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US4288845A Expired / Lapsed US ⏱️ 0.0 years remaining

Aerial refueling receptacle floodlights-spoiler and fuselage, nose mounted

Assignee: United States Department of the Air Force
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Filing: 1979-08-08
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Granted: 1981-09-08
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Expires: 1999-08-08
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Abstract

Abstract A floodlight illumination system, in structural combination with a fuel-receiving aircraft having an aerial refueling receptacle, that permits efficient and effective in-flight night refueling of the aircraft. The illumination system comprises: a selectively lightable, retractable aerodynamically shaped spoiler mounted on the nose of the aircraft which illuminates the top surface of the refueling receptacle, and, two similar (i.e., symmetrically shaped and dimensioned), selectively lightable fairings mounted on the port and starboard sides of the hose of the aircraft, parallel to airflow lines, with one fairing illuminating the port side surface of the refueling receptacle, and with the other fairing illuminating the starboard side surface of the refueling receptacle. The result is adequate and glare-free lighting of the refueling receptacle of the receiving aircraft, which, in turn, allows the operator of the refueling boom of the refueling aircraft to refuel the receiving aircraft without the loss of depth of perception, and without the glare, which ordinarily occur when a receiving aircraft is conventionally illuminated for in-flight night refueling.

Inventors

  • 👤 Wilma L. Finsness
  • 👤 Richard I. McMonagle
  • 👤 Edward M. Sedenquist

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 17:09
CPC Classifications
B; B64; B64D; B64D47/00; B64D47/02

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 397 words
An aerial refueling receptacle floodlight illuminating system for use at night in combination with an aricraft having a longitudinal axis, a fuselage with a nose section having an upper surface and airflow lines along said upper surface, a cockpit windshield aft of said upper surface of said nose section and in alignment with said longitudinal axis, and an aerial refueling receptacle located on said upper surface of said nose section and in alignment with said longitudinal axis, with said receptacle having top and front surfaces, comprising: a. a spoiler floodlight assembly disposed on and in said upper surface of said nose section wherein said assembly includes: (1) an aerodynamically configurated spoiler retractably mounted substantially vertically upward on said upper surface of said nose section, aft of said refueling receptacle and forward of said cockpit windshield, and disposed transverse to said longitudinal axis; (2) a first floodlight means for selectively illuminating said refueling receptacle, with said means disposed partially within said spoiler; (3) and, means for retracting said spoiler into a stowed and longitudinal-like position which is essentially flush with said upper surface of said nose section; b. a first nose fairing floodlight assembly disposed on and in said upper surface of said nose section, wherein said assembly includes: (1) a first blade-like configurated fairing mounted substantially vertically upward on said upper surface of said nose section, forward of said cockpit windshield, adjacent to and port of said refueling receptacle, and parallel to such airflow lines along said upper surface of said nose section; (2) and, a second floodlight means for selectively illuminating said refueling receptacle, with said means disposed partially within said first nose fairing; c. and, a second nose fairing floodlight assembly disposed on and in said upper surface of said nose section, wherein said assembly includes: (1) a second blade-like configurated fairing mounted substantially vertically upward on said upper surface of said nose section, forward of said cockpit windshield, adjacent to and starboard of said refueling receptacle, and parallel to said airflow lines along said upper surface of said nose section; (2) and, a third floodlight means for selectively illuminating said refueling receptacle, with said means disposed partially within said second nose fairing floodlight assembly; whereby, when said first, second and third floodlight means for selectively illuminating said refueling receptacle are activated, said top and side surfaces of said receptacle are adequately illuminated without glare.
Claim 2
Dependent Claim 397 words
An aerial refueling receptacle floodlight illuminating system for use at night in combination with an aricraft having a longitudinal axis, a fuselage with a nose section having an upper surface and airflow lines along said upper surface, a cockpit windshield aft of said upper surface of said nose section and in alignment with said longitudinal axis, and an aerial refueling receptacle located on said upper surface of said nose section and in alignment with said longitudinal axis, with said receptacle having top and front surfaces, comprising: a. a spoiler floodlight assembly disposed on and in said upper surface of said nose section wherein said assembly includes: (1) an aerodynamically configurated spoiler retractably mounted substantially vertically upward on said upper surface of said nose section, aft of said refueling receptacle and forward of said cockpit windshield, and disposed transverse to said longitudinal axis; (2) a first floodlight means for selectively illuminating said refueling receptacle, with said means disposed partially within said spoiler; (3) and, means for retracting said spoiler into a stowed and longitudinal-like position which is essentially flush with said upper surface of said nose section; b. a first nose fairing floodlight assembly disposed on and in said upper surface of said nose section, wherein said assembly includes: (1) a first blade-like configurated fairing mounted substantially vertically upward on said upper surface of said nose section, forward of said cockpit windshield, adjacent to and port of said refueling receptacle, and parallel to such airflow lines along said upper surface of said nose section; (2) and, a second floodlight means for selectively illuminating said refueling receptacle, with said means disposed partially within said first nose fairing; c. and, a second nose fairing floodlight assembly disposed on and in said upper surface of said nose section, wherein said assembly includes: (1) a second blade-like configurated fairing mounted substantially vertically upward on said upper surface of said nose section, forward of said cockpit windshield, adjacent to and starboard of said refueling receptacle, and parallel to said airflow lines along said upper surface of said nose section; (2) and, a third floodlight means for selectively illuminating said refueling receptacle, with said means disposed partially within said second nose fairing floodlight assembly; whereby, when said first, second and third floodlight means for selectively illuminating said refueling receptacle are activated, said top and side surfaces of said receptacle are adequately illuminated without glare.
Claim 3
Dependent Claim 30 words
An aerial refueling receptacle floodlight illuminating system, as set forth in claim 1, wherein said first floodlight means of said spoiler floodlight assembly includes a plurality of floodlight illuminating subassemblies.
Claim 4
Dependent Claim 29 words
An aerial refueling receptacle floodlight illuminating system, as set forth in claim 2, wherein said plurality of floodlight illuminating subassemblies of said spoiler floodlight assembly comprises four such subassemblies.
Claim 5
Dependent Claim 36 words
An aerial refueling receptacle floodlight illuminating system, as set forth in claim 3; wherein said second and third floodlight means of, respectively, said first and second nose fairing floodlight assemblies, each includes one floodlight illuminating subassembly.
Claim 6
Dependent Claim 34 words
An aerial refueling receptacle floodlight illuminating system, as set forth in claim 4, wherein each of said plurality of floodlight illuminating subassemblies of said spoiler floodlight assembly includes a plurality of floodlight illuminating sources.
Claim 7
Dependent Claim 45 words
An aerial refueling receptacle floodlight illuminating system, as set forth in claim 5, wherein said floodlight illuminating subassembly of said first nose fairing floodlight means, and said floodlight illuminating subassembly of said second nose fairing floodlight means, each includes a plurality of floodlight illuminating sources.

References Cited (Backward Citations)

US2663523A Cited
US2849200A Cited
US3108769A Cited
US3285544A Cited
US3917196A Cited
US4095761A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-09-07 1985-03-09 1985-09-08 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-09-07 1989-03-09 1989-09-08 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-09-07 1993-03-09 1993-09-08 $7700.00 Window Closed / Lapsed

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