Aircraft multi-communications system

• US 3,999,015 A
• Filed: 05/27/1975
• Issued: 12/21/1976
• Est. Priority Date: 05/27/1975
• Status: Expired due to Term

• Current Assignee: Genie Electronics Co., Inc.
• Original Assignee: Genie Electronics Co., Inc.
• Inventors: Paules, Eugene H., Snyder, Dennis G.
• Primary Examiner(s): Claffy, Kathleen H.
• Assistant Examiner(s): Kemeny, E. S. Matt
• Application Number:
  US05/581,024
• Time in Patent Office: 574 Days
• Field of Search: 179/1 VE, 179/1 VC, 179/1 H, 179/100.1, 340/22, 340/74, 340/27, 340/416
• US Class Current: 379/171
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: H04M 11/00 Telephonic communication systems specially adapted for combination with other electrical systems

Abstract

An aircraft communication system adapted to provide a plurality of communication paths from respective inputs to a plurality of outputs, the communication paths being flexible in arrangement and operator control. For use in an aircraft, the system combines an intercom for voice transmission between pilot, co-pilot and passengers, along with channels for external radio reception and transmission by pilot and co-pilot. The system also provides enabling of transducer outputs only upon detection of input signals above a given threshold, and automatic monitoring of aircraft supply voltage conditions with visual and audio outputs. Specific features of the invention include: (a) audio source input circuits feed a common point which is connected to a threshold VOX switch circuit; (b) the VOX switch circuit controls a recorder, additional audio inputs, and a master amplifier circuit inputted from the common point and connectable to output transducers, whereby signals from the audio sources are outputted only when the common point signal exceeds the predetermined threshold; and (c) the audio source input circuits include aircraft power supply high and low detection circuitry.

Claims

1. Communications apparatus for use in an aircraft, comprising:

a. a plurality of input paths, adapted to receive respective electrical input signals, said input paths having outputs connected at a common connection point;

b. threshold sensing means, connected to said common connection, for sensing when the signal at said common connection point is above a predetermined threshold level;

c. a common amplifier path, having an input connected to said common connection point, and including threshold switching means operatively responsive to said threshold sensing means, said path having an output at which is delivered an amplified signal representative of the signal provided at said common connection point as a function of the operation of said threshold sensing means;

d. a plurality of output transducers;

e. transducer switching means, connected to said amplifier output, for switchably connecting said output to respective ones of said output transducers; and

f. secondary switching means, including a switch responsive to said threshold switching means, and connected to said amplifier output, for switchably connecting secondary audio sources to said output transducers through said transducer switching means.

2. The communications apparatus as described in claim 1, comprising aircraft supply voltage processing means, having an input adapted to be connected to the aircraft voltage supply, for generating signals representative of the state of said aircraft supply voltage, and having an output at which said representative signal appears, which output is connected to said common connection point.

3. The apparatus as described in claim 2, wherein said threshold sensing means comprises amplifier means for amplifying the signal appearing at said common connection point, and a relay circuit driven by the output of said amplifier means, which relay circuit has a plurality of contacts which change positions as a function of the strength of the signal at said common connection point relative to said predetermined threshold.

4. The apparatus as described in claim 3, wherein said amplifier path contains normally open contacts which are controlled by said relay, said amplifier path further comprising a switch across said contacts to provide operator control over the effect of said threshold sensing means on said amplifier path.

5. The apparatus as described in claim 4, wherein said aircraft supply processing means comprises high voltage amplifier means for providing a signal when said aircraft supply exceeds a predetermined high voltage level, and low voltage amplifier means for providing an output signal when said aircraft supply voltage is below a predetermined voltage level.

6. The apparatus as described in claim 5, wherein said voltage processing means comprises a time delay circuit, said time delay circuit having inputs connected to said high voltage amplifier means and low voltage amplifier means respectively, said voltage processing means also including an audio generator driven by said time delay means, for providing an audio output signal upon the occurrence of an aircraft supply voltage exceeding either said predetermined high voltage or said predetermined low voltage for a predetermined time period.

7. The apparatus as described in claim 1, comprising at least two microphones connected to respective ones of said input paths, and further comprising transmit amplifiers connected to respective ones of said at least two microphones for amplifying said microphone output signals.

8. The apparatus as described in claim 7, comprising at least two switches corresponding to said at least two microphones, said switches being manually operable, and enabling means connected between respective corresponding switches and transmit amplifiers for enabling operation of said transmit amplifiers as a function of the operation of said switches.

9. The communication apparatus as described in claim 1, having means for automatic flight recording connected to said common connection point.

10. Communications apparatus for use in an aircraft, comprising:

a. a plurality of input paths, adapted to receive respective electrical input signals, said input paths having outputs connected at a common connection point and each having a mixer element with the output of said each mixer connected to said common point;

b. common threshold sensing means connected to said common connection point, for sensing when the signal at said common connection point is above a predetermined threshold level;

c. a master amplifier path having an input connected to said common connection point and including threshold switching means operatively responsive to said threshold sensing means, said threshold switching means including a two state element whereby signal transmission through said master path is passed when said element is in a first state and blocked when said element is in a second state, said path having an output at which is delivered, when said element permits signal passage, an amplified signal representative of the signal at said common connection point;

d. a plurality of output transducers;

e. transducer switching means, connected to said master amplifier path output, for switchably connecting said output to respective ones of said output transducers;

f. secondary switching means, including a switch responsive to said threshold switching means, and connected to said amplifier output, for switchably connecting secondary audio sources to said output transducers through said transducer switching means; and

g. aircraft supply voltage processing means, for generating signals representative of the state of said aircraft supply voltage, said processing means having threshold means for producing a signal in excess of the threshold level of said common threshold sensing means when the aircraft supply is not within a predetermined range.