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US3710476A - Avionic tray - Google Patents

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US3710476A
US3710476A US00125536A US3710476DA US3710476A US 3710476 A US3710476 A US 3710476A US 00125536 A US00125536 A US 00125536A US 3710476D A US3710476D A US 3710476DA US 3710476 A US3710476 A US 3710476A
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Prior art keywords
backplate
tray
members
holes
electronic equipment
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US00125536A
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R Hollingsead
C Pryor
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HOLLINGSEAD PRYOR ENTERPRISES
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HOLLINGSEAD PRYOR ENTERPRISES
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    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00Constructional details common to different types of electric apparatus
    • H05K7/14Mounting supporting structure in casing or on frame or rack
    • H05K7/1401Mounting supporting structure in casing or on frame or rack comprising clamping or extracting means
    • H05K7/1411Mounting supporting structure in casing or on frame or rack comprising clamping or extracting means for securing or extracting box-type drawers
    • H05K7/1412Mounting supporting structure in casing or on frame or rack comprising clamping or extracting means for securing or extracting box-type drawers hold down mechanisms, e.g. avionic racks
    • 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
    • Y10T403/16Joints and connections with adjunctive protector, broken parts retainer, repair, assembly or disassembly feature
    • Y10T403/1616Position or guide means
    • Y10T403/1624Related to joint component

Definitions

  • An avionic tray having a backplate secured between a pair of vertical uprights of the tray with the aid of self-jigging structure located thereon.
  • the vertical uprights include a plurality of jig pins formed on the interior sides thereof which are adapted to snap into a plurality of registering holes formed in the backplate.
  • the jig pins are formed by a half-shear punch process, while the holes are also formed by a punching process.
  • a pair of precision dies are used to accurately locate the jig pins and holes to ensure precise linear and angular positioning of the backplate relative to the tray prior to securing the backplate to the uprights with rivets, bolts or other attachment 10 Claims, 5 Drawing Figures AVIONIC TRAY BACKGROUND OF THE INVENTION 1.
  • Field of the Invention v
  • the present invention relates to means for attaching one member to another and more particularly to means for accurately positioning the two members prior to securing the two members together.
  • each piece of electronic equipment is supported on an individual tray.
  • Each tray usually comprises a bottom section having a pair of side rails extending upwardly therefrom.
  • the side rails function as guides for the supported instrument during installation and also serve as a lateral support after installation.
  • the side rails further include a pair of upright sections which are adapted to be connected to and support a backplate therebetween.
  • the backplate usually includes a pair of dagger pins accurately positioned on its front face for mating with the rear of the instrument to function as a rear hold down.
  • An electrical receptacle is mounted on the backplate and functions to receive the connectors extending out of the rear end of the instrument.
  • the backplate is also provided with a cut-out portion for receiving a portion of the receptacle along with the receptacle wires. After the backplate is connected to the tray, the backplate functions to absorb a hold-down load that is applied to the instrument from the front of the shelf. This hold-down load, usually of the magnitude of one hundred pounds, is necessary to secure the instrument during flight.
  • a serious shortcoming involved with prior assemblies is that because of the tolerance buildup involved in connecting the backplate to the tray, a great amount of misalignment occurs. This not only results in the improper support of the instrument but also results in faulty electrical connections between the instrument and the receptacles.
  • This tolerance buildup occurs in the bolting or riveting process used in interconnecting the backplate to the upright sections of the tray. More specifically, in drilling the bolt or rivet holes in the two elements, care must be taken to ensure that the center lines of the holes in each side of the connections are perpendicular to the bottom section of the tray. If such drilling is done by hand, inaccuracies occur that are quite large. If the drilling is done by machine, the accuracy is improved.
  • the bolts are inserted in upper and lower registering holes of the side sections of the backplate and the uprights. Because of the loose fit of the bolts, the backplate can be easily tilted as the bolts are applied. In fact, the bottom of the backplate can move in one direction the total amount of tolerances found in the two holes and the bolt, while the upper portion of the backplate can move the same distance in the opposite direction. This tolerance buildup can actually result in a total angular displacement of up to 15 from the perpendicular. Not only is this angular displacement of the backplate sufficient to cause misalignment of the instrument, but it is sufficient enough to prevent the instrument from being properly connected to the electrical receptacle mounted on the backplate.
  • the present invention obviates the above-mentioned shortcoming by providing self-jigging means for perpendicularly mounting the backplate on the tray with a high degree of accuracy.
  • the uprights of the tray are provided with jig pins formed thereon which are adapted to mate with registering apertures on the backplate to permit the backplate to be snapped onto the uprights in a perpendicular relationship before the bolts or rivets are secured within the holes.
  • a die having a perpendicular edge is positioned adjacent the bottom surface of the tray.
  • a pair of female holes is located on each side of the die with the center lines of these holes being perpendicular to the base plate.
  • a pair of male punches of a diameter larger than the diameter of the female holes is then applied to the opposite side of the uprights to press metal from the uprights inwardly into the female holes of the die. The punches extend half way into the uprights to half-shear the pressed metal to form.
  • a plurality of jig pins Registering holes are likewise formed in the backplate with the exception that punches equal to the size of the female holes are utilized to extend entirely through the material of the backplate and completely shear off the metal and form the holes.
  • the main advantage of the present invention is that the interconnecting members have self jigging means formed thereon which function to align the backplate in a perpendicular position with respect to the tray with a high degree of accuracy prior to applying the bolts or rivets. In this manner, the interconnection of the memhers is not influenced in any way by the tolerance buildup or the rivet or bolt means.
  • FIG. 1 is an exploded view of an avionic die apparatus having a backplate positioned between two uprights by means of self-jigging means in accordance with the present invention
  • FIG. 2 is a fragmentary perspective view showing a die positioned on the tray to form the jig pins
  • FIG. 3 is a fragmentary perspective view of the rear of the backplate, showing a die positioned therein to form the jig holes;
  • FIG. 4 is an enlarged fragmentary sectional view of the jig pin connection; and 7 FIG. is a fragmentary perspective view of the apparatus in its assembled form.
  • FIG. 1 shows an avionic tray, generally indicated by arrow 10, for supporting an electronic instrument (shown in broken lines).
  • the tray 10 comprises a bottom section 11 and a pair of side rails 13 extending upwardly along the lateral edges thereof.
  • the bottom section llis adapted to be mounted'at its ends to a pair of cross channels 15.
  • the bottom section 1 1 also includes a metering section 17 extending below the surface of the tray with-the metering section 17 having a plurality of metering ports 19 for controlling the amount of air drawn through the instrument.
  • An annular'gaske t 21 extends around the periphery of the metering section 17 and above the surface of the tray to sealingly engage the bottom of the supported instrument.
  • the side rails 13 further include a pair of uprights 23 which are adapted to be connected to and laterally support a backplate 25.
  • Thebackplate 25 is perpendicularly positioned with respect to the bottom surface of the tray and includes a pair of dagger pins 27 for mating with a pair of registering apertures on the supported instrument.
  • the backplate further includes a cut-out portion 29 for receiving a portion of an electrical receptacle (not, shown) along with the receptacle wires.
  • the backplate 25 functions to support the rear of the instrument as a holding force is applied at the front of the instrument.
  • the perpendicular orientation of the backplate 25 permits the instrument to lie flush against the backplate 25 to ensure a proper electrical connection between the instrument and the receptacle.
  • the backplate 25 is secured to the uprights 23 by means of bolts 31 extending through registering holes 33 formed on the uprights 23 and the lateral sides 35 of the backplate 25 Prior to such connections, however, the backplate is mounted on the uprights by means of jig pins 37 formed on the interior sides of the uprights 23 which extend into a plurality of registering apertures 39 formed in the lateral sides 35 of the backplate 25.
  • a die 41 is utilized having a face portion 43 on the bottom edge thereof which is adapted to contact the bottom surface of the tray 10.
  • a plurality of female apertures 45 is formed within the lateral sides of the die 41 with each pair of apertures being accurately formed to cause their center lines to be perpendicular to the face portion 43.
  • the die 41 is mounted on the tray 10 in such a manner that the face portion 43 rests against the bottom section 11 of the tray 10 and the female apertures 45 are aligned adjacent the uprights 23.
  • a plurality of punches 47 are then provided to contact that por-, tion of the uprights 23 that registers with the female apertures 45.
  • the punches 47 are dimensioned to be larger than the diameter of the female apertures.
  • a second die 49' is provided to extend within the cavity formedin the backplate 25.
  • the die 49 includes a face portion 51 adapted to lie flush against the rear surface of the backplate 25 and a pair of lateral sides having pairs of female apertures 53 whose center lines are parallel to the face portion 51.
  • a second plurality of punches 55 are provided to contact the backplate material adjacent the female apertures 53 with the punches being of the same cross sectional area as the female apertures. This permits the punches 55 to extend entirely through the backplate material to completely shear off the punched out portion to form the apertures 53.
  • backplate 25 is first snapped onto the jig pins 37 of the uprights 23.
  • a typical connection is shown in FIG. 4. Because of the exceptionally low tolerances of i the manufacturing process, the backplate is precisionally positioned to be perpendicular with respect to bottom section 11 of the tray 10. In such a secured position the bolts 31 are then inserted through the aligned holes 33 with each connection being secured by a nut.
  • the backplate 25 is shown connected to the uprights 23 in FIG. 5.
  • the backplate 25 is secured in position before the bolts 31 are used. As a result, the positioning of the backplate 25 is completely independent of the tolerance buildup found and the holes.
  • the forming of the jig pins 37 and apertures 39 is accomplished with a very high degree of accuracy.
  • the dies 41 and 49 are both precisionally made and are easy to operate.
  • Apparatus for securing a backplate member 'on a tray comprising: I
  • the apparatus of claim 1 further comprising means for securing said vertical upright members to said backplate member after said jig pins are engaged in said jig holes.
  • said tray is an avionic tray adapted to support electronic equipment and said backplate is adapted to mate with said electronic equipment for fastening said electronic equipment in position and said vertical uprights are integral with said avionic tray.
  • said tray is an avionic tray adapted to support electronic equipment and said backplate is adapted to mate with said electronic equipment for fastening said electronic equipment in position; a metering plate for controlling air flow to said electronic equipment and a gasket for sealingly engaging said electronic equipment, said evionic tray having an opening on its surface for receiving said gasket and metering plate.
  • said means for securing includes said members having holes extending therethrough and fasteners for interconnecting said members.

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  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Casings For Electric Apparatus (AREA)

Abstract

An avionic tray is disclosed having a backplate secured between a pair of vertical uprights of the tray with the aid of selfjigging structure located thereon. The vertical uprights include a plurality of jig pins formed on the interior sides thereof which are adapted to snap into a plurality of registering holes formed in the backplate. The jig pins are formed by a half-shear punch process, while the holes are also formed by a punching process. A pair of precision dies are used to accurately locate the jig pins and holes to ensure precise linear and angular positioning of the backplate relative to the tray prior to securing the backplate to the uprights with rivets, bolts or other attachment means.

Description

United States Patent 1 Hollingsead et al.
[54] AVIONIC TRAY -[75] lnventors: Robert A. Hollingsead, Yorba Linda; Clyde Robert Pryor, Anaheim, both of Calif.
[73] Assignee: Hollingsead-Pryor Enterprises, Inc.,
Santa Fe Springs, Los Angeles.
County, Calif.
[22] Filed: March 18, 1971 [21] Appl. N0.: 125,536
3,426,419 2/1969 Banks ..29/200 P [451 Jan. 16, 1973 Primary Examiner-Thomas H. Eager Attorney.lackson & Jones [57] ABSTRACT An avionic tray is disclosed having a backplate secured between a pair of vertical uprights of the tray with the aid of self-jigging structure located thereon. The vertical uprights include a plurality of jig pins formed on the interior sides thereof which are adapted to snap into a plurality of registering holes formed in the backplate. The jig pins are formed by a half-shear punch process, while the holes are also formed by a punching process. A pair of precision dies are used to accurately locate the jig pins and holes to ensure precise linear and angular positioning of the backplate relative to the tray prior to securing the backplate to the uprights with rivets, bolts or other attachment 10 Claims, 5 Drawing Figures AVIONIC TRAY BACKGROUND OF THE INVENTION 1. Field of the Invention v The present invention relates to means for attaching one member to another and more particularly to means for accurately positioning the two members prior to securing the two members together.
2. Description of the Prior Art In an aircraft, each piece of electronic equipment is supported on an individual tray. Each tray usually comprises a bottom section having a pair of side rails extending upwardly therefrom. The side rails function as guides for the supported instrument during installation and also serve as a lateral support after installation. The side rails further include a pair of upright sections which are adapted to be connected to and support a backplate therebetween.
The backplate usually includes a pair of dagger pins accurately positioned on its front face for mating with the rear of the instrument to function as a rear hold down. An electrical receptacle is mounted on the backplate and functions to receive the connectors extending out of the rear end of the instrument. The backplate is also provided with a cut-out portion for receiving a portion of the receptacle along with the receptacle wires. After the backplate is connected to the tray, the backplate functions to absorb a hold-down load that is applied to the instrument from the front of the shelf. This hold-down load, usually of the magnitude of one hundred pounds, is necessary to secure the instrument during flight.
A serious shortcoming involved with prior assemblies is that because of the tolerance buildup involved in connecting the backplate to the tray, a great amount of misalignment occurs. This not only results in the improper support of the instrument but also results in faulty electrical connections between the instrument and the receptacles. This tolerance buildup occurs in the bolting or riveting process used in interconnecting the backplate to the upright sections of the tray. More specifically, in drilling the bolt or rivet holes in the two elements, care must be taken to ensure that the center lines of the holes in each side of the connections are perpendicular to the bottom section of the tray. If such drilling is done by hand, inaccuracies occur that are quite large. If the drilling is done by machine, the accuracy is improved.
However, even if the center lines are perfect, there is a tolerance problem in forming the holes to accept the rivets or bolts. This is because inthe manufacturing of rivets or bolts, there is an acceptable tolerance in which the bolt or rivet diameter can be manufactured. As a result, the holes must be drilled to such a size that even the largest bolt made within those tolerances can go through. Moreover, the holes are made within tolerances also. As a result, the holes must be dimensioned such that the low side of the tolerance level of the holes be sufficient to accommodate the bolts made on the high side of its tolerance level.
It follows, then, that through random selection, a small bolt can be mounted in relatively large holes in the backplate and uprights.
Upon installing the backplate, the bolts are inserted in upper and lower registering holes of the side sections of the backplate and the uprights. Because of the loose fit of the bolts, the backplate can be easily tilted as the bolts are applied. In fact, the bottom of the backplate can move in one direction the total amount of tolerances found in the two holes and the bolt, while the upper portion of the backplate can move the same distance in the opposite direction. This tolerance buildup can actually result in a total angular displacement of up to 15 from the perpendicular. Not only is this angular displacement of the backplate sufficient to cause misalignment of the instrument, but it is sufficient enough to prevent the instrument from being properly connected to the electrical receptacle mounted on the backplate.
SUMMARY OF THE INVENTION The present invention obviates the above-mentioned shortcoming by providing self-jigging means for perpendicularly mounting the backplate on the tray with a high degree of accuracy.
In accordance with the present invention, the uprights of the tray are provided with jig pins formed thereon which are adapted to mate with registering apertures on the backplate to permit the backplate to be snapped onto the uprights in a perpendicular relationship before the bolts or rivets are secured within the holes.
In forming these jig pins on the uprights, a die having a perpendicular edge is positioned adjacent the bottom surface of the tray. A pair of female holes is located on each side of the die with the center lines of these holes being perpendicular to the base plate. A pair of male punches of a diameter larger than the diameter of the female holes is then applied to the opposite side of the uprights to press metal from the uprights inwardly into the female holes of the die. The punches extend half way into the uprights to half-shear the pressed metal to form. a plurality of jig pins. Registering holes are likewise formed in the backplate with the exception that punches equal to the size of the female holes are utilized to extend entirely through the material of the backplate and completely shear off the metal and form the holes.
- The main advantage of the present invention is that the interconnecting members have self jigging means formed thereon which function to align the backplate in a perpendicular position with respect to the tray with a high degree of accuracy prior to applying the bolts or rivets. In this manner, the interconnection of the memhers is not influenced in any way by the tolerance buildup or the rivet or bolt means.
The features of the present invention which are believed to be novel are set forth with particularity in the appended claims. The present invention, both as to its organization and manner of operation, together with further objects and advantages thereof, may best be understood by reference to the following description, taken in connection with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is an exploded view of an avionic die apparatus having a backplate positioned between two uprights by means of self-jigging means in accordance with the present invention;
FIG. 2 is a fragmentary perspective view showing a die positioned on the tray to form the jig pins;
FIG. 3 is a fragmentary perspective view of the rear of the backplate, showing a die positioned therein to form the jig holes;
FIG. 4 is an enlarged fragmentary sectional view of the jig pin connection; and 7 FIG. is a fragmentary perspective view of the apparatus in its assembled form.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawings, FIG. 1 shows an avionic tray, generally indicated by arrow 10, for supporting an electronic instrument (shown in broken lines). The tray 10 comprises a bottom section 11 and a pair of side rails 13 extending upwardly along the lateral edges thereof. The bottom section llis adapted to be mounted'at its ends to a pair of cross channels 15. The bottom section 1 1 also includes a metering section 17 extending below the surface of the tray with-the metering section 17 having a plurality of metering ports 19 for controlling the amount of air drawn through the instrument.
An annular'gaske t 21 extends around the periphery of the metering section 17 and above the surface of the tray to sealingly engage the bottom of the supported instrument.
The side rails 13 further include a pair of uprights 23 which are adapted to be connected to and laterally support a backplate 25. Thebackplate 25is perpendicularly positioned with respect to the bottom surface of the tray and includes a pair of dagger pins 27 for mating with a pair of registering apertures on the supported instrument. The backplate further includes a cut-out portion 29 for receiving a portion of an electrical receptacle (not, shown) along with the receptacle wires. The backplate 25 functions to support the rear of the instrument as a holding force is applied at the front of the instrument. Moreover, the perpendicular orientation of the backplate 25 permits the instrument to lie flush against the backplate 25 to ensure a proper electrical connection between the instrument and the receptacle.
The backplate 25 is secured to the uprights 23 by means of bolts 31 extending through registering holes 33 formed on the uprights 23 and the lateral sides 35 of the backplate 25 Prior to such connections, however, the backplate is mounted on the uprights by means of jig pins 37 formed on the interior sides of the uprights 23 which extend into a plurality of registering apertures 39 formed in the lateral sides 35 of the backplate 25.
As shown in FIG. 2, in fabricating the jig pins 37, a die 41 is utilized having a face portion 43 on the bottom edge thereof which is adapted to contact the bottom surface of the tray 10. A plurality of female apertures 45 is formed within the lateral sides of the die 41 with each pair of apertures being accurately formed to cause their center lines to be perpendicular to the face portion 43.
In operation, the die 41 is mounted on the tray 10 in such a manner that the face portion 43 rests against the bottom section 11 of the tray 10 and the female apertures 45 are aligned adjacent the uprights 23. A plurality of punches 47 are then provided to contact that por-, tion of the uprights 23 that registers with the female apertures 45. The punches 47 are dimensioned to be larger than the diameter of the female apertures. In
pressing the material with the punches 47 a portion of the upright material is forced into the female apertures 7 ensured. The punches travel about half way through the uprights to create the half-sheared pins 37.
As shown in FIG. 3, a second die 49'is provided to extend within the cavity formedin the backplate 25. The die 49 includes a face portion 51 adapted to lie flush against the rear surface of the backplate 25 and a pair of lateral sides having pairs of female apertures 53 whose center lines are parallel to the face portion 51.
A second plurality of punches 55 are provided to contact the backplate material adjacent the female apertures 53 with the punches being of the same cross sectional area as the female apertures. This permits the punches 55 to extend entirely through the backplate material to completely shear off the punched out portion to form the apertures 53.
In connecting the backplate 25 to the tray 10, the
backplate 25 is first snapped onto the jig pins 37 of the uprights 23. A typical connection is shown in FIG. 4. Because of the exceptionally low tolerances of i the manufacturing process, the backplate is precisionally positioned to be perpendicular with respect to bottom section 11 of the tray 10. In such a secured position the bolts 31 are then inserted through the aligned holes 33 with each connection being secured by a nut. The backplate 25 is shown connected to the uprights 23 in FIG. 5.
As can be seen, the backplate 25 is secured in position before the bolts 31 are used. As a result, the positioning of the backplate 25 is completely independent of the tolerance buildup found and the holes.
Moreover, the forming of the jig pins 37 and apertures 39 is accomplished with a very high degree of accuracy. The dies 41 and 49 are both precisionally made and are easy to operate.
It should be noted that various modifications can be made to the apparatus while still remaining within the purview of the following claims.
It should also be noted that such self-jigging means can be used to secure any two elements together whenever precision alignment is required.
What is claimed is:
1. Apparatus for securing a backplate member 'on a tray comprising: I
a pair of vertical upright members connected to said tray, said backplate member positioned between said upright members;
a plurality of jig pins aligning said upright members .and said backplate member and formed on .at least one of said members; and
a plurality of jig holes formed on the other of said members for registering with said jig pins.
2. The apparatus of claim 1 further comprising means for securing said vertical upright members to said backplate member after said jig pins are engaged in said jig holes.
3. The apparatus of claim 1 wherein said jig pins are integrally formed from the material of one of said members.
in the use of the bolts pendicular to the surface of said tray.
5. The apparatus of claim 1 wherein said tray is an avionic tray adapted to support electronic equipment and said backplate is adapted to mate with said electronic equipment for fastening said electronic equipment in position and said vertical uprights are integral with said avionic tray.
6. The apparatus of claim 1 wherein said tray is an avionic tray adapted to support electronic equipment and said backplate is adapted to mate with said electronic equipment for fastening said electronic equipment in position; a metering plate for controlling air flow to said electronic equipment and a gasket for sealingly engaging said electronic equipment, said evionic tray having an opening on its surface for receiving said gasket and metering plate.
7. The apparatus of claim 2 wherein said means for securing includes said members having holes extending therethrough and fasteners for interconnecting said members.
8. The apparatus of claim 5 wherein a pair of jig pins are provided on each side of said tray.
9. The apparatus of claim 8 wherein means for locking said vertical members are provided between said jig pins.
10. The apparatus of claim 8 wherein said jig pins are I integrally formed of the material of one of said members.

Claims (10)

1. Apparatus for securing a backplate member on a tray comprising: a pair of vertical upright members connected to said tray, said backplate member positioned between said upright members; a plurality of jig pins aligning said upright members and said backplate member and formed on at least one of said members; and a plurality of jig holes formed on the other of said members for registering with said jig pins.
2. The apparatus of claim 1 further comprising means for securing said vertical upright members to said backplate member after said jig pins are engaged in said jig holes.
3. The apparatus of claim 1 wherein said jig pins are integrally formed from the material of one of said members.
4. The apparatus of claim 1 wherein said jig pins are formed such that the front face of the backplate is perpendicular to the surface of said tray.
5. The apparatus of claim 1 wherein said tray is an avionic tray adapted to support electronic equipment and said backplate is adapted to mate with said electronic equipment for fastening said electronic equipment in position and said vertical uprights are integral with said avionic tray.
6. The apparatus of claim 1 wherein said tray is an avionic tray adapted to support electronic equipment and said backplate is adapted to mate with said electronic equipment for fastening said electronic equipment in position; a metering plate for controlling air flow to said electronic equipment and a gasket for sealingly engaging said electronic equipment, said evionic tray having an opening on its surface for receiving said gasket and metering plate.
7. The apparatus of claim 2 wherein said means for securing includes said members having holes extending therethrough and fasteners for interconnecting said members.
8. The apparatus of claim 5 wherein a pair of jig pins are provided on each side of said tray.
9. The apparatus of claim 8 wherein means for locking said vertical members are provided between said jig pins.
10. The apparatus of claim 8 wherein said jig pins are integrally formed of the material of one of said members.
US00125536A 1971-03-18 1971-03-18 Avionic tray Expired - Lifetime US3710476A (en)

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Cited By (10)

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US3809969A (en) * 1973-01-30 1974-05-07 Dole Electro Systems Probe connector receptacle device for area type electrical distribution system
US4513351A (en) * 1982-09-29 1985-04-23 International Business Machines Corporation Electronic assembly with forced convection cooling
US4766517A (en) * 1987-04-28 1988-08-23 Abell Robert H Avionic tray of decreased weight
US4888664A (en) * 1988-07-05 1989-12-19 Aspen Industries, Inc. Cooling airflow coupling apparatus for avionic trays
US5129594A (en) * 1991-10-18 1992-07-14 Hollingsead International, Inc. Avionic tray and method of making same
US5267656A (en) * 1992-07-10 1993-12-07 Nichols David G Display stand apparatus
US5297684A (en) * 1992-07-24 1994-03-29 Vibrachoc Avionic tray
US20100243312A1 (en) * 2009-03-30 2010-09-30 Lockheed Martin Corporation Equipment container retention and bonding system and method
US8449009B1 (en) * 2006-12-06 2013-05-28 Raytheon Company Adapter for attachment of a display unit to a console of a vehicle
US9297494B1 (en) * 2013-08-28 2016-03-29 The Boeing Company Dagger pin interface apparatus with swivel pin

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US3276112A (en) * 1964-04-06 1966-10-04 Fruehauf Corp Method and apparatus for making integral rivet connections
US3426419A (en) * 1966-10-21 1969-02-11 Plastiglide Ltd Locator plate
US3541395A (en) * 1968-11-15 1970-11-17 Lockheed Aircraft Corp Aviation rack with cooling ducts
US3570554A (en) * 1967-09-12 1971-03-16 Hellermann Gmbh P Method of tieing a bundle of cables

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Publication number Priority date Publication date Assignee Title
US3276112A (en) * 1964-04-06 1966-10-04 Fruehauf Corp Method and apparatus for making integral rivet connections
US3426419A (en) * 1966-10-21 1969-02-11 Plastiglide Ltd Locator plate
US3570554A (en) * 1967-09-12 1971-03-16 Hellermann Gmbh P Method of tieing a bundle of cables
US3541395A (en) * 1968-11-15 1970-11-17 Lockheed Aircraft Corp Aviation rack with cooling ducts

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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