US20050078475A1 - Protective system for airport runway and taxiway light fixtures - Google Patents
Protective system for airport runway and taxiway light fixtures Download PDFInfo
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- US20050078475A1 US20050078475A1 US10/847,146 US84714604A US2005078475A1 US 20050078475 A1 US20050078475 A1 US 20050078475A1 US 84714604 A US84714604 A US 84714604A US 2005078475 A1 US2005078475 A1 US 2005078475A1
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- Prior art keywords
- mat
- recited
- anchor
- earth
- engagement
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V21/00—Supporting, suspending, or attaching arrangements for lighting devices; Hand grips
- F21V21/08—Devices for easy attachment to any desired place, e.g. clip, clamp, magnet
- F21V21/0824—Ground spikes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
- B64F1/20—Arrangement of optical beacons
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F15/00—Safety arrangements for slowing, redirecting or stopping errant vehicles, e.g. guard posts or bollards; Arrangements for reducing damage to roadside structures due to vehicular impact
- E01F15/02—Continuous barriers extending along roads or between traffic lanes
- E01F15/04—Continuous barriers extending along roads or between traffic lanes essentially made of longitudinal beams or rigid strips supported above ground at spaced points
- E01F15/0461—Supports, e.g. posts
- E01F15/0469—Covers, e.g. of ground surface around the foot
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- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F9/00—Arrangement of road signs or traffic signals; Arrangements for enforcing caution
- E01F9/50—Road surface markings; Kerbs or road edgings, specially adapted for alerting road users
- E01F9/553—Low discrete bodies, e.g. marking blocks, studs or flexible vehicle-striking members
- E01F9/559—Low discrete bodies, e.g. marking blocks, studs or flexible vehicle-striking members illuminated
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V15/00—Protecting lighting devices from damage
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
- F21S8/00—Lighting devices intended for fixed installation
- F21S8/08—Lighting devices intended for fixed installation with a standard
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
- F21W2111/06—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for aircraft runways or the like
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/57—Distinct end coupler
- Y10T403/5741—Separate screw or pin-type connections
Definitions
- This instant invention relates to a system for the protection of airport runway light fixtures, airport signs located on grass or earth, and markers disposed at or near the edge of aircraft runways and taxiways.
- the system more particularly includes a thin flexible mat having an axial opening proportioned to enable placement of a runway light fixture or marker therethrough; and a plurality of peripherally disposed apertures within said mat.
- the system further includes a plurality of anchors for said mat, each of which comprises a planar head, and means for penetration and engagement of earth upon which said mat is positioned. Said penetration and engagement means of each anchor integrally and rigidly depend from a lower surface of said planar head at a central axis thereof.
- planar heads of said anchors each engage said mat when said engagement means have fully penetrated the earth upon which the mal is to he secured.
- the upper surface of the planar head of each anchor comprises an axially disposed nut, Allen head screw or the like proportioned for complemental engagement with the drive element of a power tool to effect rotation of the anchor into the earth.
- FIG. 1 is a perspective view of a single unit of the present inventive system after the same has been fully installed.
- FIG. 2 is a bottom plan view of FIG. 1 .
- FIG. 3 is a side elevational view of the inventive system, showing the salt lip thereof.
- FIG. 4 is a perspective view of an anchoring element employed with the present system.
- FIGS. 5 and 6 are top schematic view showing potential travel paths of edges of airport lawn mowing equipment.
- FIG. 7 is a top schematic view of an elliptical embodiment of the invention, also showing the travel paths of edges of airport mowing equipment.
- FIG. 8 is a perspective view of a further embodiment of the invention.
- FIG. 1 With reference to the perspective view of FIG. 1 , the present system is shown as it appears after the same has been fully installed about an airport runway light fixture.
- a lighting fixture 10 of a type commonly used at airports.
- Such fixtures depend upwardly from a rigid conduit 12 which accommodates electrical cabling from a rigid convex concrete base 14 which is typically circular in structure and extends to periphery 16 shown in FIG. 1 .
- Beneath the protective concrete structure 14 is earth 18 which will extend to the edge of airport runway or taxiway 20 .
- the inventive includes a flexible partially convex mat 22 which includes an axial opening 24 -proportioned to facilitate placement of the light fixture 10 therethrough.
- a plurality of apertures 30 are disposed about or near the periphery of mat 22 , the purpose of which is to enable passage therethrough of a corresponding plurality of anchors 32 which (see also FIG. 4 ) which each include a planar head 34 and a typically spiral means 36 for the penetration and engagement of earth 18 upon which the mat 22 is to be positioned.
- the engagement means is integrally and rigidly dependent from a lower surface of the planar head 34 . Accordingly, mat apertures 30 are proportioned to slidably accommodate the greatest cross-section of the anchors 32 thereby facilitating complemental insertion of the spiral elements thereof through such apertures during the process of installation.
- an anchor consisting of a large diameter head, typically in a range of about 4 to about 8 inches
- the present system when properly installed, will secure mat 22 such that it is immovable under any influence including water, weather, and jet blast. Therein erosion is most difficult and vegetation is unable to grow close enough to fixture 10 to impair the runway illumination function thereof.
- the edges of mowing equipment of a type typically used at airports can safely pass over annular area 28 of the mat 22 , this due to the minimal thickness of the mat which is in a range of 0.15 to 0.50 inches, but preferably 0.375 inches.
- the mat is formed of an elastomeric material preferably a polymeric plastic such as an EPDM polypropylene terpolymer.
- the weight of a mat of the above dimensions made of such material would be about 28 pounds, with a density of 0.68 ounces/cu. inch. and tensile strength of about 650 pounds.
- the present system will not interfere with the normal operation of airport mowing equipment.
- a soft lip 44 the function of which is to contain salt which will melt snow or ice that may fall onto the mat.
- anchor shown in FIG. 4 comprises a spiral structure having a diameter of about two inches and a length of about one foot, that other securement means may be employed within the scope of the present invention as long as a planar head 34 is employed, this for the reasons set forth above.
- an elliptical mat 122 in lieu of the circular mat 22 above described. Typical dimensions thereof would be about 48 inches by 84 inches with a weight of about 50 pounds.
- Such an elliptical mat structure may be advantageously employed in a number of application where, for example, ground surface, visibility, or aesthetic considerations may dictate. For example, extending the length, in even a single axis, of the mat portion of the present system, will enhance ease of mowing and visibility of light fixture 10 from the aircraft runway 20 , even if vegetation or foliage at the edge of the runway is not trimmed for a considerable period of time.
- mat 22 or 122 may be provided with holes for the accommodation of so-called snow poles 48 (set: FIG. 1 ) which arc commonly used at airports in colder climates during much of the year.
- a mat 100 is entirely flat or co-planar, that is, does not include a convex axial portion.
- This embodiment is applicable where a runway light fixture 110 does not utilize a convex support or base.
- slits 114 in the mat are used in lieu of axial opening 24 of mat 22 , described above.
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- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Road Paving Structures (AREA)
- Road Signs Or Road Markings (AREA)
Abstract
A system for the protection of airport runway light fixtures and markers is disposed at or near the edge of aircraft runways, taxiway and airport signs. The system includes a thin flexible mat having an axial opening proportioned to enable placement of a runway light fixture or marker therethrough; and peripherally disposed apertures within the mat. The system further includes several anchors for the mat, each of which comprises a planar head, and means for penetration and engagement of earth upon which the mat is positioned. The penetration and engagement elements of each anchor integrally and rigidly depend from a lower surface of the planar head at a central axis. A greatest transverse cross-section of the engagement element is proportioned for complemental insertion within the peripheral apertures of the convex mat. The planar heads of the anchors each engage the mat when the engagement means have fully penetrated the earth upon which the mat is to be secured. The upper surface of the planar head of each anchor preferably includes an axially disposed nut, Alien head screw or the like proportioned for complemental engagement with the drive element of a power tool to effect rotation of the anchor into the earth.
Description
- This application is a continuation of U.S. application Ser. No. 10/369,494, filed Feb. 21, 2003, which is a continuation-in-part of U.S. application Ser. No. 10/029,923, filed Dec. 31, 2001, now U.S. Pat. No. 6,527,407 B2, which is a continuation of U.S. application Ser. No. 09/638,621, now abandoned, the contents of which are all incorporated herein by reference. This application also claims the benefit of International Application PCT/US02/41585, filed Dec. 26, 2002, the contents of which are incorporated herein by reference.
- Present day airports, of whatever size, make use of numerous, often hundreds, of light fixtures for purposes of illumination of the edge of the airport runway, taxiway and parking areas to thereby minimize the possibility that an aircraft will inadvertently travel off the edge thereof. Such airport light fixtures involve considerable cost, both by way of initial capital investment, accidental breakage and maintenance in that the state-of-the-art runway light fixture is designed to withstand intense vibration and high wind velocity encountered in take-off and landing operations of jet aircraft, as well as bad weather. Such fixtures must, as well, remain operable over a broad range of environmental factors including heat, humidity, erosion, dust, wind, vegetation and insects. Accordingly, each runway light fixture represents a significant, but risk prone, capital asset of the airport. In order to protect this asset and to ensure maximum functionality, extensive use of mowing and other equipment is made to trim and limit the growth of grass and vegetation thereabout. However, such equipment may itself cause damage to runway lights. In many areas, it is also necessary to employ plant poisons and pesticides to protect runway lights from insects and the ingrowth of vegetation. Accordingly, the maintenance of runway lights entails not only the cost labor associated with continual trimming of vegetation but, as well, the potentially hazardous use of herbicides and pesticides to protect the light from vegetation, insects, and other small animals which might otherwise damage the runway lighting.
- The prior art has addressed the above problem through the suggestion of complicated and expensive light fixtures or light fixture protectors and, inter alia, is represented by U.S. Pat. No. 4,104,711 (1978) to Carter, entitled Airport Light Fixture; No. 5,122,798 (1992) to Kaolian, entitled Airport Ground Light Arrangement; No. 5,669,691 (1997) to Barrow, entitled Airport Runway or Taxiway Light Fixture; and No. 5,971,561 (1999) to Fitzwater, entitled Airport Field Light Protector.
- All of the above solutions, while clearly useful in extending the life of airport runway light fixtures, provide no help in the above-described environmental problems associated with extensive groundwork and other maintenance directed to the vegetation which inevitably will try to envelop runway light fixtures. A recognition of such limitations in the prior art is reflected in Kaolian above which suggests the use of a semi-rigid disk shaped body formed of a weather-resistant material which comprises an integral part of the runway fixture per se. Therein, the disk requires excavation of earth and insertion of gravel under the disk. In other words, in systems such as Kaolian and Fitzwater above, a protective rigid or semi-rigid disk is essentially integrated as a part of the airport ground light unit. In such solutions, the outermost edge or periphery of such disk-like elements are susceptible to uplifting under the effect of jet blast, ambient wind, water, and the activity of insects and small animals even if the disk is positioned below ground level. Accordingly, none of the suggestions in the prior art which might, superficially, appear related to the present invention, are practical in terms of such long-term external effects thereupon. In addition, it is essential that any peripheral disk, skirt, or the like associated a runway light be as flat as possible to minimize interference with, or damage to, lower blades of landscaping equipment, the use of which would remain necessary with respect to airport maintenance beyond the periphery of any system for the protection of airport runway light fixtures. It is further noted that the use of gravel to suppress foliage about landing strips has given rise to its own problems; for example, jet blast is capable of dislodging and blowing gravel about a taxiway thereby creating a hazard to other aircraft and to personnel in the area.
- It is, thereby, to be appreciated that prior art attempts to suppress the growth of foliage and to control other factors impacting upon airport ground lights have been relatively ineffective and, as well, have proven costly in terms of manpower, maintenance and particularly the replacement of lights and other components of such ground light systems when damage thereto occurs. The present invention thereby represents an effective alternative to such art as Kaolian and Fitzwater, referenced above.
- This instant invention relates to a system for the protection of airport runway light fixtures, airport signs located on grass or earth, and markers disposed at or near the edge of aircraft runways and taxiways. The system more particularly includes a thin flexible mat having an axial opening proportioned to enable placement of a runway light fixture or marker therethrough; and a plurality of peripherally disposed apertures within said mat. The system further includes a plurality of anchors for said mat, each of which comprises a planar head, and means for penetration and engagement of earth upon which said mat is positioned. Said penetration and engagement means of each anchor integrally and rigidly depend from a lower surface of said planar head at a central axis thereof. Therein a greatest transverse cross-section of said engagement means is proportioned for complemental insertion within said peripheral apertures of the convex mat. Said planar heads of said anchors each engage said mat when said engagement means have fully penetrated the earth upon which the mal is to he secured. In a preferred embodiment, the upper surface of the planar head of each anchor comprises an axially disposed nut, Allen head screw or the like proportioned for complemental engagement with the drive element of a power tool to effect rotation of the anchor into the earth.
- In view of the above, it is an object of the present invention to provide an improved system for (lie protection of airport runway light fixtures from airfield maintenance equipment, this inclusive of a protective mat therefore and method of efficient securement thereof to the area surrounding such runway and taxiway light fixtures.
- It is another object of the invention to provide an airport ground lighting system having improved means for the suppression of foliage and pests thereabout.
- It is a further object to provide a system of the above type which will reduce mowing presently associated with runway lighting and lighting fixtures.
- It is a further object to provide an airport ground light system protection for reduction of soil erosion in the area about the fixture.
- It is a yet further object of the invention to provide a means for the protection of airport runway light fixtures not susceptible to uplift under the influence of jet or propeller airblast.
- It is still another object to provide an improved system to enhance the visibility of runway ground lights.
- It is a still further object of the invention to provide a system for the protection of airport runway lights which will reduce the cost of labor associated with the use of herbicides and pesticides about said lights and will reduce risks to workers otherwise required to walk onto or near the airfield for such tasks.
- It is a yet further object to provide a system of the above type which is fully compatible with all sizes and weights of lawn maintenance equipment and which will pose no risk to such equipment or to an aircraft that may inadvertently travel over such a system.
- It is a still further object of the invention to provide a system of the above type which will, through the use of conventional portable power tools, can be quickly installed or repositioned.
- It is a further object to provide a system of the above type which is essentially immovable after it has been properly secured about a runway light fixture or airport sign and into the earth.
- The above and yet other objects and advantages of the present invention will become apparent from the hereinafter set forth Brief Description of the Drawings, Detailed Description of the Invention and claims appended herewith.
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FIG. 1 is a perspective view of a single unit of the present inventive system after the same has been fully installed. -
FIG. 2 is a bottom plan view ofFIG. 1 . -
FIG. 3 is a side elevational view of the inventive system, showing the salt lip thereof. -
FIG. 4 is a perspective view of an anchoring element employed with the present system. -
FIGS. 5 and 6 are top schematic view showing potential travel paths of edges of airport lawn mowing equipment. -
FIG. 7 is a top schematic view of an elliptical embodiment of the invention, also showing the travel paths of edges of airport mowing equipment. -
FIG. 8 is a perspective view of a further embodiment of the invention. - With reference to the perspective view of
FIG. 1 , the present system is shown as it appears after the same has been fully installed about an airport runway light fixture. Therein may be seen alighting fixture 10 of a type commonly used at airports. Such fixtures depend upwardly from arigid conduit 12 which accommodates electrical cabling from a rigid convex concrete base 14 which is typically circular in structure and extends toperiphery 16 shown inFIG. 1 . Beneath the protective concrete structure 14 isearth 18 which will extend to the edge of airport runway ortaxiway 20. The inventive includes a flexible partiallyconvex mat 22 which includes an axial opening 24-proportioned to facilitate placement of thelight fixture 10 therethrough. - As may be noted in the views of
FIGS. 1 through 3 , the mat comprises acentral convex area 26 and an outer substantially flatannular area 28. Said inner area, which covers the protective base 14 surroundingfixture 10 will typically have a radius in the range of 8 to 16 inches, whileannular area 28 will exhibit a radius in a range of 16 to 32 inches. The total radius ofmat 22 would be about 24 inches. The elevation of convexcentral portion 26 relative to flat annular portion 28 (seeFIG. 3 ) will typically be in a range of 1 to 3 inches depending upon the height of the protective base 14 surroundingfixture 10 and itscable support conduit 12. - As may be noted in
FIG. 2 , a plurality ofapertures 30 are disposed about or near the periphery ofmat 22, the purpose of which is to enable passage therethrough of a corresponding plurality ofanchors 32 which (see alsoFIG. 4 ) which each include aplanar head 34 and a typically spiral means 36 for the penetration and engagement ofearth 18 upon which themat 22 is to be positioned. As may be noted inFIG. 4 , the engagement means is integrally and rigidly dependent from a lower surface of theplanar head 34. Accordingly,mat apertures 30 are proportioned to slidably accommodate the greatest cross-section of theanchors 32 thereby facilitating complemental insertion of the spiral elements thereof through such apertures during the process of installation. This process, it is noted, is considerably facilitated through the provision, upon an upper surface ofplanar head 34, of a protruding element such as a hex or Alien head nut proportioned for complemental engagement with a drive head of a portable power tool to thereby effect rotation of such element and, thusly, of the entire anchor such that each anchor may be quickly inserted into the ground. Such insertion is also facilitated by providing asharp tip 40 at the end of thespiral portion 36 of theanchor 32. It has been found that inexpensive readily available power tools such as a Makita or Black and Decker power drill.Anchor 32 may be easily inserted into earth having a wide range of soil types. - Through the use of an anchor consisting of a large diameter head, typically in a range of about 4 to about 8 inches, the present system, when properly installed, will secure
mat 22 such that it is immovable under any influence including water, weather, and jet blast. Therein erosion is most difficult and vegetation is unable to grow close enough tofixture 10 to impair the runway illumination function thereof. - Further, as may be noted with reference to
FIGS. 5 and 6 , the edges of mowing equipment of a type typically used at airports can safely pass overannular area 28 of themat 22, this due to the minimal thickness of the mat which is in a range of 0.15 to 0.50 inches, but preferably 0.375 inches. In general, the mat is formed of an elastomeric material preferably a polymeric plastic such as an EPDM polypropylene terpolymer. The weight of a mat of the above dimensions made of such material would be about 28 pounds, with a density of 0.68 ounces/cu. inch. and tensile strength of about 650 pounds. Accordingly due to the thinness, strength and flexibility ofmat 22, the present system will not interfere with the normal operation of airport mowing equipment. By the same token, there need not be a concern that the wheels or landing gear of an aircraft, which happens to pass beyond the edge of runway ortaxiway 20, will be interfered with by eithermat 22 or the planar heads 34 of the mat anchors 32. - With reference to
FIG. 3 , there is also shown asoft lip 44, the function of which is to contain salt which will melt snow or ice that may fall onto the mat. - It is to be appreciated that while the anchor shown in
FIG. 4 comprises a spiral structure having a diameter of about two inches and a length of about one foot, that other securement means may be employed within the scope of the present invention as long as aplanar head 34 is employed, this for the reasons set forth above. - In an alternate embodiment of the invention, shown in
FIG. 7 , there may be provided anelliptical mat 122 in lieu of thecircular mat 22 above described. Typical dimensions thereof would be about 48 inches by 84 inches with a weight of about 50 pounds. Such an elliptical mat structure may be advantageously employed in a number of application where, for example, ground surface, visibility, or aesthetic considerations may dictate. For example, extending the length, in even a single axis, of the mat portion of the present system, will enhance ease of mowing and visibility oflight fixture 10 from theaircraft runway 20, even if vegetation or foliage at the edge of the runway is not trimmed for a considerable period of time. Also, resistance to erosion of the earth surrounding lighting fixtures is increased through the use of the elliptical structure ofmat 122. Such a structure, as is also noted inFIG. 7 , is completely compatible with use with lawn mowing equipment and, in certain respects, is more suitable for such use in that the turning radii associated with mower travel along the edge ofmat 122 is much than is the case of the turning radii associated with mower travel along or upon the periphery ofcircular mat 22. In FIGS. 5 to 7, the path of travel of the edge of the moving equipment is indicated by 42 and 142.numbers - It is further noted that
22 or 122 may be provided with holes for the accommodation of so-called snow poles 48 (set:mat FIG. 1 ) which arc commonly used at airports in colder climates during much of the year. - With reference to
FIG. 8 , there is shown a further embodiment of the invention in which a mat 100 is entirely flat or co-planar, that is, does not include a convex axial portion. This embodiment is applicable where arunway light fixture 110 does not utilize a convex support or base. In said embodiment, slits 114 in the mat are used in lieu of axial opening 24 ofmat 22, described above. - While there has been shown and described the preferred embodiment of the instant invention it is to be appreciated that the invention may be embodied otherwise than is herein specifically shown and described and that, within said embodiment, certain changes may be made in the form and arrangement of the parts without departing from the underlying ideas or principles of this invention as set forth in the claims appended herewith.
Claims (20)
1. A system for the protection of airport runway lighting fixtures, the system comprising:
(a) a flexible convex mat including an axial opening proportioned to enable placement of a runway light fixture therethrough, and a plurality of peripherally located apertures;
(b) a plurality of anchors for said mat, each of said anchors comprising a planar head, and means for penetration and engagement of earth upon which said mat is to be positioned, said penetration and engagement means integrally and rigidly depend from a lower surface of said planar head at a center axis thereof, in which a greatest transverse cross-section of said penetration means is proportioned for complemental insertion through said peripheral apertures of said mat,
whereby said heads of said anchors each engage said mat when said penetration means have fully penetrated the earth upon which said mat is to be secured.
2. The system as recited in claim 1 , in which an upper surface of said planar head of said anchor comprises an axially disposed element proportioned for complemental engagement with a drive head of a power tool to thereby effect rotation of said anchor into the earth.
3. The system as recited in claim 2 , in which said penetration means of said anchor comprises an elongate spiral having a pointed tip thereof.
4. The system as recited in claim 3 , in which said spiral of said anchor comprises a diameter of about two inches and a length of about one-foot.
5. The system as recited in claim 2 , in which said planar head of said anchor defines a circle having a diameter in a range of about four to about eight inches.
6. The system as recited in claim 2 , in which said mat defines a circle.
7. The system as recited in claim 2 , in which said convex mat defines an ellipse.
8. The system as recited in claim 1 , in which said mat comprises a convex inner region and an integral outer annular region which is substantially flat.
9. The system as recited in claim 2 , in which said mat includes therein holes for the accommodation of snow poles.
10. The system as recited in claim 8 , in which an upper surface of said planar head of said anchor comprises an axially disposed element proportioned for complemental engagement with a drive means of a power tool to effect rotation of said anchor into the earth.
11. The system as recited in claim 10 , in which said penetration means of said anchor comprises an elongate spiral having a pointed tip thereof,
12. The system as recited in claim 1 , in which said planar head defines a circle having a diameter in a range of about 4 to about 8 inches.
13. The system as recited in claim 2 , in which said mat comprises an inner convex region and an integral annular substantially flat outer region.
14. The system as recited in claim 8 , in which an upper surface of said planar head of said anchor comprises an axially disposed element proportioned for complemental engagement with a drive means of power tool.
15. The system as recited in claim 1 , in which said mat comprises a thickness of between about 0.15 and about 0.50 inches.
16. The system as recited in claim 15 , in which said planar head defines a circle having a diameter in range of about 4 to about 8 inches.
17. The system as recited in claim 16 , in which a radius of said mat comprises a radius in a range of about 18 to about 40 inches.
18. The system as recited in claim 2 in which said mat comprises a convex portion about said axial opening thereof.
19. The system as recited in claim 18 , in which a vertical elevation of said convex portion of said mat comprises a range of between about one and about three inches above the earth.
20. The system as recited in claim 18 , in which a vertical elevation of said mat defines a rectangle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/847,146 US20050078475A1 (en) | 2000-08-15 | 2004-05-17 | Protective system for airport runway and taxiway light fixtures |
Applications Claiming Priority (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US63862100A | 2000-08-15 | 2000-08-15 | |
| US10/029,923 US6527407B2 (en) | 2000-08-15 | 2001-12-31 | Protective system for airport runway and taxiway light fixtures |
| WOPCT/US02/41585 | 2002-12-26 | ||
| PCT/US2002/041585 WO2003057992A1 (en) | 2001-12-31 | 2002-12-26 | Protective system for airport runway and taxiway light fixtures |
| US10/369,494 US20040052071A1 (en) | 2001-12-31 | 2003-02-21 | Protective system for airport runway and taxiway light fixtures |
| US10/847,146 US20050078475A1 (en) | 2000-08-15 | 2004-05-17 | Protective system for airport runway and taxiway light fixtures |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/369,494 Continuation US20040052071A1 (en) | 2000-08-15 | 2003-02-21 | Protective system for airport runway and taxiway light fixtures |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20050078475A1 true US20050078475A1 (en) | 2005-04-14 |
Family
ID=21851584
Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/029,923 Expired - Fee Related US6527407B2 (en) | 2000-08-15 | 2001-12-31 | Protective system for airport runway and taxiway light fixtures |
| US10/369,494 Abandoned US20040052071A1 (en) | 2000-08-15 | 2003-02-21 | Protective system for airport runway and taxiway light fixtures |
| US10/847,146 Abandoned US20050078475A1 (en) | 2000-08-15 | 2004-05-17 | Protective system for airport runway and taxiway light fixtures |
Family Applications Before (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/029,923 Expired - Fee Related US6527407B2 (en) | 2000-08-15 | 2001-12-31 | Protective system for airport runway and taxiway light fixtures |
| US10/369,494 Abandoned US20040052071A1 (en) | 2000-08-15 | 2003-02-21 | Protective system for airport runway and taxiway light fixtures |
Country Status (3)
| Country | Link |
|---|---|
| US (3) | US6527407B2 (en) |
| AU (1) | AU2002364248A1 (en) |
| WO (1) | WO2003057992A1 (en) |
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| US20080034682A1 (en) * | 2006-08-08 | 2008-02-14 | Carpenter Thomas J | Erosion control mat anchor system |
| USD571246S1 (en) * | 2007-02-05 | 2008-06-17 | Jean Yves Belanger | Laser runway lighting device |
| US20090016826A1 (en) * | 2007-07-12 | 2009-01-15 | Carpenter Thomas J | Erosion control system |
| US20090279287A1 (en) * | 2008-05-06 | 2009-11-12 | Honeywell International Inc. | Elevated light with a safety power cut-off switch |
| US20090303084A1 (en) * | 2008-06-10 | 2009-12-10 | Honeywell International | Method and apparatus for providing visible indication of elevated airport light color |
| US20090317190A1 (en) * | 2008-06-18 | 2009-12-24 | Carpenter Thomas J | Shoreline erosion control system |
| US20100080542A1 (en) * | 2008-09-29 | 2010-04-01 | Honeywell International Inc. | Infrared led apparatus and surface heater |
| US20100196102A1 (en) * | 2009-02-05 | 2010-08-05 | Carpenter Thomas J | Anchor system |
| KR101065600B1 (en) * | 2003-08-28 | 2011-09-20 | 가부시키가이샤 한도오따이 에네루기 켄큐쇼 | Thin film transistor, manufacturing method of thin film transistor and manufacturing method of display device |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6527407B2 (en) * | 2000-08-15 | 2003-03-04 | Lyle E. Gluck | Protective system for airport runway and taxiway light fixtures |
| WO2003044283A1 (en) * | 2001-11-20 | 2003-05-30 | Gary Reinert | Segmented foundation installation apparatus and method of installation therefor |
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| CN111981389B (en) * | 2020-08-21 | 2022-06-10 | 深圳安航科技有限公司 | Portable helicopter parking apron emergency navigation aid system |
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| US5308188A (en) * | 1991-06-04 | 1994-05-03 | Shaftner Timothy K | Ramp for temporarily elevated utility access hole |
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| USD442719S1 (en) * | 2000-09-18 | 2001-05-22 | Lyle E. Gluck | Protective unit for airport runway light fixtures |
| US6533446B2 (en) * | 2001-02-16 | 2003-03-18 | Dialight Corporation | Omnidirectional light with protected in-ground light source |
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| US4240766A (en) * | 1979-02-05 | 1980-12-23 | Halsey Dave R | Traffic delineator |
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| US6527407B2 (en) * | 2000-08-15 | 2003-03-04 | Lyle E. Gluck | Protective system for airport runway and taxiway light fixtures |
-
2001
- 2001-12-31 US US10/029,923 patent/US6527407B2/en not_active Expired - Fee Related
-
2002
- 2002-12-26 AU AU2002364248A patent/AU2002364248A1/en not_active Abandoned
- 2002-12-26 WO PCT/US2002/041585 patent/WO2003057992A1/en not_active Ceased
-
2003
- 2003-02-21 US US10/369,494 patent/US20040052071A1/en not_active Abandoned
-
2004
- 2004-05-17 US US10/847,146 patent/US20050078475A1/en not_active Abandoned
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4808025A (en) * | 1987-08-21 | 1989-02-28 | Mcginnis Robert E | Temporary device for use during street repairs |
| US5122798A (en) * | 1990-05-14 | 1992-06-16 | Morgan Kaolian | Airport ground light arrangement |
| US5308188A (en) * | 1991-06-04 | 1994-05-03 | Shaftner Timothy K | Ramp for temporarily elevated utility access hole |
| US5436812A (en) * | 1992-08-27 | 1995-07-25 | Stewart; John C. | Airport marker system |
| US5582477A (en) * | 1995-03-13 | 1996-12-10 | Reinert, Sr.; Gary L. | Finned container bases |
| US5971561A (en) * | 1997-05-09 | 1999-10-26 | Fitzwater; Donald B. | Airport field light protector |
| USD441477S1 (en) * | 2000-09-18 | 2001-05-01 | Stephen J. Byers | Protective unit for airport runway light fixtures |
| USD442719S1 (en) * | 2000-09-18 | 2001-05-22 | Lyle E. Gluck | Protective unit for airport runway light fixtures |
| US6533446B2 (en) * | 2001-02-16 | 2003-03-18 | Dialight Corporation | Omnidirectional light with protected in-ground light source |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101065600B1 (en) * | 2003-08-28 | 2011-09-20 | 가부시키가이샤 한도오따이 에네루기 켄큐쇼 | Thin film transistor, manufacturing method of thin film transistor and manufacturing method of display device |
| US20080034682A1 (en) * | 2006-08-08 | 2008-02-14 | Carpenter Thomas J | Erosion control mat anchor system |
| US7862259B2 (en) | 2006-08-08 | 2011-01-04 | Erosion Tech, Llc | Erosion control mat anchor system |
| USD571246S1 (en) * | 2007-02-05 | 2008-06-17 | Jean Yves Belanger | Laser runway lighting device |
| US7828499B2 (en) * | 2007-07-12 | 2010-11-09 | Erosion Tech, Llc | Erosion control system |
| US20090016826A1 (en) * | 2007-07-12 | 2009-01-15 | Carpenter Thomas J | Erosion control system |
| US20090279287A1 (en) * | 2008-05-06 | 2009-11-12 | Honeywell International Inc. | Elevated light with a safety power cut-off switch |
| US20090303084A1 (en) * | 2008-06-10 | 2009-12-10 | Honeywell International | Method and apparatus for providing visible indication of elevated airport light color |
| US7695219B2 (en) | 2008-06-18 | 2010-04-13 | Erosion Tech, Llc | Shoreline erosion control system |
| US20090317190A1 (en) * | 2008-06-18 | 2009-12-24 | Carpenter Thomas J | Shoreline erosion control system |
| US20100080542A1 (en) * | 2008-09-29 | 2010-04-01 | Honeywell International Inc. | Infrared led apparatus and surface heater |
| US20100196102A1 (en) * | 2009-02-05 | 2010-08-05 | Carpenter Thomas J | Anchor system |
| US8157482B2 (en) | 2009-02-05 | 2012-04-17 | Erosion Tech, Llc | Anchor system |
Also Published As
| Publication number | Publication date |
|---|---|
| US20020054492A1 (en) | 2002-05-09 |
| US6527407B2 (en) | 2003-03-04 |
| AU2002364248A1 (en) | 2003-07-24 |
| US20040052071A1 (en) | 2004-03-18 |
| WO2003057992A1 (en) | 2003-07-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |