BACKGROUND OF THE INVENTION
1. Field of the invention
[0001] The present invention relates to wiring installations and more particularly to wiring
installations in aircraft electronics bays, main instrument panels or overhead panels
which require extremely complex wiring of multiple systems.
2. Description of the Prior Art
[0002] In the patent literature U.S. patent No. 4,583,215 to Hargrave, et al, shows a telephone
line access system for main distribution frame that employs access blocks comprising
sockets and pins for coupling two rows of lightning protectors. One or more integrated
circuit modules are attached to each access block and these may be readily affixed
to and disconnected from a main distribution frame.
[0003] U.S. patent No. 4,320,261 to Scerbo, et al, shows a method for optimizing cable routing
in the distribution panels for an office environment. Means are described for minimizing
crossovers and cable lengths. Optimization is based on crossovers and length in contrast
to the present method which considers separation requirements. Also Scerbo, et al,
is hardwired in contrast to the present method of using connectors.
[0004] U.S. patent No. 4,972,298 to Casa, et al, is illustrative of high density circuit
computer assemblies, while U.S. patent No. 2,098,321 to Treptow is illustrative of
distributing frames in telephone systems.
[0005] The problems of wiring separation, congestion, integration, routing, cross-connected
wire bundles, disconnects in aircraft installations have been tolerated and accepted
without solution, the traditional method of complex wiring of multiple systems being
to hand wire from a connector at the peripheral device to another at e.g., an overhead
panel or directly into the overhead panel. There has been no consistent system for
achieving wire separation, avoiding cross-connects or minimizing connections or any
attempts made to solve the congestion problem during aircraft final assembly.
SUMMARY OF THE INVENTION
[0006] This invention employs a plural-level system to achieve simplicity. Each panel is
analyzed to assign wire separation categories for every required connection and then
one or more connectors (designated separation dedicated connectors) is incorporated
for each category. The opposite end of the system is composed of a set of "integration
disconnects". The connections on these are determined by performing a wire separation
category analysis on the wires coming into the instrument bay from the peripherals
in a given physical area (called a destination area) and assigning at least one connector
for each category. The third portion of the system is composed of the "integration
wire bundles". These are designed with breakouts from the bundle body so that they
connect the proper terminals of the dedicated separation connectors to the proper
terminals of the integration disconnects. In addition to the above advantages, the
present invention importantly practically eliminates the need for doing hand wiring
at final assembly. The features, objects and advantages of the present invention will
be apparent hereinafter from a detailed description of the invention and the appended
claims taken in conjunction with the attached drawing of a preferred embodiment.
BRIEF DESCRIPTION OF THE DRAWINGS
[0007]
Figure 1 is a schematic block diagram of the present basic plural level wiring interface;
Figure 2A is an exemplary overlay of a present system wiring interface layout for
an overhead panel;
Figures 2B and 2C are taken together on an enlarged view of the system of Figure 2A;
and
Figures 3A and 3B are an exemplary representation of a typical bundle.
Figures 4A and 4B show examples of Integration Disconnects with and without wiring.
DETAILED DESCRIPTION
[0008] Initially upon reviewing the aircraft overhead panel or electronics bay of an aircraft,
and due to its inherent wire congestion, complexity, and separation problems, efforts
towards a solution of the problem have generally not been attempted or abandoned.
The present invention however solves the separation problem by utilizing separation
dedicated connectors. Using this method a wire is inserted into the connector meeting
the wires separation requirement; should multiple connectors meet the wire's separation
requirement, the wire is inserted into the connector also meeting the wire's destination
requirements, thereby providing a solution to the separation routing congestion, cross-connected
wire bundles, and complexity problems. A wiring matrix results in simplified discrete
integrated wire bundles which are assembled and positioned on the module or overhead
panel before final assembly thereby completing a module or panel and wiring assembly.
Routing integration previously achieved by end point aircraft final assembly wiring
with complex integration wiring panels is eliminated in accordance with the present
plural level wiring interface hereinafter described utilization which is
a system utilizing separation dedicated connectors, integration disconnects (having no wiring, Ref.
Fig. 4A and 4B), Ref. Fig. 1 and 2, modular integrated wire bundles and panels, destination
dedicated connectors, and wire bundle breakouts from the bundle body (Ref. Fig. 1,
3A and 3B. The present system permits wire bundle production on foam boards including
connectors and wiring as integral unitary modules.
[0009] Concern has been expressed with regard to the problem of cross-connected wire bundles
at a connector (wiring more than one wire bundle to a single connector). This concern
is expressed primarily due to production, installation and separation problems. The
cross-connection problem is herein solved by the utilization of separation dedicated
connectors on modules and panels.
[0010] Turning now to Figure 1, a plural level wiring interface system is shown in which
the following symbols are representative of the interface components:
MP1,MP2,MP3 are modules or panels
ID1,ID2,ID3 are integration disconnects
IB1,IB2,IB3 are integration wire bundles
DB1,DB2,DB3 are distribution wire bundles
D1,D2,D3,D4,D5 are destination devices
E1,E2 are assemblies
A,B,C,N are dedicated separation categories at connectors
1,2,3,4,5,6,7,8,9,10 are connectors
[0011] In the following, the method by which wiring interfaces are defined and developed
will be described:
[0012] As shown in Figure 1; starting with the most complex module or panel integration
assembly, the separation categories in the module or panel are determined; A,B,C,
and N for example, where N is a neutral or non-critical separation; and for example
Separation A is routed on the left side, B is routed on the right side, and C is redundant
to A and/or B and routed away from A and B. The module or panel is assigned a connector
for each separation category in the module or panel.
[0013] As shown in Figure 1; MP2 is assigned separation connectors A,B,C; MP3 is assigned
separation connectors B, & C; and MP1 is assigned separation connector A/N (since
separation category N may be combined with any other separation category). The internal
wiring of the modules or panels are separation routed and connected to the separation
dedicated connectors of the module or panel interface. Integration wire bundles IB1,
IB2, IB3 are used to route wires of similar separation from the module or panel separation
dedicated connector interface to an integration disconnect ID1 via breakouts from
the bundle body. Wires from separation dedicated connectors; A of MP2 and A/N of MP1
are combined into IB1; B of MP2 and MP3 are combined into IB2; and C of MP2 and MP3
are combined into IB3. Integration wire bundles IB1, IB2, and IB3 are kept separate
from each other and routed to an integration disconnect ID1. (Thus a failure in one
bundle will not affect the wiring in another bundle.). This integration disconnect
is close to or part of the module or panel assembly E1. The integration disconnect
provides a disconnect for the assembly E1 as well as an integration interface to the
distribution wire bundles. IB1 mates with connector 1 (separation dedicated A/N) and
connector 2 (separation dedicated N); [Note: The integration disconnect connector
2 is
used to route a portion of the separation N wires based on destination, and eliminates
the need for wiring at the integration disconnect to enter another distribution wire
bundle, Ref. Fig. 4A and 4B]. IB2 mates directly with DB2 and provides a disconnect
function at connector 3. IB3 mates with connectors 4 and 5 to accommodate the volume
of wires and provide the disconnect function. The distribution wire bundles are used
to make long runs with breakouts from the bundle body (Ref. Fig. 1) to other integration
or destination areas. DB1 routes separation category A wires direct from ID1 to ID2;
(integration disconnect, ID2, is shown being used as a production break interface).
DB2 routes separation category B wires to both ID2 and ID3 (ID3 being shown as an
integration disconnect interface on an enclosed assembly E2). DB3 accepts separation
category N wires from IB1 for routing to destination device D5 having a single C/N
separation dedicated connector; DB3 also has routing breakouts from the bundle body
(Ref. Fig. 1) for separation category C wiring to ID2 and ID3.
[0014] Turning now to Figure 2A there is seen a plural level wiring interface of the kind
shown in Figure 1 however as adapted for an overhead panel. Only the elements of the
present system are shown in heavy lines.
[0015] Referring to Figure 2A, and enlarged in Figures 2B and 2C, giving details the following
symbols are representative of the interface components:
MP1 thru MP23 are modules
ID1A and ID1B are integration disconnects
IB1 thru IB5 are integration wire bundles
DB1 thru DB7 are distribution wire bundles
E1 is a panel assembly
A thru G are dedicated separation categories at connectors
1 thru 19 are connectors.
[0016] Separation categories D and E represent (in air/in space/at sea) and (on ground/at
port) usage respectively, exclusive usage allows the combining of these wires into
a single connector.
[0017] Separation categories F and G are redundant to categories A and B, and may be combined
(provided they have protective shielding from A and B) to the first distribution breakout.
[0018] Figure 2A (and 2B and 2C) is a detail of a complex panel, thus destination devices
are not shown.
[0019] Modules MP22 and MP23 interface with both integration and distribution wire bundles.
[0020] Connectors (1,2,3), (4,5,6), and (10,11,12) are provided to handle the volume of
wires.
[0021] Connectors 8 and 9 on integration disconnect ID1A are provided to separate and distribute
separation category D and E wires.
[0022] Connectors 7 and 13 on integration disconnects ID1A and ID1B are provided to separate
and distribute separation category A and B from F and G.
[0023] Connectors 1 thru 19 also provide a panel disconnect function.
[0024] It will be further understood that the plural level wiring interface arrangements
and methods herein described is not limited to the specific embodiment disclosed by
way of illustration, but may assume other embodiments limited only by the scope of
the appended claims.
DEFINITIONS
[0025]
Separation Dedicated - Routing necessary for isolation of critical circuits to provide safety, dependability
and the redundancy to prevent hazardous malfunction or simultaneous loss of equipment
functions or propagation of a malfunction or failure.
Integration Disconnect - Anything that provides a method of mating one or more contacts or connectors with
the function or purpose of providing integration, combining or distributing, multiple
bundles without wiring between mating bundle contacts or connectors.
Bundle Body - the main portion (structure) or collective group of physical elements comprising
the bundle.
Breakout - Elements comprising the bundle which exit or enter the bundle body