U.S. patent number 3,809,144 [Application Number 05/307,984] was granted by the patent office on 1974-05-07 for weather curtain for airplane hangar entrance.
Invention is credited to James F. Garufo.
United States Patent |
3,809,144 |
Garufo |
May 7, 1974 |
WEATHER CURTAIN FOR AIRPLANE HANGAR ENTRANCE
Abstract
A pass-through curtain suspended across the entrance of a large
enclosure such as an airplane hangar or other building has an inner
and outer series of transparent, back-to-back, depending closure
flaps which are arranged in overlapping relationship with one
another to prevent the escape of temperate air from the hangar or
the inflow of ambient air when the hangar door is open, yet allow
the forced entry of an airplane by deflecting and parting of the
flaps. A substantially air-impervious barrier portion of the
curtain above the pass-through, flap portion and along each end
thereof precludes air flow through areas of the curtain other than
the flap portion to thereby further reduce the total volume of air
passed by the curtain. A transverse, air-inflated, stiffening tube
extending across the curtain slightly above the flaps and an
individual, vertically extending stiffening tube on each flap
rigidify the curtain and flaps so that the flaps quickly return to
their undeflected positions instead of clinging to the wings and
tail structure of the airplane as it moves through the curtain.
Zippered pockets of granular weight material along the bottom of
the flaps provide variable ballast.
Inventors: |
Garufo; James F. (Wichita,
KS) |
Family
ID: |
23192026 |
Appl.
No.: |
05/307,984 |
Filed: |
November 20, 1972 |
Current U.S.
Class: |
160/184 |
Current CPC
Class: |
E06B
3/01 (20130101) |
Current International
Class: |
E06B
3/00 (20060101); E06B 3/01 (20060101); A47h
023/05 () |
Field of
Search: |
;160/126,184,332,349,273
;52/2 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Stein; Mervin
Assistant Examiner: Kannan; Philip C.
Attorney, Agent or Firm: Schmidt, Johnson, Hovey &
Williams
Claims
Having thus described the invention what is claimed as new and
desired to
1. A pass-through curtain for use on an enclosure across an
entrance thereof, said curtain comprising:
a substantially solid, normally upper barrier portion precluding
pass-through when the curtain is in use;
at least one series of side-by-side, elongated closure flaps
depending from said upper portion along the lower extent of the
latter,
said flaps having a line of hinging movement defined at their upper
ends by their junction with the upper portion,
said hinge line extending transversely to said flaps for the full
length of said series thereof; and
an elongated, overhanging, flap-restraining element extending along
said hinge line closely adjacent the same for the full length
thereof to stiffen the curtain and to resist excessive deflection
of the flaps,
said element in its transverse dimension projecting outwardly for a
distance from one side of the curtain beyond the flaps to provide a
limit
2. A pass-through curtain as claimed in claim 1, wherein said
element is generally cylindrical in cross-sectional configuration
having its outermost arcuate periphery overlying the region within
which the flaps
3. A pass-through curtain as claimed in claim 1, wherein said
element
4. A pass-through curtain as claimed in claim 1, wherein is
provided a second element on the opposite side of the curtain in
alignment with the first-mentioned element for limiting swinging of
the flaps in the opposite
5. A pass-through curtain as claimed in claim 4, wherein each of
said elements comprises an inflatable tube having its outermost
periphery overlying the respective regions within which the flaps
swing during
6. A pass-through curtain as claimed in claim 5, wherein each of
said flaps is provided with a weight at its lowermost end for
augmenting the swing-limiting action of said tubes.
Description
This invention relates broadly to closure structures for the
entrances of large enclosures such as aircraft hangars and the like
and, more particularly, to a special pass-through, weather curtain
mounted across the entrance of such an enclosure, which minimizes
the inflow and outflow of air through the entrance during ingress
and egress of objects such as airplanes from the enclosure.
Hangars of many diverse sizes and configurations have been provided
in the past to accommodate airplanes for both storage and
maintenance purposes. In many instances, such hangars encompass a
wide expanse of floor area and are sufficiently tall to accommodate
aircraft with high tail sections. Thus, large open areas are
presented which cause difficulty in heating and cooling the hangar
to maintain comfortable working conditions, particularly in those
climates where extreme heat or cold is experienced.
For example, in environments of extreme cold, it may be difficult
in the first instance to bring the area within the hangar up to a
comfortably warm temperature and to maintain it at such
temperature, even with the hangar door fully closed. When the door
is subsequently opened for entry or exit of an airplane, a large
amount of the heat within the hangar may be lost through the hangar
entrance, particularly in those situations where strong, gusty
winds prevail. Moreover, since the door must remain open for a
substantial period of time to allow the airplane to fully clear the
hangar entrance before once again closing the door, further heat
loss is experienced as a function of the time the door remains
open. In situations where the heat loss is particularly severe, it
may be several hours before heating equipment for the hangar can
once again bring the temperature to a comfortable level. Hangars
having unusually busy traffic patterns are more susceptible to heat
loss than others, and may even render it virtually impossible to
maintain a comfortable, working temperature within the hangar.
Similarly, in climates where air conditioning is required to cool
the hangar interior to a comfortable working temperature,
conditioned air is lost when the hangar door is opened, thereby
creating unpleasant working conditions and causing the air
conditioning equipment to function inefficiently.
Accordingly, one important object of the present invention is to
provide a special pass-through weather curtain suspended across the
entrance of an enclosure such as a hangar immediately behind the
door thereof which is designed to maintain substantial continuity
of working conditions within the hangar when the door thereof is
opened for passage of an object such as an airplane through the
curtain and entrance.
Another important object of the present invention is to provide a
weather curtain as aforesaid having a substantially solid,
air-barrier upper portion through which neither air nor parts of
the object such as an airplane pass and a lower pass-through
portion which yields to the forced entry of the object, but not to
the efforts of air seeking to flow through the entrance.
A further important object of this invention is to provide a
special weather curtain having barrier and pass-through portions as
set forth above wherein the pass-through portion is only as large
as that necessary to accommodate the largest airplane or other
object anticipated, thereby maximizing the air-repelling area of
the curtain to maximize its ability to maintain continuity of
working temperature within the hangar.
An additional important object of this invention is to provide a
double series of side-by-side, depending flexible flaps in the
pass-through portion of the curtain wherein the flaps of one series
overlap those of the other series to close slits presented between
adjacent flaps which would otherwise permit airflow
therethrough.
Yet another important object of the instant invention is the
provision of an inflated stiffening tube which extends across the
curtain slightly above the flexible, pass-through flap portion
thereof and individual, vertically extending stiffening tubes on
the flaps to increase the structural rigidity of the curtain and
flaps to an extent that clinging of the flaps to the wings and tail
structure of the airplane passing through the curtain is strongly
resisted.
Other important objects of this invention include providing
ballast-increasing weight pockets filled with granular material
along the bottom of each flap; constructing the flaps of
transparent material to provide full and clear vision during entry
and exit of an airplane; and providing a curtain which is capable
of carrying out all of the above object without detracting from its
ability to be raised and lowered by wrapping and unwrapping the
same from around a storage cylinder or roll.
In the drawing:
FIG. 1 is a fragmentary elevational view of an enclosure in the
form of a hangar employing a weather curtain which embodies the
principles of the present invention, the hangar door being shown in
a fully raised condition to reveal the curtain there behind, and
the outline of an airplane behind the curtain being indicated in
phantom;
FIG. 2 is a fragmentary, vertical cross sectional view through the
hangar taken along line 2--2 of FIG. 1;
FIG. 3 is an enlarged, fragmentary cross sectional view through the
curtain taken along line 3--3 of FIG. 1;
FIG. 4 is an enlarged, fragmentary cross sectional view through the
hangar and curtain taken along line 4--4 of FIG. 1;
FIG. 5 is an enlarged, fragmentary horizontal sectional view
through one sheet of the curtain showing the valve fitting for the
stiffening air tube of the curtain; and
FIG. 6 is an enlarged, fragmentary view of the front of the curtain
showing the individual stiffening tubes on the flaps, the front
sheet and flaps of the curtain being partially broken away to
reveal the rear sheet and its flaps.
An enclosure 10 in the form of an aircraft hangar may assume any
one of a variety of configurations and has an entrance 12 closable
by a door 14 which may be of any suitable character, here indicated
as being of the vertically folding type. The weather curtain
assembly of the present invention, denoted broadly by the numeral
16, is disposed immediately behind door 14 and includes a curtain
18 suspended across entrance 12 by an idler roll 20 and an actable
motor 22 which provides power for raising and lowering of curtain
18. A driven roll 24 operably coupled with motor 22 provides a base
upon which the curtain 18 may be rolled when not in use.
The curtain 18 includes a pair of back-to-back, identical sheets 26
and 28 of canvass or other suitably air-impervious material and has
a generally upper, barrier portion defined by the flat expanse of
sheets 26 and 28, and a lower, pass-through portion defined by a
large opening 30 in each sheet. Marginal side extensions of the
barrier portion are presented by marginal edge sections 32 on each
sheet 26 and 28 on opposite ends of their respective openings 30.
The sheets 26 and 28 are sewn together at least in two places along
seams 34 and 36 as shown in FIG. 3 so that the openings 30 are in
exact registration with one another and are maintained in such
registration even during raising and lowering of curtain 18.
The openings 30 of sheets 26 and 28 are ach of such a size and
configuration to minimize the pass-through portion of curtain 18 so
that a large expanse of curtain 18 may be devoted purely to
resisting the flow of air into or out of hangar 10 during passage
of an object such as an airplane through entrance 12. In this
respect, it is important that each opening 30 conform generally to
the basic shape of the object, in this instance an airplane 38. For
airplane 38, each opening 30 has a lower, rectangular main area 30a
which is adapted to clear the fuselage 40 and wings 42 of the
airplane 38 and an upper, centrally located area 30b which adjoins
and communicates with area 30a to clear the tail structure 43 of
the airplane 38. It will be seen that by limiting the width and
height of central area 30b to a size which is just sufficient to
clear the largest and tallest tail structure 43 of an airplane
contemplated to be using entrance 12, a relatively large expanse of
curtain 18 may be retained on opposite sides of area 30b to
function as a barrier and resist outflow or inflow of air through
entrance 12.
The presence of the additional barrier area on opposite sides of
open area 30b is especially important when it is considered that
the hangar 10 may be situated in an environment of extremely
adverse weather conditions, such as extreme cold with strong, gusty
winds or extreme heat. In these situations, every extra amount of
curtain 18 that can be devoted to the retention of the temperature
controlled air within hangar 12 and the repulsion of ambient air
contributes significantly to the maintenance of comfortable working
conditions within hangar 10. In this respect, it should be noted
also that the marginal side sections 32 of each sheet 26 and 28
further contribute to minimizing the open expanse of curtain 18 and
should be as wide as permitted by the wingspan of the largest
airplane contemplated for using hangar 10. The double thickness
provision of curtain 18 as presented by sheets 26 and 28 is also
important in minimizing the passage of air through curtain 18, and
it is contemplated that where the cost is not prohibitive, sheets
26 and 28 may be constructed of a solid, homogeneous material as
opposed to a woven fabric material such as canvas.
The sheets 26 and 28 are provided with an inner and outer series of
depending, flexible closure flaps 44 and 46 which fill their
corresponding openings 30 to provide limited entry therethrough.
Each series of flaps 46 and 48 is secured to its corresponding
sheet 26 and 28 along the seam 36, and the outer flaps 44 overlap
the inner flaps 46 such that the slits presented between adjacent
flaps 44 or 46 are covered to minimize the passage of air
therethrough. If desired, the flaps 44 and 46 may be constructed of
a transparent, plastic material to provide full and clear vision
through curtain 18 and thereby minimize the possibility of
accidents occuring during entry or exit of airplane 38.
Each of the individual flaps 44 and 46 is provided with variable
ballast means in the form of a zippered pocket 48 at its lower
extremity which is adapted to contain a granular weight material
such as sand 50. Through the provision of a zipper 52 on each
pocket 48, it is possible to add to or substract from the amount of
sand 50 contained within pockets 48, thereby varying their effects
as ballast for the flaps 44 and 46.
The curtain 18 is retained in place during pass-through of airplane
38 by the joint efforts of retaining and guiding structure 54 (FIG.
4) along the sides of curtain 18 and transverse stiffening means 56
across the curtain 18. The guiding and retaining structure 54
includes a split tube guide track 58 which extends vertically along
each side of curtain 18 on hangar 10 and a following bead 60 formed
in each outer extremity of the marginal sections 32 of sheets 26
and 28, each bead 60 being formed by sewing a flexible element
between the sheets 26 and 28 as indicated in FIG. 4. The size of
bead 60 is such that it will move longitudinally with ease within
tube 58, yet may not be withdrawn from the latter through slit 62
in tube 58. The flexible nature of bead 60 permits curtain 18 to be
rolled up during storage.
The transverse stiffening means 56 comprises a pair of inflated
tubes 64 and 66 on the sheets 26 and 28 respectively which follow
the outline of openings 30 a short distance above the upper
extremities of the respective flaps 44 and 46. The tubes 64 and 66
decrease deflection of curtain 18 as a whole when airplane 38
passes through flaps 44 and 46, and thereby facilitate the movement
of airplane 38 through flaps 44 and 46. Without tubes 64 and 66,
the flaps 44 and 46 would tend to cling to the projecting parts of
airplanes 38 since the whole of curtain 18 would bow in upon
receiving the push from airplane 38. Tubes 64 and 66 provide a
firm, rigid base from which flaps 44 and 46 can swing. Also, as
clearly shown in FIG. 3, the tubes 64 and 66 project transversely
outwardly from the curtain overhanging the regions within which the
flaps 44 and 46 swing. The tubes 64 and 66 therefore can act as
upper limits for the swinging flaps 64 and 66 as is obvious from
FIG. 3. In this regard, it will be noted that in hangars where the
distance from the entrance 12 to the rear of hangar 10 is such that
airplane 38 is maintained closely adjacent curtain 18 when the
airplane 38 is parked within hangar 10, the clinging problem may be
accentuated. However, the stiffening tubes 64 and 66 discourage
such clinging even in this situation, limiting upward swinging of
flaps 44 and 46 and urging the same to their normal depending
positions, aided by the ballast pockets 48. As shown in FIG. 5,
valve fitting 68 is provided on each tube 64 and 68 for inflating
or deflating the same.
In addition to the action of transverse stiffening tubes 64 and 68,
clinging of the flaps 44 and 46 to the airplane 38 is also
discouraged by individual, vertically extending stiffening air
tubes 70 (FIG. 6) on the individual flaps 44 and 46. The air
pressure in the individual tubes 70 is separate from that of
transverse tubes 64 and 66, and tubes 70 may be totally independent
of one another or have a common connecting conduit. In either
event, a valve fitting (not shown) similar to fitting 68 may be
provided for tubes 70 to permit regulation of the air pressure
therewithin.
It should be apparent from the forgoing that my weather curtain
assembly 16 is ideally suited for solving the problems heretofore
experienced in maintaining continuity of working conditions within
large enclosures such as airplane hangars, particularly in
environments of extreme heat or cold. The overlapping flaps 44 and
46 do not allow the passage of air when door 14 is raised; only the
forced entry of airplane 38 is permitted. Accordingly, even though
the winds outside of hangar 10 may be cold and blustery, or hot and
humid, door 14 may be raised and left open for substantial periods
of time without fear of losing the comfortable working temperature
within hangar 10. The airplane 38 may thus be moved through
entrance 12 with all the deliberate care and speed which should be
exercised when handling expensive, sophisticated equipment of this
type.
Many of the flaps 44 and 46 remain undeflected during passage of
airplane 38, and these provide a barrier to air seeking to escape
from hangar 10 or the ambient air seeking to enter hangar 10.
Moreover, the large expanse of solid, barrier area above flaps 44
and 46 and along the ends of openings 30 increases the ability of
curtain 18 to prevent the passage of air substantially beyond that
which could be obtained if flaps 44 and 46 extended the full height
and width of curtain 18. In the event that the weather conditions
existing at hangar 10 are moderate, the curtain 18 may be readily
raised and stored in roll form on roll 24, although it may be
necessary to first deflate tubes 64, 66, and 70.
* * * * *