US2364512A - Fastening of sheet material into frames and like members - Google Patents

Fastening of sheet material into frames and like members Download PDF

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Publication number
US2364512A
US2364512A US504073A US50407343A US2364512A US 2364512 A US2364512 A US 2364512A US 504073 A US504073 A US 504073A US 50407343 A US50407343 A US 50407343A US 2364512 A US2364512 A US 2364512A
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Prior art keywords
panel
groove
cement
frame
members
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US504073A
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Bower Charles
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Reid and Sigrist Ltd
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Reid and Sigrist Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476Canopies; Windscreens or similar transparent elements
    • B64C1/1492Structure and mounting of the transparent elements in the window or windscreen
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/47Molded joint

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)

Description

Dec. 5, 1944. c. BOWER 2,364,512
FASTENING OF SHEET MATERIAL INTO FRAMES AND LIKE MEMBERS Filed Sept. 27, 1945 Inventor Attorneys Fatented Wee. 5, P944 FASTENING OF SHEET MATERIAL INTO FRAMES AND LIKE MEMBERS Charles Bower, Kirby Muxloe, England, assignor to Reid and Sigrist Limited, Kirby Muxloe,
England Application September 27, 1943, Serial No. 504,073 In Great Britain October 22, 1942 4 Claims.
This invention relates to the securing of panels into frames and the like and its object is to provide a method which will allow the panel to move lengthwise in the frame members while preventing it from being withdrawn edgewise. The method according to this invention is particularly useful in cases where the panel is of a material different from that of the frame and in which, therefore, differential thermal expansion might cause the panel or the frame to be buckled or otherwise damaged.
The invention may advantageously be employed for securing the margins of windows, hoods and the like of aircraft in metal frame members. Such windows or hoods are ordinarily made of transparent synthetic resin or like materials, such for example as those known under the registered trade-marks Perspex and Plexiglass, and the marginal parts have hitherto been secured to frames or reinforcing members of channel or grooved cross-section by means of rivets, screws or the like. It has been found in practice, however, that the differential expansion and contraction between the synthetic resin material and the metal of the frame, and the vibration to which they are subjected, sometimes cause the material to break away from the rivets or the like.
According to the present invention this disadvantage is avoided by securing the margin of the panel in the groove in the frame or like member by means of a cement which adheres to the panel but not to the frame member, and which fills the space between the panel and the sides of the groove, the groove being undercut or otherwise shaped in cross-section so that when the cement filling solidifies the edge of the panel is positively held against movement towards the mouth of the groove.
The cement may. be prevented from adhering to the frame member by coating the internal surface of the groove with material such as grease or oil, or with French chalk or like powdery material, either alone or in conjunction with grease or oil, prior to the insertion of the cement. Alternatively, the groove may be lined with thin sheet material which is not adversely affected by the cement. For example, thin sheet rubber, or the sheet material known under the registered trade-mark Cellophane may be used for this purpose.
The cement may consist of a paste containing a solvent, in which case it solidifies by evaporation of the solvent, or it may be a thermoplastic material requiring heat to bring it into the re- 'tate in the case of Perspex.
quired pasty or semi-pasty condition, and becoming solid when cool.
Referring to the accompanying drawing:
Figure 1 is a perspective view of a metal channel member and a portion of the panel to be secured therein;
Figure 2 is a cross-section showing the cement inserted and the margin of the panel about to be inserted;
Figure 3 is a view similar to Figure 2 showing the joint completed; and
Figures 4, 5 and 6 are views similar to Figure 3 showing modified forms of channel member.
Referring to Figures 1 to 3, which show the preferred form of channel member, this member is made of sheet metal bent to a channel section, one side Ill being fiat and the other side it reversely curved so that the groove M is of unsym metrical bulb shape. The edge of the flat side Ill extends beyond the edge of the curved side it, thereby making the panel l6 stronger along the line where it leaves the frame firstly by avoiding steep temperature gradients when the parts are being warmed or cooled, and secondly by reinforcing the panel where the bending moment is liable to be greatest. The width of the groove is at the neck of the bulb is just sufiicient to admit the panel l6 and the maximum width of the lower bulbous portion of the groove is about twice the thickness of the panel. The edge of the panel is bevelled as indicated at It on the side which is to lie against the flat side ll] of the frame.
The inner surface of the groove is smeared or spread with oil and then coated with powdery material, such as French chalk, this coating being indicated at 20. cement 22 is then inserted and is uniformly distributed along the length of the groove. The amount of cement used is such that when the edge of the panel I6 is inserted into the groove and pressed home, the cement occupies substantially the whole of the remaining space within the bulb portion of the groove as shown in Figure 3.
In the case of a window, hood or the like made of Perspex or similar material, the cement may conveniently consist of the same material made into a paste with a suitable solvent, which may be benzene, toluene, Xylene, acetone, chloroform, trichlorethylene, or ethyl-, butyl-, or amyl-ace- Such a cement attaches itself very firmly to the window or the like owing to the action of the solvent and when the solvent has evaporated the bulb portion of the groove is occupied by a hard beading formed The appropriate quantity of.
partly by the margin of the window or the like and partly by the cement integrally united therewith. This beading prevents the window or the like from being drawn out of the groove edgewise but owing to the action of the French chalk and the oil or grease coating, the beading is free to move lengthwise in the groove. Thus, the window or the like and the frame can expand and contract independently when temperature changes occur and the straining of either of the parts is avoided. Furthermore, owing to the avoidance of rivets or the like fastening devices, vibration cannot set up heavy local stresses which might cause fracture.
Figure 4 shows a modified frame, the crosssection of which is a symmetrical bulb. Figure 5 shows another form in which the frame is of rectangular section; and Figure 6 shows yet another form having its two sides 24, 26 of unequal height, as in the form shown in Figures 1 to 3, and of waved or sinuous shape in cross-section, so that although the width of the groove is the same at all points the cement 22 forms longitudinal beadings or bulges on the panel it which prevent the withdrawal of the panel. It will be evident that many other forms of frame may be employed, the only requirements being that the cross-section of the groove should be substantially uniform throughout its length and should be such that the cement forms one or more ibeadings which prevent the withdrawal of the panel.
It will [be understood that the invention is applicable also to panels or the like of material other than plastics, for example plywood, fibreboard and the like and in such cases a cement is employed which becomes bonded to the rough or fibrous surfaces of these materials. A suitable cement for uch materials may consist of a viscous solution of Celluloid in acetone or amyl acetate with a filling of saw-dust.
What I claim is:
1. The method of securing the margin of a panel in a frame member formed with a groove at least one side of which is spaced away from the surface of the panel to form a substantially closed pocket, consisting in applying a coating of adhesion-preventing material to the surfaces of said groove, inserting into said groove a quantity of viscous cement which adheres to the rpanel but not to the coated surfaces of the frame member, said quantity being less than that required to fill the groove, inserting the margin of the panel edgewise into the groove to displace said cement into said pocket and maintaining said panel in place until the cement has solidified, thereby to produce a solid projection on the panel which prevents the panel from being withdrawn from the groove edgewise while allowing endwise movement of the panel in the groove.
2. The method of securing the margin of a [panel in a frame member formed with a groove at least one side of which is spaced away from the surface of the panel to form a substantially closed :pocket, consisting in applying a. coating of grease and French chalk to the surfaces of said groove, inserting into said groove a quantity of viscous cement which adheres to the panel but not to the coated surfaces ofthe frame member, said quantity being less than that required to fill the groove, inserting the margin of the panel edgewise into the groove to displace said cement into said pocket and maintaining said panel in place until the cement has solidified, thereby to produce a solid projection on the panel which :prevent the panel from being withdrawn from the groove edgewise while allowing endwise movement of the panel in the groove.
3. The method of securing the margin of a panel in a frame member formed with a groove at least one side of which is spaced away from the surface of the (panel to form a substantially closed pocket, consisting in inserting a lining of thin sheet material into said groove, inserting into said groove a quantity of viscous cement which adheres to the panel, said quantity being less than that required to fill the groove, inserting the margin of the panel edgewise into the groove to displace said cement into said pocket and maintaining said panel in place until the cement has solidified, thereby to produce a solid projection on the panel which prevents the panel from being withdrawn from the groove edgewise while allowing endwise movement of the panel in the groove.
4. The method of securing the margin of a panel of synthetic resin in a fram member formed with a groove at least one side of which is spaced away from the surface of the panel to form a substantially closed pocket, consisting in coating the surfaces of said groove with adhesion-preventing material, and filling said pocket with a cement consisting of said synthetic resin and a solvent thereof said cement when it has become solidified forming a. solid integral projection on the panel which prevents the panel from being withdrawn from the groove edgewise while allowing endwise movement of the panel in the groove.
CHARLES Bowen.
US504073A 1942-10-22 1943-09-27 Fastening of sheet material into frames and like members Expired - Lifetime US2364512A (en)

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2440616A (en) * 1944-12-02 1948-04-27 Lockheed Aircraft Corp Apparatus for testing panels and the like
US2534947A (en) * 1946-12-31 1950-12-19 Elvin M Bright Golf club head
US2576392A (en) * 1945-05-15 1951-11-27 Pittsburgh Plate Glass Co Laminated glass unit
US2954992A (en) * 1955-02-15 1960-10-04 Gen Motors Corp Ball and socket joint assembly and method of making same
US3098698A (en) * 1961-10-31 1963-07-23 Saint Gobain Corp Method of attaching a metal channel to a glass plate
US3098357A (en) * 1959-01-26 1963-07-23 Continental Aviat & Eng Corp Gas turbine engine construction
US3542913A (en) * 1967-12-28 1970-11-24 Buckeye Molding Co Process for capping containers
FR2406528A1 (en) * 1977-10-18 1979-05-18 Rotring Werke Riepe Kg PROCESS FOR MAKING STENCILS FOR WRITINGS OR DRAWINGS
US4382049A (en) * 1981-11-30 1983-05-03 Mcdonnell Douglas Corporation Forming a lightning spark isolation barrier
US20040121109A1 (en) * 2002-12-20 2004-06-24 Anderson Richard N. Process for manufacturing composite profiles

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2440616A (en) * 1944-12-02 1948-04-27 Lockheed Aircraft Corp Apparatus for testing panels and the like
US2576392A (en) * 1945-05-15 1951-11-27 Pittsburgh Plate Glass Co Laminated glass unit
US2534947A (en) * 1946-12-31 1950-12-19 Elvin M Bright Golf club head
US2954992A (en) * 1955-02-15 1960-10-04 Gen Motors Corp Ball and socket joint assembly and method of making same
US3098357A (en) * 1959-01-26 1963-07-23 Continental Aviat & Eng Corp Gas turbine engine construction
US3098698A (en) * 1961-10-31 1963-07-23 Saint Gobain Corp Method of attaching a metal channel to a glass plate
US3542913A (en) * 1967-12-28 1970-11-24 Buckeye Molding Co Process for capping containers
FR2406528A1 (en) * 1977-10-18 1979-05-18 Rotring Werke Riepe Kg PROCESS FOR MAKING STENCILS FOR WRITINGS OR DRAWINGS
US4225548A (en) * 1977-10-18 1980-09-30 Mesne Koh-I-Noor Rapidograph, Inc. Method for producing drawing stencils
US4382049A (en) * 1981-11-30 1983-05-03 Mcdonnell Douglas Corporation Forming a lightning spark isolation barrier
US20040121109A1 (en) * 2002-12-20 2004-06-24 Anderson Richard N. Process for manufacturing composite profiles

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