US3388651A - Covering for airplanes and method for applying same - Google Patents

Covering for airplanes and method for applying same Download PDF

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Publication number
US3388651A
US3388651A US523599A US52359966A US3388651A US 3388651 A US3388651 A US 3388651A US 523599 A US523599 A US 523599A US 52359966 A US52359966 A US 52359966A US 3388651 A US3388651 A US 3388651A
Authority
US
United States
Prior art keywords
covering
frame
adhesive
plastic
airplane
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 - Lifetime
Application number
US523599A
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English (en)
Inventor
Axelrod Sidney
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.)
TOP FLITE MODELS Inc
Original Assignee
TOP FLITE MODELS Inc
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 TOP FLITE MODELS Inc filed Critical TOP FLITE MODELS Inc
Priority to US523599A priority Critical patent/US3388651A/en
Priority to GB24600/66A priority patent/GB1104353A/en
Priority to DEA52653A priority patent/DE1243570B/de
Priority to DEA26690U priority patent/DE1953943U/de
Application granted granted Critical
Publication of US3388651A publication Critical patent/US3388651A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00—Toy aircraft; Other flying toys
    • A63H27/001—Making or assembling thereof, e.g. by folding
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00—Toy aircraft; Other flying toys
    • A63H27/02—Model aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C61/00—Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor
    • B29C61/06—Making preforms having internal stresses, e.g. plastic memory
    • B29C61/0608—Making preforms having internal stresses, e.g. plastic memory characterised by the configuration or structure of the preforms
    • B29C61/0616—Making preforms having internal stresses, e.g. plastic memory characterised by the configuration or structure of the preforms layered or partially layered preforms, e.g. preforms with layers of adhesive or sealing compositions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2067/00—Use of polyesters or derivatives thereof, as moulding material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/722—Decorative or ornamental articles

Definitions

  • This invention relates to a covering for airplanes and more particularly relates to a covering for model airplanes and the method for applying the same.
  • Model airplanes which are built for the sport of flying normally comprise an airplane frame covered by a light weight material.
  • a thin light material of paper or silk was placed over the frame, then wetted to cause shrinkage, after which many layers of dope or lacquer were placed over the material.
  • a thin light material of paper or silk was placed over the frame, then wetted to cause shrinkage, after which many layers of dope or lacquer were placed over the material.
  • Even the most skilled found that the aforementioned method had many objectionable features.
  • the main objection was the time involved in properly covering and finishing the airplane frame. lIn fact, many who were interested in the flying or competitive aspect of a model airplane hobby were discouraged from pursuing the same due to the time factor in fabricating the airplane models.
  • lt is a further object to provide an airplane covering that is not susceptible to the occurrences of weight imbalances when applied over the frame.
  • a ⁇ defect in prior model airplane coverings was the susceptibility of the same to lose its bond with the frame when fuel would seep into the area between the outer surface of the covering and the frame.
  • the inside was through the lap over joint which is the area where an edge of a portion of the covering lies ori a surface of another portion of :the covering.
  • the fuel would eat its way through the paint finish and the dope.
  • Still a further defect of some of the prior model airplane coverings was the tendency of the same to develop a large tear from even the slightest puncture.
  • FIGURE l is a perspective view of a model airplane ernbodying the principles of the invention.
  • FIGURE 2 is a wing of a model airplane with portions of the covering cut away to show the wing structure of the frame;
  • FIGURE 3 is a sectional view showing a layer of pressure sensitive adhesive material attached between a layer of plastic material and a layer of release paper;
  • FIGURE 4 is a fragmentary sectional view showing the adhesive layer attached to the plastic layer and spaced from a section of the frame of the model airplane;
  • FIGURE 5 is an enlarged fragmentary sectional view showing the adhesive layer attached to a porous frame and with portions of the adhesive layer extending into the pores of the frame;
  • FIGURE 6 is an enlarged fragmentary View of the tail of the model airplane in FIGURE l, and showing in phantom movable parts thereof in an angularly displaced position;
  • FIGURE 7 is a sectional view taken substantially on the plane of the line '7 7 in FIGURE 6, viewed in the 3 direction indicated, and showing the model airplane covering acting as a joint to permit movement of one section from another;
  • FIGURE 8 is a fragmentary enlarged sectional view illustrating the lap joint on a model airplane covering where an edge of a portion of the plastic layer lies on a surface of another portion of the plastic layer.
  • FIGURE l illustrates a model of a conventional airplane having a pair of wings 12 and a tail 14 iixedly attached to the main body section or fuselage 16 when operatively assembled together.
  • a covering 18 extends over substantially the entire airplane frame and is generally attached to the main parts thereof prior to the assembling of the same.
  • the covering 18 comprises an outer layer or lilm of a clear plastic material 24 and an inner layer of adhesive 26 which is adhesively attached to the inside surface of the plastic layer 24 (FIGS. 4 and 5).
  • the adhesive layer 26 may be of the pressure sensitive type.
  • the adhesive 26 is preferably releasably attached to a sheet of release paper 30 (FIG. 3).
  • a polyester resin such as Mylar has been found to be an acceptable plastic material.
  • An acrylic material has been successfully used as a pressure sensitive adhesive.
  • Coloring for the covering 18 is provided in the adhesive layer 26.
  • Dyes such as inorganic pigments of the type used in paints, may be incorporated into the adhesive to provide the various colors. In this manner, the coloring of the model airplane is protected by the plastic outer layer 44 and, hence, does not wear away due to the exposure to the elements nor dissolve from the effects of fuel.
  • a dry adhesive layer 26 which is activated by heat or a solvent is also within the contemplation of this invention.
  • a suitable material to the exposed face of a pressure sensitive adhesive, the same may also be converted ⁇ into a dry adhesive.
  • a powder made from a zinc stearate material was sprinkled over the exposed face of a pressure sensitive adhesive causing the same to loose its tackiness. After covering a portion of the model airplane frame and applying heat and pressure to the plastic layer 26, the adhesive was activated and caused a bond between the plastic and the frame.
  • Zinc stearate is referred to merely for example, and other materials that would cause the cnverting of the pressure sensitive adhesive to a dry adhesive and the activation of the adhesive with heat, would also be suitable.
  • the adhesive coated plastic may be conveniently stored in rolls rather than sheets and any particular length thereof could be easily dispensed therefrom and shipped to the purchaser. Also, with a dry adhesive the adhesive coated plastic is manipulable into the proper position with greater facility, and furthermore there would be substantially less possibility of the plastic wrinkling when applying the same to the airplane frame.
  • the length and shape constituting the covering or portions thereof are initially cut out from a sheet comprising a layer of clear plastic material 24 and a layer of colored adhesive 26 coated to the plastic and releasably attached to a layer of release paper 30 (FIG. 3).
  • a layer of release paper 30 (FIG. 3).
  • the adhesive were a dry adhesive, the layer of release paper would not be necessary.
  • the release paper 30 is removed from the cut out adhesive coated plastic, the same as shown in FIG. 4, may now be applied to a section 31 of the model airplane frame.
  • the plastic layer 24 After applying,r the adhesive layer 26 to the frame, the plastic layer 24 is smoothened out in every direction to remove wrinkles therefrom and to press the adhesive layer 26 in tight contact with the area of the airplane it covers. Although the smoothing out of the plastic layer 24 straightens the same, it will be immediately apparent that the tautness is substantially less than desired.
  • heat should initially be applied to the outer perimeters of the frame to cause the plastic layer 24 thereat lto make a secure bond with the frame. Then, heat is applied to the area of the plastic layer 24 between the bonded perimeters and upon cooling the plastic shrinks tight against the frame. With particular reference to FIGURE 2, the initial application of heat .is applied along the lateral edges 32 of the wing 12 to bond the plastic thereto.
  • the method of the invention does not require that the covering be initially placed on the frame in a careful and smooth manner or that the covering be wrinkle free.
  • the heating of the plastic layer will remove all traces of wrinkles and provide a skin tight and wrinkle free covering.
  • the heat is applied to the lateral edges for a suicient length of time to permit a portion of the adhesive layer 26 to impregnate the pores and thereby securely bond the plastic layer 24 to the frame edges, as is particularly shown in FIGURE 5.
  • the heat may be necessary to apply sufficient pressure with the heat in order to compress the adhesive and force the same into the pores. With the adhesive impregnated in the pores, a secure bond is made with the irregularly shaped walls of the pores.
  • the heating of the edge of the adhesive layer 26a causes the plastic layer 24a to make a secure bond with plastic layer 2412 at the lap joint or seam 36.
  • the lap joint 36 on the covering 1S is the area where an edge of a portion of the plastic layer lies on the surface of another portion of the plastic layer.
  • the part of the covering 18 at the joint 36 is compressed tight together with heat and pressure to afford a secure bond thereat. This prevents the seepage of the fuel used by the model airplane in between the plastic layer 24 and the frame.
  • the heat appears to seal or cure the adhesive and prevent the same from dissolving from the fuel.
  • a fuel :film often forms on the covering and heretofore would cause the dissolving or loosening of the covering from the trame.
  • the tail 14 includes a rudder 38, a iin 4t) and stabilizer 42.
  • Stabilizer 42 includes a movable elevator 44. The movement of rudder 38 and elevator 44 may be controlled.
  • the covering 13 is adaptable to provide a movable joint 50 to permit the rudder 3S to be pivoted outwardly away from iin 40.
  • the covering 13 on the upper surface of the rudder 38 and iin 40 does not extend across the adjacent edges thereof.
  • the covering 18 on the lower surfaces extends across the adjacent edges to afford a pivot 50 whereby rudder 38 may be pivoted away from lin 40 as shown in phantom in FIGURE 7.
  • the adjacent edges of the iin and rudder are angled to permit the movement of the rudder upward or downward (FIG. 7).
  • 56 on the wing 12 may use the covering 18 for a pivot joint.
  • the adhesive layer 26 is dyed to a particular color and hence the application of the covering to the frame has eliminated the need to paint the airplane. Therefore, by predetermining the airplane color scheme, the various strips of adhesive plastic applied to the frame would correspond accordingly to the desired coloring. Moreover, any dirt and grime that collects on the plastic layer may be wiped clean therefrom and the airplane, even after much use, would have a new glossy appearance. Also, by having the coloring inside the adhesive and the plastic layer thereover, there is no damage or chipping of paint which, heretofore, invariably occurred after even the slightest use.
  • a covering material applied thereto comprising a flexible, clear heat-shrunk film of polyester resin precoated over substantially the entire surface of one side with a layer of adhesive containing coloring material interspersed therewith, said layer of adhesive and interspersed coloring material being bonded to said iilm.
  • a method for covering an airplane frame with a covering material comprising a flexible, clear, heatshrinkahle film of polyester resin pre-coated on one side with a layer of adhesive containing coloring material, the steps of applying a predetermined length of said covering material to a section of said frame so that the film comprises the outer side thereof and thereafter applying heat to the film to cause the lm to shrink tautly to the contours of the frame and the adhesive to bond the lm to the frame.
  • a covering for a model airplane frame comprising: an outer plastic lm; an adhesive layer of material between said plastic film and said frame, said adhesive layer securing said plastic film to the frame; and said frame including at least one movable section, the edge of the movable section being adjacent an edge of another section of the frame, each of said sections having at least two surfaces, the covering on one surface of said sections extending only to the adjacent edges of the sections, the covering on the other surface of said sections extending across said edges to afford a pivot joint means whereby said movable section may be pivoted with respect to the other sectio-n.

Landscapes

  • Toys (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Adhesive Tapes (AREA)
  • Laminated Bodies (AREA)
US523599A 1966-01-28 1966-01-28 Covering for airplanes and method for applying same Expired - Lifetime US3388651A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US523599A US3388651A (en) 1966-01-28 1966-01-28 Covering for airplanes and method for applying same
GB24600/66A GB1104353A (en) 1966-01-28 1966-06-02 Covering material for model airplanes and other frames and methods for applying same
DEA52653A DE1243570B (de) 1966-01-28 1966-06-03 Verfahren zur Herstellung einer Bespannung des Skelettes eines Modellflugzeuges
DEA26690U DE1953943U (de) 1966-01-28 1966-11-10 Ueberzug fuer oberflaechen an flugzeugen, insbesondere flugzeugmodellen.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US523599A US3388651A (en) 1966-01-28 1966-01-28 Covering for airplanes and method for applying same

Publications (1)

Publication Number Publication Date
US3388651A true US3388651A (en) 1968-06-18

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ID=24085649

Family Applications (1)

Application Number Title Priority Date Filing Date
US523599A Expired - Lifetime US3388651A (en) 1966-01-28 1966-01-28 Covering for airplanes and method for applying same

Country Status (3)

Country Link
US (1) US3388651A (de)
DE (2) DE1243570B (de)
GB (1) GB1104353A (de)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3521630A (en) * 1967-04-07 1970-07-28 Minnesota Mining & Mfg Respirator face mask with replaceable filter
US3590517A (en) * 1968-08-10 1971-07-06 Simprop Electronic Motor driven model airplane
US3871126A (en) * 1973-06-22 1975-03-18 Edward A Miller Model airplanes and method of making same
US3935353A (en) * 1970-05-22 1976-01-27 Detroit Gasket & Manufacturing Co. Heat shrinkable decorative covering material for vehicle panels
US3945147A (en) * 1974-12-18 1976-03-23 Crowder Thomas T Hand launch glider
JPS5172548A (ja) * 1974-12-19 1976-06-23 Fuji Sangyo Co Ltd Mokeihikotaikoseibuzaino seizohoho
US4095760A (en) * 1975-10-10 1978-06-20 James A. Black Structural skin construction materials and method
US4204358A (en) * 1978-03-13 1980-05-27 Briggs Donald L Aluminum model airplane kit
DE4439031A1 (de) * 1994-11-02 1996-05-09 Siegfried Lanitz Polymerbeschichtetes Mehrschichtmaterial und Verfahren zu seiner Herstellung
WO2005037899A1 (ja) 2003-10-21 2005-04-28 Toyo Boseki Kabushiki Kaisha 熱収縮性ポリエステル系フィルムおよび熱収縮性ポリエステル系フィルムロール
US20050227582A1 (en) * 2004-01-16 2005-10-13 Kloos Wade M Composite model construction and method
US20050233672A1 (en) * 2004-04-16 2005-10-20 Michael Shantz Propeller impact protector and model flying airplane incorporating same
US20060038072A1 (en) * 2004-08-17 2006-02-23 Gary Schott Aircraft fuselage training device for fire fighters
US20090236473A1 (en) * 2008-03-21 2009-09-24 Rawdon Blaine K Providing skins for aircraft fuselages
CN103640686A (zh) * 2013-12-13 2014-03-19 新誉集团有限公司 具有温控功能的蒙皮及其制作方法
US20160017902A1 (en) * 2013-03-12 2016-01-21 Texas Tech University System Fibrillar structures to reduce viscous drag on aerodynamic and hydrodynamic wall surfaces

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1979000904A1 (en) * 1978-04-08 1979-11-15 Nielsen M Edge-sealing of plate materials
EP0039600B1 (de) * 1980-05-03 1985-12-04 Raychem Limited Vorrichtung und Verfahren zum Umschliessen von Gegenständen
GB9501088D0 (en) 1995-01-20 1995-03-08 Zeneca Ltd Monoazo pigments

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2096750A (en) * 1935-05-11 1937-10-26 Kaumagraph Co Method of printing self-attaching fabric labels
US2560742A (en) * 1949-01-29 1951-07-17 Monogram Models Inc Wing construction for model airplanes
US2767436A (en) * 1952-08-25 1956-10-23 Sanders Methods of forming smooth surfaces on thermoplastic sponge
US2802764A (en) * 1952-10-08 1957-08-13 Owens Corning Fiberglass Corp Acoustical material
US2920682A (en) * 1956-06-22 1960-01-12 Paul W Lindberg Plastic resinous toy parts and method of making and assembling the same
US3273281A (en) * 1965-10-04 1966-09-20 Lawrence V Harrison Model aircraft wing construction

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1919046A1 (de) * 1969-04-15 1970-10-22 Bayer Ag Verfahren zur Herstellung von Polypentenamer

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2096750A (en) * 1935-05-11 1937-10-26 Kaumagraph Co Method of printing self-attaching fabric labels
US2560742A (en) * 1949-01-29 1951-07-17 Monogram Models Inc Wing construction for model airplanes
US2767436A (en) * 1952-08-25 1956-10-23 Sanders Methods of forming smooth surfaces on thermoplastic sponge
US2802764A (en) * 1952-10-08 1957-08-13 Owens Corning Fiberglass Corp Acoustical material
US2920682A (en) * 1956-06-22 1960-01-12 Paul W Lindberg Plastic resinous toy parts and method of making and assembling the same
US3273281A (en) * 1965-10-04 1966-09-20 Lawrence V Harrison Model aircraft wing construction

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3521630A (en) * 1967-04-07 1970-07-28 Minnesota Mining & Mfg Respirator face mask with replaceable filter
US3590517A (en) * 1968-08-10 1971-07-06 Simprop Electronic Motor driven model airplane
US3935353A (en) * 1970-05-22 1976-01-27 Detroit Gasket & Manufacturing Co. Heat shrinkable decorative covering material for vehicle panels
US3871126A (en) * 1973-06-22 1975-03-18 Edward A Miller Model airplanes and method of making same
US3945147A (en) * 1974-12-18 1976-03-23 Crowder Thomas T Hand launch glider
JPS5172548A (ja) * 1974-12-19 1976-06-23 Fuji Sangyo Co Ltd Mokeihikotaikoseibuzaino seizohoho
US4095760A (en) * 1975-10-10 1978-06-20 James A. Black Structural skin construction materials and method
US4204358A (en) * 1978-03-13 1980-05-27 Briggs Donald L Aluminum model airplane kit
DE4439031A1 (de) * 1994-11-02 1996-05-09 Siegfried Lanitz Polymerbeschichtetes Mehrschichtmaterial und Verfahren zu seiner Herstellung
US6548428B1 (en) 1994-11-02 2003-04-15 Siegfried Lanitz Polymer-coated multi-layer material and process for producing it
WO2005037899A1 (ja) 2003-10-21 2005-04-28 Toyo Boseki Kabushiki Kaisha 熱収縮性ポリエステル系フィルムおよび熱収縮性ポリエステル系フィルムロール
US20070104931A1 (en) * 2003-10-21 2007-05-10 Toyo Boseki Kabushiki Kaisha Heat-shrinkable polyester film and heat-shrinkable polyester film roll
EP1681312A4 (de) * 2003-10-21 2009-04-15 Toyo Boseki Wärmeschrumpfbare polyesterfolie und rolle von wärmeschrumpfbarer polyesterfolie
EP1681312A1 (de) * 2003-10-21 2006-07-19 Toyo Boseki Kabushiki Kaisha Wärmeschrumpfbare polyesterfolie und rolle von wärmeschrumpfbarer polyesterfolie
US20050227582A1 (en) * 2004-01-16 2005-10-13 Kloos Wade M Composite model construction and method
US20050233672A1 (en) * 2004-04-16 2005-10-20 Michael Shantz Propeller impact protector and model flying airplane incorporating same
US7331838B2 (en) * 2004-04-16 2008-02-19 Jasman Asia Ltd. Propeller impact protector and model flying airplane incorporating same
US20060038072A1 (en) * 2004-08-17 2006-02-23 Gary Schott Aircraft fuselage training device for fire fighters
US7527499B2 (en) * 2004-08-17 2009-05-05 Gary Schott Aircraft fuselage training device for fire fighters
US20090236473A1 (en) * 2008-03-21 2009-09-24 Rawdon Blaine K Providing skins for aircraft fuselages
US8128025B2 (en) * 2008-03-21 2012-03-06 The Boeing Company Providing skins for aircraft fuselages
US20160017902A1 (en) * 2013-03-12 2016-01-21 Texas Tech University System Fibrillar structures to reduce viscous drag on aerodynamic and hydrodynamic wall surfaces
US10830261B2 (en) * 2013-03-12 2020-11-10 Texas Tech University System Fibrillar structures to reduce viscous drag on aerodynamic and hydrodynamic wall surfaces
CN103640686A (zh) * 2013-12-13 2014-03-19 新誉集团有限公司 具有温控功能的蒙皮及其制作方法
CN103640686B (zh) * 2013-12-13 2016-01-13 新誉集团有限公司 具有温控功能的蒙皮的制作方法

Also Published As

Publication number Publication date
DE1243570B (de) 1967-06-29
GB1104353A (en) 1968-02-28
DE1953943U (de) 1967-01-19

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