Aircraft deployable rotating phased array antenna

• US 5,357,259 A
• Filed: 08/13/1993
• Issued: 10/18/1994
• Est. Priority Date: 08/13/1993
• Status: Expired due to Term

• Current Assignee: Grumman Aerospace Corporation (Northrop Grumman Corporation)
• Original Assignee: Grumman Aerospace Corporation (Northrop Grumman Corporation)
• Inventors: Nosal, Paul
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/106,874
• Time in Patent Office: 431 Days
• Field of Search: 342/372, 342/398, 343/757, 343/763, 343/766, 343/705
• US Class Current: 342/398
• CPC Class Codes: G01S 7/032 Constructional details for solid-state radar subsystems
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 3/04 for varying one co-ordinate of the orientation

Abstract

A stacked Yagi phased array is located within a foil-shaped enclosure that is connected to a rotary joint which allows rotation of the antenna over 360° in azimuth. The radar is normally stored within the equipment bay of an aircraft and is deployed therefrom when radar surveillance by the aircraft is desired. When the antenna is stored, aircraft drag is reduced and radar signature is low. The combination of mechanical and electronic scan permits increased search in critical sectors of interest and allows skipping of other sectors. The rotary joint of the invention requires no RF power or analog signals to pass through it.

Claims

1. An aircraft surveillance antenna comprising:

a foil-shaped enclosure deployable from within a fuselage of an aircraft;

a plurality of phased array antenna elements located in the enclosure;

a drive shaft connected at a first end to the enclosure and at another end to the aircraft for selectively rotating the enclosure 360°

; and

a rotary joint disposed along the drive shaft for coupling therethrough

electrical power and control signals to the antenna elements; and

received signals from the antenna elements;

the antenna being capable of simultaneous mechanical rotation and electronic radar scan.

2. The antenna set forth in claim 1 wherein the phased array comprises a plurality of Yagi elements.

3. The antenna set forth in claim 1 together with a plurality of transmit/receive modules located within the enclosure and respectively mounted rearwardly of each element of the array.

4. The antenna set forth in claim 2 wherein the Yagi elements are arranged in a double stacked configuration within the enclosure.

5. An aircraft surveillance antenna comprising:

a foil-shaped enclosure deployable from within a fuselage of an aircraft;

a plurality of phased array Yagi antenna elements located in the enclosure;

a plurality of transmit/receive modules located within the enclosure and respectively mounted rearwardly of each element of the array;

a drive shaft connected at a first end to the enclosure and at another end to the aircraft for selectively rotating the enclosure 360°

;

a rotary joint disposed along the drive shaft and including

slip rings for coupling external power to the modules;

first fiber optic means for coupling control signals to a signal generator located inside the enclosure; and

second fiber optic means for coupling received signal from the modules to an external utilization device;

the antenna being capable of simultaneous mechanical rotation and electronic radar scan.

6. The antenna set forth in claim 5 wherein the rotary joint further comprises a means for coupling external cooling fluid to the interior of the enclosure for cooling the modules located therein.