubes 16 during deicing process, all tubes will be in full communication with the central passageway in the manifold 'ply 40 which in turn communicates with the central bore 29 of the air connecting means 30. Such deicer boot may be mounted on any airfoil of an aircraft in a manner old and well-known in the art.
It will be apparent that, although a specific emhodiment and certain modifications of the invention have been described in detail, the invention is not limited to the specifically illustrated and described constructions since variations may be made without departing from the principles of the invention.
-.: .
- ' ~ ,, .
Claims (17)
1. An inflatable deicer boot for mounting on an airfoil comprising a series of tubular members selectively inflated and deflated for breaking up the formation of ice on said airfoil; a manifold ply of rubberized material extending transversely across said series of tubular members; said manifold ply having a passageway therethrough for the flow of air to pressurize or exhaust air from said tubular members; each of said tubular members having a port communicating with said passageway in said manifold ply; each of said tubular members having an inner peripheral surface of fabric;
each said tubular members being covered with in-cure, non-flowing rubberized compound; a sealing layer of a vul-canizable material impervious to air overlaying said mani-fold ply and said tubular members, and at least another sealing layer of a vulcanizable material impervious to air underlaying said tubular members.
each said tubular members being covered with in-cure, non-flowing rubberized compound; a sealing layer of a vul-canizable material impervious to air overlaying said mani-fold ply and said tubular members, and at least another sealing layer of a vulcanizable material impervious to air underlaying said tubular members.
2. An inflatable deicer boot as set forth in claim 1, wherein said in-cure, non-flowing rubberized compound contains greater than one percent by weight of cross-linked natural rubber.
3. An inflatable deicer boot as set forth in claim 2, wherein each of said tubular members has a channel extending longitudinally therein communicating with said passageway in said manifold ply and with said ports.
4. An inflatable deicer boot as set forth in claim 1, 2 or 3, wherein said tubular members are fabricated from a knit fabric.
5. An inflatable deicer boot as set forth in claim 1, 2 or 3, wherein said tubular members are fabricated from a tricot knit fabric.
6. An inflatable deicer boot for mounting on an airfoil comprising an inner ply for attachment to said airfoil; an extensible elastic air impervious outer ply overlaying said inner ply; a plurality of laterally spaced tubular members interposed between said inner ply and said outer ply; a manifold ply extending transversely across said tubular members; said manifold ply having a plurality of fibres on one side whose interstices form a passageway that extends laterally across said tubular members; each of said tubular members having a port that communicates with said passageway for selective inflating and deflating of said tubular members to shatter ice films accumulating on the outside surface of said boot; each of said tubular members having an inner peripheral surface of fabric;
each said tubular member having an outer surface of non-flowing, in-cure rubberized compound; fill gum between said inner and outer plies and at least the outermost tubular members, and all of said plies fill gum, and nonflowing rubberized compound being vulcanized to form a unitary integral deicer boot.
each said tubular member having an outer surface of non-flowing, in-cure rubberized compound; fill gum between said inner and outer plies and at least the outermost tubular members, and all of said plies fill gum, and nonflowing rubberized compound being vulcanized to form a unitary integral deicer boot.
7. An inflatable deicer boot as set forth in claim 6, wherein said fabric of said tubular members is a woven fabric.
8. An inflatable deicer boot as set forth in claim 4, wherein said nonflowing, in-cure compound for said tubular members contains over one percent by weight of cross-linked natural rubber.
9. An inflatable deicer boot as set forth in claim 8, wherein each of said tubular members has a channel that extends along one side thereof communicating with said passageway in said manifold ply, and each of said ports in each of said tubular members merges with said channel in their respective said tubular members.
10. An inflatable deicer as set forth in claim 6, 7 or 9, wherein fill gum is disposed between said laterally spaced tubular members.
11. A process for the fabrication of an inflatable deicer boot comprising the steps of mounting a plurality of laterally spaced tubular members with passageways therethrough on a lower vulcanizable elastomeric ply of material; each of said tubular members having an inner peripheral surface of fabric and being covered on an outer tubular surface with in-cure, nonflowing rubberized compound containing over one percent by weight cross-linked natural rubber; laying a manifold ply with a central passageway therein across said tubular members; said central passage-way in said manifold ply communicating with said passage-ways in said tubular members; overlaying said lower ply, tubular members and manifold ply with an upper ply of vulcanizable material, pulling a vacuum on said manifold and all of said passageways in said tubular members, vulcanizing said deicer boot into a unitary structure, and connecting an inflation valve to said manifold through said upper ply.
12. A process as set forth in claim 11, wherein said tubular members are fabricated from a knit fabric.
13. The method of fabricating an inflatable deicer comprising the steps of laying a plurality of deflated elastomeric tubular members having an inner peripheral surface of fabric and being covered on an outer tubular surface with in-cure, nonflowing rubberized compound containing over one percent by weight of cross-linked natural rubber, in laterally spaced relationship on a ply of vulcanizable elastomeric material; laying a manifold ply of vulcanizable elastomeric material across said tubular members to communicate a passageway extending through all of said tubular members with a central passage-way in said manifold ply, overlaying a ply of vulcanizable material over said first mentioned ply, said tubular members, and said manifold ply to form a deicer boot; vulcanizing said deicer boot; and connecting an inlet member to said central passageway of said manifold ply to provide means for supplying pressurized air to said tubular members and for exhausting pressurized air from said tubular members.
14. The method as set forth in claim 13, wherein said tubular members are fabricated from a knit fabric.
15. The method of fabricating an inflatable deicer as set forth in claim 13, wherein said deicer boot prior to vulcanization is covered with a ply of wicking paper, covering said boot and wicking paper with a cover ply of vulcanizable rubber; piercing said cover ply to communicate with said paper; pulling a vacuum from said pierced hole; sealing said pierced hole; vulcanizing said deicer boot; and removing said cover ply and paper to form said deicer boot.
16. The method of fabricating an inflatable deicer as set forth in claim 12, wherein said deicer boot prior to vulcanization is covered with a ply of wicking paper, covering said boot and wicking paper with a cover ply of vulcanizable rubber; piercing said cover ply to communicate with said paper; pulling a vacuum from said pierced hole; sealing said pierced hole; vulcanizing said deicer boot; and removing said cover ply and paper to form said deicer boot.
17. The method of fabricating an inflatable deicer as set forth in claim 15 or 16, wherein said deicer boot prior to vulcanization is covered with a nylon mesh fabric prior to being covered with said ply of wicking paper.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US88492378A | 1978-03-09 | 1978-03-09 | |
US884,923 | 1992-05-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1110607A true CA1110607A (en) | 1981-10-13 |
Family
ID=25385726
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA320,038A Expired CA1110607A (en) | 1978-03-09 | 1979-01-22 | Pneumatic deicer |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS54126400A (en) |
CA (1) | CA1110607A (en) |
DE (1) | DE2905627A1 (en) |
FR (1) | FR2419217A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113459613A (en) * | 2021-04-11 | 2021-10-01 | 凯迪西北橡胶有限公司 | Rubber deicing airbag for turboprop aircraft |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2436889A (en) * | 1944-06-09 | 1948-03-02 | Goodrich Co B F | Protective apparatus for preventing accumulation of ice on airfoils |
US2536739A (en) * | 1947-12-18 | 1951-01-02 | Goodrich Co B F | Apparatus for preventing the accumulation of ice upon surfaces |
US2568669A (en) * | 1948-01-23 | 1951-09-18 | Goodrich Co B F | Inflatable covering for surfaces |
FR1271461A (en) * | 1957-02-16 | 1961-09-15 | Goodrich Co B F | Inflatable device for removing ice from the surface of aircraft |
US3604666A (en) * | 1969-08-25 | 1971-09-14 | Goodrich Co B F | Pneumatic deicer |
-
1979
- 1979-01-22 CA CA320,038A patent/CA1110607A/en not_active Expired
- 1979-02-12 DE DE19792905627 patent/DE2905627A1/en not_active Withdrawn
- 1979-02-19 FR FR7904179A patent/FR2419217A1/en not_active Withdrawn
- 1979-03-09 JP JP2760079A patent/JPS54126400A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113459613A (en) * | 2021-04-11 | 2021-10-01 | 凯迪西北橡胶有限公司 | Rubber deicing airbag for turboprop aircraft |
Also Published As
Publication number | Publication date |
---|---|
DE2905627A1 (en) | 1979-09-20 |
JPS54126400A (en) | 1979-10-01 |
FR2419217A1 (en) | 1979-10-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4613102A (en) | Pneumatic deicers with template | |
US3370814A (en) | Aircraft deicing shoe | |
US5314145A (en) | Compressible nose dynamic de-icer | |
US5112011A (en) | Pneumatic deicer for shedding thin ice | |
CA1165216A (en) | Tire repair patch and method of manufacture | |
US4463919A (en) | Pneumatic deicers for aircraft | |
EP3556544B1 (en) | Propeller blade spar | |
US3604666A (en) | Pneumatic deicer | |
US8758006B2 (en) | Processes and systems for manufacturing spars and other hollow structures | |
EP3498608B1 (en) | Sewn alternate inflate pneumatic de-icer | |
FR2545786A1 (en) | PNEUMATIC DEFROSTING SYSTEM FOR AIRCRAFT | |
US4328053A (en) | Apparatus and method for retreading tires | |
US4779823A (en) | Pneumatic deicer | |
US4516745A (en) | Pneumatic deicer and deicing method | |
US4105482A (en) | Method of vulcanizing a prevulcanized tread | |
US4595442A (en) | Method of making a pneumatic deicer by vacuum pressing utilizing a curable rubber-cross-linked rubber composition | |
US5449133A (en) | Pneumatic de-icer having improved aerodynamic characteristics | |
US4361298A (en) | Pneumatic deicer | |
CA1110607A (en) | Pneumatic deicer | |
DK161756B (en) | PROCEDURE FOR FIXING A TREAD ON A COVER | |
US2547146A (en) | Hollow pontoon structure and method of making the same | |
CN101277811B (en) | Method for through repair of a composite structure comprising three skins and two core layers | |
CA1319666C (en) | Pneumatic deicer | |
CN207419390U (en) | Gas shield dam air bag | |
EP0173162A1 (en) | Pneumatic deicer |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
MKEX | Expiry |