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US4916445A Expired / Lapsed US ⏱️ 0.0 years remaining

Obstruction proximity indication system for an aircraft

Assignee: Individual
•
Filing: 1988-11-09
•
Granted: 1990-04-10
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Expires: 2008-11-09
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Abstract

Abstract Visually observable safe limits for the proximity of an aircraft, such as a helicopter, to obstructions are provided by pairs of lights which provide collimated beams intersecting at limit points located radially outwardly of the arc of the helicopter rotor blades so that light scattered from the intersecting beams at the limit points provides the helicopter pilot with visual references of the rotor arc. Each light of each pair has a concave reflector and a lamp at the focal point of the reflector to provide the collimated beams and transparent plastic shields over the open ends of the reflectors have concavities in central portions to provide diverging beams that illuminate the obstructions.

Inventors

  • 👤 Simon M. Crossley

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 00:17
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/006; B64D; B64D47/00; B64D47/02; B64D47/06

Claims Analysis

Total Claims: 12
Claim 1
Independent Claim 114 words
A system for providing a visual indication of a safe limit of proximity between an aircraft and a stationary object, comprising: a first light source mounted on the fuselage of the aircraft and comprising collimation means for providing a collimated beam of light of a first selected color extending outwardly from the aircraft; and a second light source mounted on the fuselage of the aircraft and comprising collimation means for providing a collimated beam of light of a second selected color extending outwardly from the aircraft to intersect the collimated beam provided by the first light source at a selected proximity limit location outside the volume of space containing all portion of the aircraft.
Claim 2
Independent Claim 114 words
A system for providing a visual indication of a safe limit of proximity between an aircraft and a stationary object, comprising: a first light source mounted on the fuselage of the aircraft and comprising collimation means for providing a collimated beam of light of a first selected color extending outwardly from the aircraft; and a second light source mounted on the fuselage of the aircraft and comprising collimation means for providing a collimated beam of light of a second selected color extending outwardly from the aircraft to intersect the collimated beam provided by the first light source at a selected proximity limit location outside the volume of space containing all portion of the aircraft.
Claim 3
Dependent Claim 45 words
The system of claim 1 comprising a plurality of first light sources and an equal number of second light sources paired with the first light sources to provide a plurality of pairs of collimated light beams intersecting at a plurality of selected proximity limit locations.
Claim 4
Dependent Claim 14 words
The system of claim 2 wherein said first color differs from said second color.
Claim 5
Dependent Claim 109 words
The system of claim 2 wherein the collimation means of each of the first light sources and each of the second light sources comprises: a concave reflector; and a lamp placed at the focal point of the reflector; and wherein each of the first and second light sources further comprises a transparent reflector shield extending over the open end of the reflector, each reflector shield having a concavity formed in a central portion of the surface thereof between the lamp and the proximity limit location selected for the light source to provide a diverging beam of light substantially centered on the proximity limit location selected for the light source.
Claim 6
Dependent Claim 38 words
The system of claim 3 wherein the aircraft is a helicopter and wherein the selected proximity limit locations are on a level with and radially displaced from the path of travel of the rotor blades of the helicopter.
Claim 7
Dependent Claim 109 words
The system of claim 1 wherein the collimation means of each of the first light sources and each of the second light sources comprises: a concave reflector; and a lamp placed at the focal point of the reflector; and wherein each of the first and second light sources further comprises a transparent reflector shield extending over the open end of the reflector, each reflector shield having a concavity formed in a central portion of the surface thereof between the lamp and the proximity limit location selected for the light source to provide a diverging beam of light substantially centered on the proximity limit location selected for the light source.
Claim 8
Dependent Claim 38 words
The system of claim 6 wherein the aircraft is a helicopter and wherein the selected proximity limit location is on a level with and radially displaced from the path of travel of the rotor blades of the helicopter.
Claim 9
Dependent Claim 37 words
The system of claim 1 wherein the aircraft is a helicopter and wherein the selected proximity limit location is on a level with and radially displaced from the path of travel of the rotors of the helicopter.
Claim 10
Dependent Claim 14 words
The system of claim 8 wherein said first color differs from said second color.
Claim 11
Dependent Claim 39 words
The system of claim 1 wherein each of the first and second light sources further comprises means for providing an additional beam of light diverging from the light source along the collimated beam of light from the light source.
Claim 12
Dependent Claim 14 words
The apparatus of claim 10 wherein said first color differs from said second color.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1993-04-09 1993-10-09 1994-04-10 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1997-04-09 1997-10-09 1998-04-10 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2001-04-09 2001-10-09 2002-04-10 $7700.00 Window Closed / Lapsed

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