Air ceiling inlet unit

Abstract

A ceiling inlet unit that assists in bringing air into the interior room of a building. The unit has a housing providing an opening to the attic of the building, the housing having movable blades with brush borders on the ends, pivotally mounted with a continuous hinge in the housing with seals to minimize air leakage when the blades are closed. The housing is designed in such a way to provide optimal air mixing situations through available cross-sectional area at different ventilation stages. The blades are designed to maximize air jet throw during lower ventilation stages, and provide superior total airflow during maximum ventilation stages.

Claims

1. An air inlet unit for use in a building and having a fan that provides airflow between an interior of the building and an exterior of the building, wherein the air inlet unit comprises: a frame suitable for mounting the air inlet unit in a wall of the building, the frame including endcaps and longitudinal members combined with and extending between the endcaps, wherein each of the endcaps includes an endcap frame, a foam insert and an endcap cover, and wherein the frame has an opening providing communication to the exterior of the building; at least one blade assembly having a louver with an aerodynamic shape comprising a top edge, a bottom edge and outer ends, wherein the at least one blade assembly is mounted at the top edge between the longitudinal members of the frame so as to be moveable from an open position to a closed position, wherein in the closed position the bottom edge engages one of the longitudinal members; a continuous hinge for mounting the at least one blade assembly at the top edge and for restricting air flow leakage at the top edge, wherein the continuous hinge is located between the longitudinal members.

2. The air inlet unit of claim 1, further comprising a center member extending between and connected to the endcaps, wherein the continuous hinge is connected to the center member for mounting the at least one blade assembly.

3. The air inlet unit of claim 2, wherein the at least one blade assembly includes two blade assemblies each connected to the center member at respective top edges of the two blade assemblies by the continuous hinge.

4. The air inlet unit of claim 1, wherein each blade assembly includes the blade and blade ends located at the outer ends.

5. The air inlet unit of claim 4, wherein the blade ends each include a brush border seal.

6. The air inlet unit of claim 1, wherein the at least one blade assembly includes a rounded edge and the frame includes a rounded edge to facilitate the airflow into and through the air inlet unit.

7. The air inlet unit of claim 1, wherein the continuous hinge extends between the endcaps to span a length of the air inlet unit.

8. The air inlet unit of claim 2, wherein the continuous hinge is connected to the center member and the top edge of the at least one blade assembly along a length of the center member between the endcaps.

9. The air inlet unit of claim 1, wherein the continuous hinge and the longitudinal members have rounded interior edges to facilitate the airflow through the opening of the frame.

10. The air inlet unit of claim 1, wherein the frame is substantially square-shaped.

11. The air inlet unit of claim 1, wherein the top edge of the louver is provided with a longitudinally extending opening for receiving the continuous hinge.

12. The air inlet unit of claim 2, wherein the top edge of the blade assembly is provided with a longitudinally extending opening for receiving a first portion of the continuous hinge and the center member is provided with longitudinally extending opening for receiving a second portion of the continuous hinge.

13. The air inlet unit of claim 1, wherein at a minimum ventilation in the open position, the bottom edge of the at least one blade assembly does not engage with the longitudinal members and the outer ends of the at least one blade assembly engage with the endcaps for an increase of a jet throw of the air flow.

14. The air inlet unit of claim 1, wherein at a maximum ventilation in the open position, the at least one blade assembly is pivoted at the continuous hinge such that the bottom edge extends at least 8 inches from the longitudinal members.

15. The air inlet unit of claim 1, wherein the air inlet unit is fully insulated.

16. The air inlet unit of claim 1, wherein the at least one blade assembly has a longitudinal length which is between one and one half to three times a width of the at least one blade assembly.

17. The air inlet unit of claim 1, wherein the continuous hinge includes two “T” geometries with a flexible middle between the two “T” geometries.

18. The air inlet unit of claim 1, wherein the at least one blade assembly provides a longitudinally extending opening for receiving the continuous hinge.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a perspective view of a ceiling inlet unit constructed according to the principles of the invention, viewing the unit as it would appear from the top before installation, the view showing the two blades in the closed or shutoff position;

(2) FIG. 2 is a top view of a ceiling inlet constructed according to the principles of the invention;

(3) FIG. 3 is a section view of the ceiling inlet unit taken on the line 3-3 of FIG. 2, but viewing the unit as it would appear from the right when inside the room of a building, the view also showing the two blade assemblies in the closed position;

(4) FIG. 3A is an enlarged view of a portion of the hinge assembly of the ceiling inlet unit of FIG. 3;

(5) FIG. 3-3 is a side view of the ceiling inlet of FIG. 1, viewing the inlet as it would appear from the side when inside the room of a building, the view showing both blade assemblies in the closed position;

(6) FIG. 4 is a section view of the ceiling inlet unit similar to FIG. 3, viewing the unit as it would appear from the right when inside the room of a building, the view also showing the two blade assemblies in the closed position;

(7) FIG. 4A is an enlarged view of a portion of FIG. 4 but showing where the blade meets the frame profile;

(8) FIG. 5 is a perspective of a ceiling inlet unit constructed according to the principles of the invention, viewing the unit as it would appear from the top before installation, the view showing the two blades in the minimum ventilation position;

(9) FIG. 6 is a section view of the ceiling inlet similar to FIG. 3, viewing the unit as it would appear from the right when inside the room of a building, the view also showing the two blades in the minimum ventilation position;

(10) FIG. 6A is an enlarged view of a portion of FIG. 6 but showing the blade curvature during minimum ventilation as well as the endcap design;

(11) FIG. 6-6 is a side view of the ceiling inlet similar to FIG. 3-3, viewing the inlet as it would appear from the side when inside the room of a building, but showing one blade in the minimum ventilation position;

(12) FIG. 7 is a perspective view of the air ventilating unit of the invention, viewing the unit as it would appear from the top before installation, the view showing the two blades in the maximum ventilation position;

(13) FIG. 8 is a section view similar to FIG. 3, viewing the unit as it would appear from the right when inside the room of a building, the view also showing the two blade assemblies in the maximum ventilation position;

(14) FIG. 8-8 is a side view of the ceiling inlet similar to FIGS. 3-3 and 6-6 and viewing the inlet as it would appear from the side when inside the room of a building, but showing one blade in the maximum ventilation position;

(15) FIG. 9 is an exploded perspective view of the blade assembly as it would appear from the top of the ceiling inlet;

(16) FIG. 9A is an enlarged view of the blade endcap design from the portion of FIG. 9 where the brush border/seal is mated with the endcap;

(17) FIG. 10 is a side view of the curved louver geometry as it would appear from the right view of the blade assembly;

(18) FIG. 11 are views showing the continuous hinge from an end view and also a portion of the hinge in perspective;

(19) FIG. 12 is a prior art psychrometric chart from the air conditioning company

(20) Carrier Corporation;

(21) FIG. 13 us a graphical representation from data of the inlet of the invention showing the efficiency of the inlet;

(22) FIG. 14 is a graphical representation illustrating the efficiency of the inlet of the invention because of the increased velocity of air flow through the inlet when partially open; and

(23) FIG. 15 is a graphical representation similar to FIG. 14 showing the increased velocity of air flow through the inlet when the inlet is fully open.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS OF THE INVENTION

(24) Referring first to FIGS. 1 and 2, the basic ceiling inlet unit of the invention is comprised of a frame having two endcap sub-assemblies 4 that connect the frame members and the center profile member 2 and hold them together so that the frame 1 can be used to install the ceiling inlet unit of the invention in an opening in the ceiling of an interior room of a building to be ventilated. As is well known to those skilled in the art, the ceiling inlet unit is combined with an actuator and exhaust or positive pressure fan, outlet damper, or shutter wall (not shown) which, when on and the actuator opens the ceiling inlet unit of the invention, will draw air from the attic of the building through the ceiling inlet unit, and will bring air into the interior room of the building. FIG. 1 shows the top face of the unit at it would appear when viewed from inside of the building before installation, and FIG. 2 shows the top face which faces the rough opening in the ceiling. The frame provides for installing the unit in the ceiling of a building in any suitable manner, and the frame includes two side members 1, two endcaps 4 and 7 that comprise the mounting structure for two blade assemblies 10, and the center profile member 2. FIGS. 3A and 9 show each blade assembly 10 in more detail which is comprised of a curved louver 15, two blade endcaps 13, 14, and two brush borders 17. Brush borders 17 are flexible and compressible seals attached to the blade endcaps 13, 14 to correct small differences in the louver length which occur within the tolerances of the louver. Brush borders 17 are preferably made of a flexible and/or compressible material to allow free movement of the louvers 15 in any weather or temperature.

(25) FIG. 11 shows the continuous hinge 11 which is shown having two uniform “T” geometries at either end and a thinner, flexible center which connects the two uniform “T” geometries. As best seen in FIG. 3A, each continuous hinge 11 is assembled into the blade assembly 10 and the center member 2 along the entire length of the ceiling inlet which will mitigate any leakage that may flow through the ceiling inlet into the interior room. The continuous hinge 11 has a non-uniform wall thickness in the flexible center of the hinge 11 to allow the blade assemblies 10 to move rotationally from a closed to an open position for minimum or maximum ventilation. This non-uniform wall thickness in the hinge 11 eliminates any need for additional pins or metal rods to be used for pivoting the blade assemblies 10. The continuous hinge 11 also extends the entire length of the louver blade assemblies 10 blocking any air leakage from penetrating through unplanned openings. It will be understood that the blade assemblies pivot open and shut on this continuous hinge, and the hinge allows the inlet to be opened deeper than any other inlet on the market as shown best in FIG. 8. As best seen in FIGS. 3, 4, 6A, 9 and 10, each blade assembly 10 is formed into an aerodynamic shape to maximize the air jet throw along the ceiling of the rooms where the ceiling inlets are installed. As best shown in FIG. 3A, along the top edge of the blade assembly 10 is a longitudinally extending opening 16 for receiving the continuous hinge 11 that provides for attaching each blade assembly 10 within the center member 2. As best seen in FIGS. 4 and 4A, each blade assembly 10 has geometry that mates perfectly against the frame 1 in the closed or shutoff position. This mitigates any leakage that could enter into the interior room of the building. The continuous hinge 11 may be extruded such that the two uniform “T” geometries and the flexible center are made of the same material but have different thickness so the middle is flexible while the “T” geometries are rigid.

(26) FIGS. 5, 6, and 6A show in more detail how the endcap design 7 is optimized for the minimum ventilation stage. When the blade assemblies 10 are open for minimum ventilation as shown in FIG. 5, the blades are open a few inches. The blade geometry matches the endcap design 7 as shown in FIG. 6A so that there will be no side leakage from the inlet until after minimum ventilation stages are done. As shown in FIG. 6A the blade assemblies 10 are blocked entirely on the sides by the endcap 7 which will increase the overall air jet throw of the inlet. FIG. 5 also shows that the cross-sectional area available for the air to move through the inlet is optimized through the substantially square design. In a substantially square design, the longitudinal length of the blade assembly 10 is between 1.5 to 3 times the width of the blade. Also shown in FIG. 6A is that the middle of the blade assemblies 10 do not reach below the geometry of the endcap 7 when the blade is open for minimum ventilation.

(27) FIGS. 7 and 8 show in more detail how the endcap design 7 is optimized for the maximum ventilation stage. When the blade assemblies 10 are open for maximum ventilation as shown in FIGS. 7 and 8, the blades are able to extend downward more than 8 inches due to the design of the continuous hinge 11. This allows the inlet to achieve maximum total airflow through the inlet during maximum ventilation.

(28) Performance data is shown below for three separate inlet designs from Bess Labs, a certified performance testing location understood and validated by those skilled in the art.

(29) TABLE-US-00001 University of Illinois Department of Agricultural Engineering Bloenvironmental and Structural Systems Lab Final Report Project Number: 17641 Test Date: Oct. 31, 2017 Inlet: Make- Double L Model- DL3127 Size- 25″ × 27.5″ rough opening Description: double baffle ceiling inlet Notes: Test conditions: T(wb): 57.0 Barometric pressure, recorded 29.51 T(db): 77.0 Barometric pressure, corrected 29.38 Static Pressure Airflow (in. H.sub.2O) (cfm.) Full Open 0.010 948 0.030 1663 0.050 2157 0.070 2553 0.100 3034 0.125 3355 0.150 3695 0.200 4227 0.250 4694 Baffles 8″ open 0.100 2187 Baffles 4″ open 0.100 1284 Baffles 2″ open 0.100 667 Baffles 1″ open 0.100 348 Baffles 0.5″ 0.100 221 Baffles 0.25″ 0.100 141 Baffles closed (leakage) 0.100 4 Project Number: 19572 Test Date: Dec. 4, 2019 Inlet: Make- Double L Model- DL4727 Size- 24.5″ × 44″ rough opening Description: double baffle ceiling inlet Notes: Test conditions: T(wb): 55.0 Barometric pressure, recorded 29.07 T(db): 75.0 Barometric pressure, corrected 28.95 Static Velocity Pressure Airflow Average Velocity (in, H.sub.2O) (cfm) (fpm) Max (fpm) Full Open 0.050 3325 0.070 3903 0.100 4628 0.125 5165 0.150 5708 0.200 6602 ½″ open 0.050 203 0.100 308 757 871 0.125 368 0.150 424 1″ open 0.050 415 0.100 607 843 1051 0.125 712 0.150 811 2″ open 0.050 729 0.100 1056 1055 1155 0.125 1193 0.150 1332 4″ open 0.050 1406 0.100 1982 1099 1194 0.125 2217 0.150 2240 6″ open 0.050 1960 0.100 2854 1190 1277 0.125 3140 0.150 3500 8″ open 0.050 2322 0.100 3343 1148 1236 0.125 3694 0.150 4048 Project Number: 19261 Inlet: Inlet Make- Double L Model- DL3232 Size- 28″ × 14.5″ baffles (2) Description double baffle ceiling inlet Notes 29.5″ ×29.5″ Rough opening Velocities: Kestrel 5500 anemometer Test conditions T(wb): 60.0 T(db): 78.0 Static Velocity Pressure Airflow Average Velocity (in. H.sub.2O) (cfm) (fpm) Max (fpm) 1″ Baffle openings 0.050 309 0.100 444 1005 1084 0.125 509 0.150 548 2″ Baffle openings 0.050 535 0.100 771 1111 1150 0.125 864 0.150 962 4″ Baffle openings 0.050 989 0.100 1410 1188 1214 0.125 1571 0.150 1745 6″ Baffle openings 0.050 1472 0.100 2081 1132 1214 0.125 2281 0.150 2546 8″ Baffle openings 0.050 1856 0.100 2607 1151 1202 0.125 2904 0.150 3217 Full Open 0.050 2958 0.100 4195 1223 1282 0.125 4630 0.150 5075

(30) Bess Labs Test project number 17641 is testing on a standard ceiling inlet in the industry. This inlet has a curved louver that is not as deep as the ceiling inlet of the invention and the ceiling inlet is of rectangular shape. Test project number 19572 is a similar design to the inlet in 17641, but the ceiling inlet is longer and more rectangular to achieve more maximum airflow than the option from test 17641. Test project number 19261 is performance data relating to the ceiling inlet of the invention. Testing is conducted on each inlet at different baffle openings, and baffle is a description synonymous with louver blade. Those skilled in the art understand that when the test is conducted for smaller louver openings (1″-4″) it is evaluating the performance of minimum ventilation mode. When the test is conducted for larger openings (8″, full open) it is evaluating the maximum ventilation performance. Those skilled in the art understand that the data from a 0.100″ S.P. is the typical performance data point used for comparison purposes as this static pressure is very close the operating pressure in modern livestock and swine facilities. Performance data can be applied to equation 2 from above to calculate the drag coefficient of each inlet. Those skilled in the art understand that inlet efficiency is directly related to the drag coefficient of the inlet. The drag coefficient is understood by those skilled in the art on a scale of 0 to 1, with 1 being the most efficient air inlet possible.

(31) $C_d=\frac{\stackrel{.}{V}}{A_{\mathrm{actual}}\sqrt{\frac{2\Delta P}{\rho }}}$

(32) Where: {dot over (V)}=Total volume of air entering through inlet A.sub.actual=Total Cross-sectional area of opening for air to move through C.sub.d=drag coefficient of the inlet P=Static pressure differential across inlet ρ=density of incoming air

(33) Applying the above performance data to equation number 2, and utilizing information from the Carrier psychrometric chart (see FIG. 12) that is approved by those skilled in the art yields an example drag coefficient calculation in excel as follows:

(34) TABLE-US-00002 Inlet Model Number D13127 DL4727 DL3232 Bess Labs Test Number 17641 19572 19261 Test Type: Ceiling inlet louver 2″ open Inputs: Wet bulb Temperature (° F., 57 55 60 Bess labs data) Dry Bulb Temperature (° F., 77 75 78 Bess labs data) Specific Volume (ft3/lb, 13.60 13.55 13.70 Carrier Psychometric chart) Length Blade opening (in., 28.00 43.00 29.00 inlet dimension) Depth blade opening (in., 2.00 2.00 2.00 inlet dimension) Volumetric flow rate (cfm, 667 1056 771 Bess labs data) Static Pressure (in. w.c., Bess labs data) 0.100 0.100 0.100 Calculated Values: Air density (kg/m3) 1.18 1.18 1.17 A, actual (in2) 112.00 172.00 116.00 A,actual (m2) 0.07 0.11 0.07 Volumetric flow rate (m3/s) 0.31 0.50 0.36 Static Pressue (Pa) 24.88 24.88 24.88 SQRT((2ΔP/p)) 6.50 6.49 6.52 Cd, inlet drag coefficent 0.670 0.692 0.745

(35) As shown in FIG. 12, the ceiling inlet of the invention has a proven calculated drag coefficient that is larger than other standard ceiling inlets offered by the market, and this directly correlates to the increased efficiency that the ceiling inlet of the invention offers. The ceiling inlet of the invention provides more efficient mixing at both minimum and maximum ventilation modes shown by the calculation.

(36) Another indicator of inlet efficiency understood by those skilled in the art is air jet throw which is measured as velocity. Performance data as shown by Bess Labs above displays velocities at different louver openings for review. A graph displaying the data when the ceiling inlet of the invention is open 1 inch (or during minimum ventilation) is shown in FIG. 14. This ceiling inlet of the invention provides 444 cubic feet per minute of air at a 1,005 feet per minute velocity while the standard rectangular inlet of the industry provides 607 cubic feet per minute of air at only 843 feet per minute velocity.

(37) The ceiling inlet of the invention can provide less airflow at an increased velocity compared to a standard rectangular inlet of the industry. The ability to provide less cfm of air during minimum ventilation at an increased velocity promotes uniform temperature distribution through more efficient air mixing, and this is desirable as the grower will have more control over the air entering the facility than other ceiling inlets. When inlets are less efficient and do not have high velocity or good air jet throw, the air drops to the animal occupied zone before sufficiently mixing and heating up the air and this leads to chilling animals and creating an environment that creates cold stress on the livestock or pigs.

(38) The ceiling inlet of the invention when in maximum ventilation mode (see FIG. 15) provides 4,195 cubic feet per minute (“cfm”) at a 0.100 in. S.P., and this provides a higher airflow capacity than a traditional rectangular design (DL3127). A traditional inlet design only provides 3,034 cfm at 0.100 in. S.P. Those skilled in the art understand that over 4,000 cfm is the desired target for a larger capacity ceiling inlet.

(39) Having thus described the invention in connection with the preferred embodiments thereof, it will be evident to those skilled in the art that various revisions can be made to the preferred embodiment described herein without departing from the spirit and scope of the invention.