The foregoing summary, as well as the following detailed analyses of the physical principals and detailed description of the preferred embodiment will all be better understood when read in conjunction with the appended drawings. For the purpose of illustrating the invention, particular arrangements and methodologies are shown in the drawings. It should be understood, however, that the invention is not limited to the precise arrangements shown or the methodologies of the detailed description. In the drawings:
Certain terminology is used in the following description for convenience only and is not limiting. The words “right,” “left,” “lower” and “upper” designate directions in the drawings to which reference is made. The words “inwardly” and “outwardly” refer to directions toward and away from, respectively, the geometric center of the self powered, self hoisting elevator apparatus and designated parts thereof. Unless specifically set forth herein, the terms “a”, “an” and “the” are not limited to one element but instead should be read as meaning “at least one”. The terminology includes the words noted above, derivatives thereof and words of similar import.
Referring now to the drawings, wherein the same reference numerals are used to designate the same structural features throughout the several figures there is shown a preferred embodiment of the present invention used for lifting firefighting equipment to high floors in a building. It will be appreciated that the present invention is capable of being used in other applications. For example, an embodiment of the present invention may be used for lifting materials and tools to a high floor of a building being constructed in a situation where a conventional construction elevator cannot be used.
The present invention, when used for the aforementioned fire equipment ferrying application, comprises a pre-stored passive descent unit 1 comprising a housing 1a and other parts hereinafter described which are preferably supported by the descent unit housing 1a when the descent unit 1 reaches the ground or other lower supporting surface and which convert the descent unit 1 to a self powered, self hoisting elevator apparatus 6 or ascent/descent system. One or more such descent units 1 can be pre-stored on one or more and preferably each upper floor of a high rise building 10. Alternatively completely assembled elevator apparatuses 6 may be stored on one or more upper floors of a building 10. As a further alternative, a completely assembled elevator apparatus 6 is stored at or near the ground or other supporting surface or is transported to the building 10 from some other location. Then, the free end of the elevator apparatus cable 14 is raised to the origin using a rope or some other device and is secured to a fixed anchorage as described below.
With the preferred embodiment, when a fire breaks out on an upper floor 10a of the building 10, responsible personnel in the building 10 or arriving firefighters go to the floor below the fire floor 10b (referred to as an origin) and affix the free end 14a of a cable 14 of a pre-stored descent unit 1 to a fixed anchorage such as an available structural column 10c using an attachment device such as a carabiner 11 which has been secured to the free end 14a of the cable 14. Although a carabiner 11 is used in the present embodiment it will be appreciated by those skilled in the art that any other suitable attachment device such as a hook, a snap hook or the like could alternatively be used. Additionally, although in the present embodiment the free end of the cable 14a is secured to a building column 10c it will be apparent to those skilled in the art that any other available fixed anchorage may alternatively be used. The responsible personnel or firefighters would then open or break a building window if necessary and start the descent unit 1 descending toward the ground or other lower supporting surface (See
Once the descent unit 1 initially reaches the ground or other lower supporting surface, other personnel or firefighters attach a motor 2, a power source, such as a battery pack 3, a controller such as a wireless remote controller 4 which interconnects the motor 2 and the battery pack 3 and an object receiving cargo bin 5 to the descent unit housing 1a to complete the elevator apparatus or ascent/descent system 6 (See
In the preferred embodiment, the cargo bin 5 is comprised of four substantially identical vertical side panels 51 and a base panel 52 which are attached together and are attached to a top panel 53 which is also attached to the descent unit housing 1a. In the present embodiment the components of the cargo bin 5 are made of a light weight, high strength material such as Lexan®. Other materials may alternatively be used. In the present embodiment the side panels 51 each include one or more bottom lips 51a each of which is inserted into corresponding slots or grooves 52a in the bottom panel 52. The side panels 51 are also each latched to the bottom panel 52 using suitable latching mechanisms such as wing nuts 60. Similar lips 51b along the tops of the side panels 51 are inserted into corresponding slots or grooves 53a in the top panel 53. The side panels 51 are also latched to the top panel 53 using suitable latching mechanisms such as wing nuts 60. In this manner the cargo bin 5 is securely held together. It will be appreciated that the cargo bin 5 may be held together in some other manner such as using snap or detent connections or the like. Alternatively, the components of the cargo bin 5 may be permanently secured together such as by the use of an adhesive, welding or the like. The assembled cargo bin 5 is preferably attached to the descent housing 1a using suitable latching mechanisms such as wing nuts 60 or in any other suitable manner. Preferably the side panels 51 each include windows 51c which may slide open/closed with respect to the cargo bin 5 to facilitate installation/removal of the cargo from any of the sides of the cargo bin 5 which may face a building window opening.
When the cargo bin 5 is assembled and attached to the descent unit housing 1a the cargo bin 6 may be loaded with objects such as air tanks, hose sections, and other vital firefighting equipment to be lifted upwardly. Using a wireless transmitter/controller 7 which is in wireless contact with the wireless controller 4, the motor 2 is activated thereby rotating the cable spool 13 in the second direction to rewind the cable 14 and raise the elevator apparatus 6 (See
The descent unit 1 of the preferred embodiment of present invention is based upon the apparatus for the safe, slow descent of a person from a multistory building as described in U.S. Pat. No. 6,962,235 entitled “Apparatus for the Exterior Evacuation from Buildings”, the entire subject matter of which is hereby incorporated herein by reference. The descent unit 1 of the preferred embodiment utilizes essentially the same energy dissipating mechanism as used in the described preferred embodiment of U.S. Pat. No. 6,962,235 albeit with some of the component parts arranged differently, to accomplish the controlled slow descent, and it employs at least some of the same safety features.
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The cable spool 13 in the preferred embodiment is initially wound with a full compliment of high strength cable 14, preferably made of steel wire rope, which is sufficiently long to reach from the installation floor 10b or origin down to the ground or other lower supporting surface, taking into account the maximum attachment length to the anchor column 10c on the installation floor, and any slant heights that result from any building setbacks or other potential obstructions. The cable spool 13 which is supported for rotation within the descent housing 1a mechanically connects to a large spur gear 15 through a clutch mechanism (not shown) which is designed to slip whenever the torque exceeds a preset limit, corresponding to when the cable force exceeds a preset safety limit of, for example, 650 lbs when the cable spool 13 contains its full allotment of cable 14, thereby limiting the force resulting from any initial free-fall of the descent unit 1 or elevator apparatus 6. The large spur gear 15 meshes with a smaller spur gear 16 located on an intermediate shaft 16a and a larger spur gear 17 on the intermediate shaft 16a in turn meshes with another smaller spur gear 18 located on a third shaft 18a which contains a high speed air impeller 19. The two gear meshes result in a total rotational speed multiplication of approximately 30, and thus the rotational speed of the air impeller 19 will be approximately 30 times the rotational speed of the cable spool 13. According the teachings of U.S. Pat. No. 6,962,235, it is the geared-up high speed of the air impeller 19 in conjunction with the slow play-out of the cable 14 from the cable spool 13 that efficiently dissipates the energy from the descent of the descent unit 1 or the elevator apparatus 6 and results in a slow descent speed. Calculations show that if the cable spool 13 has an average wound cable diameter of about 7.5 inches, and with the above described speed multiple of 30 for the air impeller 19, then an air impeller 19 of a similar diameter can be fashioned to rotate at about 900 RPM and keep the descent speed of a 400 pound total weight (maximum load) to an average of about 2 feet per second. And if the total weight were to be only 100 pounds (unloaded, for instance), the average descent speed would not decrease fourfold, but only twofold to about 1 foot per second. If desired some other gear arrangement or other transmission mechanism may be used to operatively connect the cable spool 13 to the air impeller 19. Further, in an alternate embodiment the energy dissipating mechanism may comprise a device other than the air impeller 19.
The above parameters may be used to form the basis of the design of a practical elevator apparatus 6, with the descent unit 1 containing an average amount of cable 14, the motor 2, controller 4 and battery pack 3, and empty cargo bin 5 would weigh about 100 pounds. Thus when the cargo bin 4 is loaded with about 300 pounds of cargo, the entire assembly would weigh about 400 pounds. The empty elevator apparatus 6 would descend at an average speed of about one foot per second, and fully loaded the elevator apparatus 6 would descend at an average speed of about two feet per second. Thus, if the battery-pack 3 should happen to run out of energy or otherwise fail while the fully loaded elevator apparatus 6 is ascending, the loaded elevator apparatus 6 would simply descend at the still-very-slow and safe speed of about two feet per second. Therefore, the present invention it considered to be failsafe.
With a fully charged battery pack 3, an electric motor 2 turning the air impeller shaft 18a in the reverse direction at 1,620 RPM would drive the elevator apparatus 6 upwardly at an average speed of about 1.8 feet per second. When the elevator apparatus 6 is loaded with 300 pounds of material, making its total weight about 400 pounds, achieving this climbing speed will require about 900 watts of power, which is equivalent to about 1.2 horsepower. A relatively small size motor that can satisfy this requirement is the Kollmorgen Servo-Disc motor, Model U16M4H which measures 7.4″ diameter×3″ long and weighs 18.7 pounds. With air cooling (from the impeller 19), this motor can achieve the required speed and torque, drawing about 12 amps with about 90 VDC input.
The battery-pack 3 must supply sufficient voltage and current for the operation of the motor 2. A model PA3383U-1BRS lithium ion 12 cell laptop computer battery can supply up to 6 amps at 14.8 volts. The ascent requirement specified above might necessitate using twelve (12) such 14.8 volt rechargeable batteries, six-in-series in parallel with another six-in-series, to supply up to 12 amps at about 89 volts. Each laptop battery is able store up to 6.45 ampH, so it can supply the necessary 6 amps for at least an hour, or 3,600 seconds. At 1.8 feet per second, 3,600 seconds is equivalent to 6,480 feet, and since the typical building story is between 9 feet and 14 feet (12.5 feet average), the fully loaded elevator apparatus 6 should be able to ascend at least 500 average stories using twelve of the laptop batteries wired as described above to make up the required ascent battery pack 3. Each of the laptop batteries is 10.75″×2.9″×1.05″ and weighs 1.4 lbs, so the ascent battery pack 3 comprising twelve such batteries would measure 10.75″×2.9″×12.6″ and weigh about 16.8 pounds.
All of the above could alternatively be achieved with a less expensive golf cart motor such as the Cushman CZ383, and sealed glass mat 12 volt batteries, but these components would be much larger and weigh more than the 35.5 pounds total for the components described in the previous paragraphs.
The preferred embodiment preferable employs as the cable 14 0.125 inch diameter 7×19 configuration galvanized aircraft cable which has a minimum breaking strength of 2,000 pounds and weighs about 2.9 lbs per hundred feet. Thus, thirty stories worth of cable would be about 375 feet long and would weigh about 10.9 pounds. Fifty stories worth of cable would be about 625 feet long and would weigh about 18.1 pounds. Seventy stories worth of cable would be about 875 feet long and would weigh about 25.4 pounds. Ninety stories worth of cable would be about 1,125 feet long and would weigh about 36.2 pounds. One-hundred-ten stories worth of cable would be about 1,375 feet long and would about weigh 40 pounds. Therefore, for most embodiments the initial cable weight will be 25±15 pounds, and since the played-out cable 14 will be no longer descending, the total descending weight will decrease as the elevator apparatus 6 descends along the side of the building 10.
As indicated previously, if the battery pack 3 should run out of power while a fully loaded elevator apparatus 6 is ascending, the elevator apparatus 6 will simply descend at a low speed back to the ground or other lower supporting surface in a failsafe manner. There the drained battery pack 3 can be quickly and conveniently replaced with a fully charged, fresh battery pack 3 and the ascents and descents of the elevator apparatus 6 can be resumed. If there is a building setback located below where the battery pack 3 runs out of power, the choices are to: 1) empty the cargo bin 5 and drag the elevator apparatus 6 to the edge and over to permit it to descend to the ground or other lower supporting surface to receive a fresh battery pack 3, 2) try to a accomplish the same result without emptying the bin 5, or 3) carry a fresh replacement battery pack 3 along with the cargo at all times so the battery pack 3 can be replaced on the setback. The third option should be considered the preferred option whenever there is a building setback along the route of the elevator apparatus 6.
The wireless transmitter/controller 7 used to control the elevator apparatus 6 may be a very simple device not substantially different than the inexpensive controllers model airplane flyers use to control model planes in flight. Control functions preferable include: motor on/motor off, brake on/brake off. Multiple control options exist as follows: 1) use of a single wireless transmitter/controller 7 on the ground, 2) use of two wireless transmitter/controllers 7, one on the ground and one up at the origin or staging floor, so that the closest controller (strongest signal) takes precedence, 3) use of multiple wireless transmitter/controllers 7 one on the ground, one up at the origin or staging floor, and one on each building setback, where again the closest wireless transmitter/controller 7 takes precedence.
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Although the preferred embodiment of the failsafe self-powered self-hoisting multi-trip anchored elevator apparatus has been described and specified in significant detail for the fire equipment ferrying application, alternate arrangements and other applications still within the scope of the present invention are feasible. It will also be appreciated by those skilled in the art that alternate uses may be found that differ from the proposed use, and changes or modifications could be made to the above-described embodiment without departing from the broad inventive concepts of the invention. Therefore it should be appreciated that the present invention is not limited to the particular use or particular embodiments disclosed but is intended to cover all uses and all embodiments within the scope or spirit of the described invention as defined by the appended claims.
This application claims priority from U.S. Provisional Patent Application No. 60/849,706 filed Oct. 5, 2006 and entitled “Failsafe Battery-Powered Self-Hoisting Multi-Trip Anchored Cargo Elevator,” the subject matter of which is hereby incorporated herein by reference.
Number | Date | Country | |
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60849706 | Oct 2006 | US |