U.S. patent number 3,602,602 [Application Number 04/825,724] was granted by the patent office on 1971-08-31 for burst containment means.
This patent grant is currently assigned to Avco Corporation. Invention is credited to Salvatore Motta.
United States Patent |
3,602,602 |
Motta |
August 31, 1971 |
BURST CONTAINMENT MEANS
Abstract
The invention relates to a means for containing burst fragments
generated when very high speed machinery, particularly gas
turbines, rupture. The containment means is a winding of tape over
the machinery housing and radially aligned along the expected path
of travel of part fragments. The winding is formed from lightweight
material having high strength and high elongation properties
providing unusual energy absorbing capabilities which tends to
contain the impact of burst fragments primarily by deflection
rather than high yield stresses.
Inventors: |
Motta; Salvatore (Lowell,
MA) |
Assignee: |
Avco Corporation (Cincinnati,
OH)
|
Family
ID: |
25244764 |
Appl.
No.: |
04/825,724 |
Filed: |
May 19, 1969 |
Current U.S.
Class: |
415/9; 415/197;
74/608 |
Current CPC
Class: |
F01D
21/045 (20130101); Y10T 74/219 (20150115) |
Current International
Class: |
F01D
21/00 (20060101); F01D 21/04 (20060101); F16p
001/02 () |
Field of
Search: |
;74/608,609
;415/9,196,174,121,197 ;416/241 ;164/152,161,227
;156/180,181,184,186,187,188,189 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Raduazo; Henry F.
Claims
The various features and advantages of the invention are thought to
be clear from the foregoing description. Various other features and
advantages not specifically enumerated will undoubtedly occur to
those versed in the art, as likewise will many variations and
modifications of the preferred embodiment illustrated, all of which
may be achieved without departing from the spirit and scope of the
invention as defined by the following claims:
1. A burst containment means comprising the combination of a
housing about a rotated bladed structure, a winding on said housing
consisting essentially of at least 15 overlapping turns of a tape
formed from a nylon ballistic material having a specific energy
absorbing capability of at least 200,000 (IN-LB/LB).
2. A burst containment means as defined in claim 1 in which the
winding is formed from a woven tape of a nylon ballistic material.
Description
The containment means described is used for the purpose of
containing burst fragments within a localized area in the event the
rotor of a very high speed machine ruptures. The invention has
immediate application to the compressor section of gas turbines and
can be further extended to the turbine section following the
development of a high temperature and high elongation plastic fiber
such as a high temperature nylon known as "Norel" for example.
In the past a metal, usually steel, in a single mass, laminated or
woven form has been used. In one respect steel would appear to be
an excellent candidate. In practice, particularly in aviation gas
turbine applications, it is practically useless for a rather
unusual reason, to be demonstrated.
It is an object of the invention to provide a burst containment
means for high energy fragments which (i) avoids the limitations
and disadvantages of prior art devices, (ii) is lightweight and
compact, (iii) made from material which is capable of absorbing at
least twice as much kinetic energy as steel of the same weight,
(iv) is constructed from a nylon tape material having a high
strength to failure ratio, and (v) comprises a winding of at least
15 turns of tape.
In accordance with the invention a burst containment means
comprises a housing, a winding made up of at least 15 overlying
turns of a tape formed from a material having a specific energy
absorbing capability of at least 200,000 (IN-LB/LB).
The novel features that are considered characteristic of the
invention are set forth in the appended claims; the invention
itself, however, both as to its organization and method of
operation, together with additional objects and advantages thereof,
will best be understood from the following description of a
specific embodiment when read in conjunction with the accompanying
drawings, in which:
FIG. 1 is a partial cross-sectional representation of a burst
containment means embodying the principles of the present
invention;
FIG. 2 is a schematic representation of the winding comprising a
portion of the burst containment means;
FIG. 3 is an expanded segmented view of the burst containment means
showing structural details; and
FIG. 4 is a pictorial representation of the invention in the act of
restraining high kinetic energy fragments.
The energy absorbing capability of a material is determined by
reference to a standard stress-strain curve of the material where
stress is specified in LB/IN.sup.2 and the strain in IN/IN. The
energy absorbing capability of a material is determined by
calculating the area under the stress-strain curve.
In tests conducted on a nylon ballistic cloth material the energy
absorbing capability of the material was determined to be 8,000
(IN-LB/IN.sup.3). The energy absorbing capability of steel that was
considered suitable for fragment containment was determined to be
35,000 (IN-LB/IN.sup.3). It would appear from the foregoing that
steel is much more suited for fragment containment than the nylon
cloth. The fact of the matter is, however, that it is, from a
practical point of view, much worse. For one thing, steel, because
it has a high modulus of elasticity, tends to resist an impact with
negligible deflection and consequently it tends to shatter rather
than absorb energy.
Another very serious limitation of steel is its weight. For
example, the specific energy absorbing capability, i.e. the energy
that a material can absorb per pound of material, of steel is
121,000 (IN-LB/LB.) The specific energy absorbing capability of
nylon, on the other hand, is 204,000 (IN-LB/LB) and is in fact a
preferred candidate material.
The low strength material is utilized to its fullest capability
when it is wound into a coil or winding containing at least 15
turns for reasons that will be explained hereinafter.
Referring to FIG. 1 of the drawings there is illustrated in cross
section the pertinent elements of a gas turbine compressor assembly
10. The assembly includes a hub 11 on the circumference of which
are fastened a plurality of compressor blades 12. Surrounding and
spaced from the compressor blades 12 is a housing 13 formed from
any suitable metal material.
Lapped around the housing 13 is a winding 14 comprising at least 15
turns 16.
The turns 16 are formed from a continuous length of a material
having a specific energy absorbing capability of 200,000 (IN-LB/LB)
or greater. A nylon ballistic cloth as defined and identified in
the Mill Standard specification Mil-C123690 is the preferred
material to use in making up the winding of 14.
FIG. 2 is a schematic representation showing the use of a
continuous tape in making up the winding 14. It also represents
schematically that there are no means for bonding or fastening the
adjacent turns 16 of the winding 14 to each other or to the housing
13.
FIG. 3 is another representation of the winding structure providing
additional detail.
FIG. 4 of the drawings serves to illustrate why it is important to
(1) provide a plurality of turns 16 preferably a minimum of 15
turns, and (2) provide a winding where adjacent turns are free to
move relative to each other. FIG. 4 illustrates the winding 14 in
the process of absorbing three high energy fragments from an
exploding mechanical member. The housing 11 has been completely
shattered and is no longer a factor in containing the fragments.
The configuration of the winding 14 has changed into an optimum
configuration for the type of impact it is resisting. The wide
center portion 19 of the three legs of the winding indicate that a
number of turns 16 of the winding 14 have failed in tension. The
high density of turns 16 adjacent to the outside of the winding 14
indicate that a substantial number of turns 16 are compressed and
absorbing the energy applied to the winding by the fragments.
It is clear that the amount of energy that is to be contained will
vary with the speed and the configuration of the high energy
fragments. The primary use of the housing relates to its function
in connection with the gas turbine compressor. Its very presence
causes it to absorb some of the energy from fragments; but because
it is made of metal and because its thickness is determined by the
gas turbine performance, it is not a good energy absorber and in
fact the major portion of the energy contained in a fragment is
absorbed by the winding 14. On occasion it has been noted that the
housing upon rupturing creates secondary high energy fragments but
generally these do not pose a serious problem.
A number of tests have been made by preparing a 3 -inch wide
winding over an 18 -inch diameter housing. Each turn was one
thirty-second inch thick and 331/3 turns were used to make up the
complete winding. This particular design has successfully resisted
impact up to and including 83,500 IN-lbs. Up to 40 percent of the
turns experienced one or more breaks. These breaks were examined
and were determined to be tension breaks. The "intact" turns
underwent appreciable elongation. High energy fragments were
completely contained in the windings.
* * * * *