U.S. patent number 3,852,526 [Application Number 05/404,522] was granted by the patent office on 1974-12-03 for inspection instrument.
This patent grant is currently assigned to Thiokol Corporation. Invention is credited to La Ron D. Binggeli, Edward E. McCullough, Kerry G. Zundel.
United States Patent |
3,852,526 |
McCullough , et al. |
December 3, 1974 |
INSPECTION INSTRUMENT
Abstract
An observation device for inspecting elongated cavities is
attached to the outer end of a cable made of pneumatic tubes and
electrical conductors encased in a flexible sheath. The cable
passes through a sleeve attached in an inflatable support that
curves through an arc of approximately 90.degree., so that it
enters the base of the inflatable support and emerges through the
top thereof. The cable is attached to a control box containing
connectors to a pressurized source of gas, a source of electrical
power, and control means therefor. A series of inflatable braces
concentrically surrounds the cable for supporting it in the center
of the cavity to be inspected, each brace being inflatable through
a pneumatic tube leading from the source of gas. The protective
sheath of the cable is inflatable to impart rigidity when in use,
and also to surround the pneumatic tubes with the same pressure as
their interiors, so that wall thicknesses thereof may be minimized
for compactness when stored.
Inventors: |
McCullough; Edward E. (Brigham
City, UT), Zundel; Kerry G. (Tremonton, UT), Binggeli; La
Ron D. (Logan, UT) |
Assignee: |
Thiokol Corporation (Bristol,
PA)
|
Family
ID: |
23599940 |
Appl.
No.: |
05/404,522 |
Filed: |
October 9, 1973 |
Current U.S.
Class: |
348/85; 396/19;
356/241.1 |
Current CPC
Class: |
G03B
37/005 (20130101); F02K 9/24 (20130101); G02B
23/2476 (20130101); G01N 33/222 (20130101) |
Current International
Class: |
G02B
23/24 (20060101); G01N 33/22 (20060101); F02K
9/00 (20060101); F02K 9/24 (20060101); G03B
37/00 (20060101); G02B 6/04 (20060101); H04n
007/18 () |
Field of
Search: |
;178/DIG.1,DIG.30,7.81,7.2 ;350/11 ;356/237,241 ;354/63
;73/167 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Britton; Howard W.
Assistant Examiner: Masinick; Michael A.
Attorney, Agent or Firm: McCullough; Edward E.
Claims
The invention claimed is:
1. A bore inspection instrument comprising:
an inflatable base;
means for anchoring the base to some stationary part adjacent the
bore to be inspected;
a cable held by the base, capable of sliding motion relative
thereto, and including pneumatic tubes;
inflatable braces attached to the cable, each being attached to a
tube therein;
means for controlling fluid flow, attached to the tubes of the
cable and attachable to a source of gas, for controlling inflation
of the base and of the inflatable braces; and
observation means attached to the end of the cable opposite the end
attached to a control means.
2. The inspection instrument of claim 1 wherein the base
comprises:
a hollow, inflatable cone made of two parallel sheets of thin,
flexible nonelastic material, sealed at their edges, and fibers
that extend from one sheet to the other, the ends of the fibers
being embedded in the sheets; and
a curved sleeve fixed in the cone and passing therethrough, one end
of the sleeve penetrating the top of the cone and the other end
extending from the bottom thereof.
3. The inspection instrument of claim 1 wherein the observation
means is a television camera.
4. The inspection instrument of claim 1 wherein the means for
controlling fluid flow comprises:
a control box having a threaded cavity for receiving a threaded
bottle of compressed gas, and a system of ducts having branch ducts
leading from the gas bottle cavity wherein each branch duct is
connectable to one of the tubes of the cable; and
a valve in each branch duct capable of opening and closing its duct
to the source of gas, and of opening the portion of its duct that
lies adjacent the cable to the atmosphere.
5. The inspection instrument of claim 4 further including:
a flow meter in each branch duct for determining when its
associated inflatable device has been inflated; and
a connector for connecting the branch ducts to the tubes of the
cable.
6. The inspection instrument of claim 1 wherein the cable comprises
an outside sheath and pneumatic tubes inside the sheath; and
wherein the inflatable braces are disks concentric about the cable
and attached thereto at intervals such that the segment of the
cable between any two adjacent braces is resistant to bending.
7. The inspection instrument of claim 6 wherein the inflatable
braces have fibers passing between opposite walls and embedded
therein to maintain dimensional stability thereof when
inflated.
8. The inspection instrument of claim 6 wherein the sheath of the
cable is connectable to a source of gas and is inflatable, whereby
stiffness may be imparted thereto to facilitate its extension into
a cavity and whereby pressure outside and within the pneumatic
tubes may be substantially equalized so that their walls may be of
minimal thickness for compactness when collapsed and folded.
9. The inspection instrument of claim 8 wherein the cable includes
electrical conductors connectable at one end to the television
camera, and the instrument further includes electrical controls
connected to the electrical conductors and also connectable to a
source of power.
10. An instrument for inspecting elongated cavities comprising:
an inflatable base comprising two annular, conical sheets of thin,
flexible, nonelastic material, sealed at their edges, fibers having
their ends embedded in the sheets to space them apart when the base
is inflated, and a curbed sleeve fixed in the cone so that it
penetrates the top of the cone and extends from the bottom
thereof;
a strap and fastening means attached to the inflatable base, for
anchoring it to some fixed part adjacent the cavity being
inspected;
a cable having an outer sheath and tubes and electrical conductors
inside the sheath, the cable being held by the base for sliding
motion therein;
a plurality of inflatable disks fixed concentrically on the cable,
being spaced apart so that the segment of the cable between
adjacent disks is bend resistant, and each disk being in sealed
relationship with one of the tubes for inflation thereby;
a control box having a threaded cavity to receive a threaded gas
bottle, and having a main duct leading from the cavity to a
plurality of branch ducts; a puncture point in the end of the
cavity for opening a gas bottle; a valve in each branch duct; a
flow meter in each branch duct; a valve in the main duct; a
connector for connecting each branch duct to one of the tubes of
the cable; and electrical conductors attachable to a power source
and to the electrical conductors of the cable; and
a television camera on the end of the cable, opposite that which is
attached to the control box, and two mutually perpendicular step
motors attaching the camera to this cable end, for orienting the
camera.
Description
BACKGROUND OF THE INVENTION
This invention relates broadly to inspection devices, and more
specifically to those that must be very portable and extensible in
one direction for inspecting elongated cavities. The invention
herein described was made in the course of or under Contract AF
04(694)-926 with the U.S. Air Force.
Sometimes it is necessary to inspect an elongated cavity in a
substantially stationary object wherein the amount of room at the
entrance to the cavity is restricted, so that the inspection
instrument must be very compact and extensible to many times its
storable length. An example of this is an experimental solid
propellant rocket having a central bore in the propellant. When
experimental propellant is used in such a rocket, it must be
inspected periodically to assure that undesirable effects, such as
cracking, have not occurred as a result of aging. Such an effect
must be known before the rocket is fired, because the greatly
increased burning surface created by the fractures can make the
rocket potentially dangerous. If the rocket is of a type having a
plurality of thrust nozzles and an axial cavity in the propellant,
any inspection device that is supported outside such a rocket motor
would have to enter one of the nozzles and then execute two
substantially 90.degree. turns in order to enter the axial cavity.
Inspection of other types of solid propellant rocket motors having
single nozzles also is usually very difficult without removing the
motor from its storage place.
SUMMARY OF THE INVENTION
The present invention, which satisfies this need, is an inspection
instrument having an observing means supported on the outer end of
a cable that comprises a plurality of pneumatic tubes and
electrical conductors encased in a flexible sheath. This cable
passes through a sleeve, one end of which enters an inflatable
support at its base, curves through about 90.degree., and
penetrates the top of the inflatable support. The support is a
hollow cone made of two parallel layers of flexible material spaced
apart by fibers anchored in the layers or sheets, the parallel
sheets being sealed at their edges to enclose an annular, conical
volume which is to be inflated. The control end of the cable is
fastened to a control box that contains connectors to a source of
electrical power and to a source of pressurized gas. This box also
contains switches, valves, or other control means for regulating
the flow of electrical power and gas to the cable. A series of
annular, inflatable braces of nonelastic, thin, flexible material
is concentrically fixed to the cable and each is inflatable via one
of the pneumatic tubes. The inflatable support may be anchored to
the rocket or to some other stationary part by means of a
strap.
When a rocket having a plurality of nozzles and a central cavity is
to be inspected, the inflatable support is centered inside the aft
closure, anchored to the rocket by means of a strap, and inflated.
Gas is then metered into the pneumatic tube that communicates with
the interior of the inflatable brace nearest the free end of the
cable and outside the inflatable support. The desired height of the
observing device in the cavity is achieved simply by threading the
cable through the sleeve, and the inflatable braces may be inflated
serially as they emerge through the inflatable support. Rigidity is
imparted to the cable by inflating its sheath. Since this
eliminates stress on the pneumatic tubes of the cable, their walls
can be of minimal thickness for compactness when stored.
Orientation and other operations of the observation means are
accomplished by appropriate well-known devices.
Objects of the invention are to provide an instrument for
inspecting bores that is very portable; convenient to use; and that
will not damage the propellant inside the rocket motor. Important
features of the invention are that it is simple in construction,
easy to manufacture, and inexpensive to make.
Other objects, features, and advantages of the invention will
become apparent as the following description is read with reference
to the accompanying drawings, wherein the same parts are designated
with the same numbers throughout the disclosure.
DESCRIPTION OF THE DRAWINGS
FIG. 1 is a longitudinal section of a typical solid-propellant
rocket motor with the invention installed therein;
FIG. 2 is a top view of the control box;
FIG. 3 is a cross section of the control box;
FIG. 4 is a side elevation of the control box, showing the cable
connector;
FIG. 5 is a perspective detail showing both parts of the cable
connector;
FIG. 6 is a perspective detail of a typical valve; and
FIG. 7 is a side elevation of the camera and associated devices for
orienting it as desired.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
As shown in FIG. 1, the invention has a cable 10 having an outer
sheath 11 that encloses a plurality of pneumatic tubes 12 and
electrical conductors 13. Each of the pneumatic tubes 12 leads from
a bottle 14 of pressurized gas, or other source of gas, to a
specific, inflatable brace 15. One of them connects the source of
gas 14 with the inflatable base or support 26. Each inflatable
brace 15 is annular, concentrically surrounding the cable 10. It is
essentially disk shaped and is somewhat thickened at the center to
prevent buckling.
A control box 16 (FIGS. 2, 3, and 4) has a cavity 17 to receive the
gas bottle 14. A threaded orifice 18 may engage threads on the end
of the bottle 14, and a puncture point 19 ruptures a diaphragm, not
shown, in the end of the bottle 14, when the threads have engaged
sufficiently to form a gastight seal. A main duct 20 leads from the
threaded orifice 18 to a plurality of branch ducts 21, each of
which connects at its other end, via a connector 22 (See FIG. 5) to
a selected tube 12. Intermediate each branch duct 21 is a valve 23
and a flow meter 24. A detail of a valve 23 is shown in FIG. 6. It
has a through passage 23a that is alignable with a branch duct 21
in "open" position and a bleed orifice 23b alignable with a branch
duct 21 when an associated device is to be deflated. In either
case, the valve member 23c must be pressed against the spring 23d.
Each of the inflatable braces 15 is made of a thin, flexible
material that is nonelastic so that it has a fixed form when fully
inflated, and, further, has fibers 15a passing between opposite
walls to promote dimensional stability.
The cable 10 passes through a curved sleeve 25 that is fixed in a
base or support 26 having the form of a hollow cone. This hollow
cone is made of two parallel sheets 27 of thin, flexible material
that is nonelastic. They are sealed together at their top and
bottom edges to form a closed, annular, inflatable space.
Dimensional stability of the base 26 is further insured by a
multiplicity of fibers 28 that extend between the sheets 27 and are
embedded therein at their ends. Material of this nature is
commercially available. A buckle equipped strap 29 is fastened to
the base of the support 26, whereby the support 26 may be centered
and firmly attached inside the cavity 30 of the rocket motor 31.
The control box 16 also has electrical controls 32 attachable to a
source of electric power, to the television camera 33, and to its
horizontal electrical step motor 34 and vertical actuator 35,
respectively. The electrical conductors are not shown. The
television camera 33 and its step motor 34 and actuator 35 are of
types well known in the art and are commercially available.
The invention may be practiced by first threading one end of the
strap through one nozzle 36 of the rocket motor 31 and allowing it
to slide down through the opposite nozzle 36. The two ends of the
strap 29 are then adjusted until the base 26 is centrally located
as desired. This may be done by matching an index mark on the strap
29 with the edge of one of the nozzles 36. The strap 29 is then
firmly fastened in place by its buckle 37. Gas from the gas bottle
14 is then allowed to pass through the valve 23 associated with the
inflatable support 26. The cable 10 is stiffened by inflating its
sheath 11 in the same manner, and is then moved through the sleeve
25 until the first inflatable brace 15 is free of the top thereof.
This can be determined by a scale, not shown, on the cable 10,
using the edge of the nozzle 36 as an index means. The valve 23
associated with that first inflatable brace 15 is then opened and
the gas is allowed to flow until the corresponding flow meter 25
indicates that this brace 15 is fully pressurized. The remaining
inflatble braces 15 are inflated in turn as needed, in the same
manner. When the top of the cable 10 has reached the desired height
in the cavity 30, the camera 33 may be oriented as desired,
horizontally by the step motor 35 and vertically by the pneumatic
actuator 35. It may be operated by the conventional electrical
controls 32 (See FIG. 7).
When the inspection is completed, the main valve 23a is closed, the
cable 10 is withdrawn through the sleeve 25, and the inflatable
braces 15 are deflated one by one in reverse order to that of their
inflation as they approach the sleeve 25. Each valve 23 is equipped
with a discharge position for this purpose, which opens its
corresponding branch duct to the atmosphere.
The base and cable sheath 11 are then deflated in the same manner,
the buckle 37 is unfastened, and the inspection instrument is
withdrawn from the rocket motor 31.
An invention has been described that advances the art of inspecting
elongated cavities. Although the preferred embodiments have been
described with considerable specificity with regard to detail, it
should be understood that many such details may be altered without
departing from the scope of the invention as it is defined in the
following claims.
* * * * *