Aircraft sensor pod assembly

• US 6,745,981 B1
• Filed: 02/25/2003
• Issued: 06/08/2004
• Est. Priority Date: 02/25/2003
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Corporation
• Inventors: Simone, Vito Richard, Fraser, Paul Arthur, Rainer, Stanley Irvin
• Primary Examiner(s): BAREFOOT, GALEN L
• Application Number:
  US10/373,459
• Time in Patent Office: 469 Days
• Field of Search: 244/118.1, 244/137.4, 244/1.R, 244/55, 244/54, 244/139, 244/129.1, 343/705
• US Class Current: 244/118.1
• CPC Class Codes: B64C 1/36 adapted to receive antennas or radomes
• CPC Class Codes: B64D 7/00 Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft dropping bombs or the like B64D1/00; armaments or mountings therefor per se F41
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 3/2605 Array of radiating elements provided with a feedback control over the element weights, e.g. adaptive arrays

Abstract

The invention is a sensor pod for mounting on the top surface of the fuselage of an aircraft. The pod it supported by right and left front supports and right and left rear supports that attach to the fuselage on either side of the longitudinal axis of the aircraft. A fifth structural support, aligned with the longitudinal axis of the aircraft, has a first end attached to the fuselage of the aircraft a second end attached to the sensor pod the aircraft.

Claims

1. A sensor pod assembly for an aircraft, the aircraft having a fuselage with a longitudinal axis, wings, control surfaces and propulsion systems, the sensor pod comprising;

an elongated tubular shaped pod having a longitudinal axis aligned with the longitudinal axis of the aircraft having front and rear ends, said pod positioned above the fuselage of the aircraft;

said pod including;

dish type communication antennas in said front and rear ends of said pod; and

a steered array radar antenna mounted in said middle top portion of said pod, said steered array antenna rotatable about said longitudinal axis of said pod;

first and second front structural supports having first ends coupled to the fuselage of the aircraft on either side of the longitudinal axis thereof and second ends coupled to the front end of said pod;

first and second rear structural supports having first ends coupled to the fuselage of the aircraft on either side of the longitudinal axis thereof and second ends coupled to the rear end of said pod; and

a fifth structural support aligned with the longitudinal axis of the aircraft having a first end attached to the fuselage of the aircraft a second end attached to the sensor pod.

2. The sensor pod assembly as set forth in claim 1 wherein said first end of said fifth structural support is mounted to the fuselage between said front and rear structural supports and extends rearward with said second end attached to said sensor pod between said rear structural supports.

3. The sensor pod assembly as set forth in claim 1 wherein said first end of said fifth structural support is mounted to the fuselage between said front and rear structural supports and extends forward with said second end attached to said sensor pod between said front structural supports.

4. The sensor pod assembly as set forth in claim 1, or 2 or 3 comprising said having an outer skin made at least partially from a material transparent to electromagnetic radiation.

5. The sensor pod assembly as set forth in claim 4 comprising said front and rear ends made of said material.

6. The sensor pod assembly as set forth in claim 5 were in a portion of the top half of said pod is made of said material.

7. The sensor pod assembly as set forth in claim 6 comprising the outer skin of said front and rear ends and the outer skin of at least a portion of the top half of said pod are made of said material.

8. The sensor pod assembly pod as set forth in claim 7 wherein said struts have an aerodynamic shape for reducing drag.