CA1303578C - Bellows seal - Google Patents

Bellows seal

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Publication number
CA1303578C
CA1303578C CA000496653A CA496653A CA1303578C CA 1303578 C CA1303578 C CA 1303578C CA 000496653 A CA000496653 A CA 000496653A CA 496653 A CA496653 A CA 496653A CA 1303578 C CA1303578 C CA 1303578C
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CA
Canada
Prior art keywords
bellows
pressure
seal
control apparatus
convolutions
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
CA000496653A
Other languages
French (fr)
Inventor
Anton Braun
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Individual
Original Assignee
Individual
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Publication date
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Priority to CA000496653A priority Critical patent/CA1303578C/en
Application granted granted Critical
Publication of CA1303578C publication Critical patent/CA1303578C/en
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Expired - Lifetime legal-status Critical Current

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  • Reciprocating Pumps (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Abstract

ABSTRACT
A bellows seal apparatus for use in compressors or the like which has pump means arranged and controlled to maintain a desired pressure differential between the inside and outside surfaces of the bellows. It also has a driving mechanism having a connection with a movable end of the bellows and an additional connection or connections with said bellows at unequally spaced points intermediate to the ends of the bellows to provide the least maximum stress levels in the bellows convolutions of each and thus the maximum life expectancy for the seal. The driving mechanism may take many forms but is so designed that it will elongate and contract each section of the bellows a distance depending upon the dynamically caused stresses in each section and the composition of and the number of bellows convolutions in each section.

Description

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Description BELLOWS SEAL
Technical Field This invention relates to hermetic type seals for recipro-cating shaft mechanisms.
The invention is of general utili-ty but of particular utility in sterling engines and heat pump apparatus or systems wherein loss of refrigerant vapor or system gas is to be avoided.
With the system operating or at rest, the high vapor pressure of the refrigerant results in leakage through conventional shaft seals. A diaphragm or a bellows seal avoids such leakage.
However, for example, the high pressure on the outer surface of a thin flexible bellows, the interior of which is at ambient or atmospheric pressure, in combination with ~he stresses caused by the expansion and contractLon of the bellows, causes distortion and rapid failure of the seal.
The present invention avoids this and other difficulties and disadvantages by providing means for controlling the pressure differential between the inside and outside of flexible seals, such as the inside and outside of a bellows type of seal, and by keeping maximum stress levels in each section caused by expansion and contraction to a minimum by appropriate division of the bellows and proper selection of the number of convolutions in each section and appropriate seleceion of the driving means for eaoh section, as will now be described.

In the drawing, Figure 1 is a schematic longitudinal section taken at Sec-tion 1-1 of Figures 2-4 showing one embodiment of the invention as applied to the compressor mechanism of a heat pump, Figures 2, 3 and 4 are partial sectional views taken at sections 2-2, 3-3 and 4-4 of Figure 1, Figure 5 is a partial sectional elevation at Section 5-5 of Figure 4, :

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Figure 6 is a schematic longitudinal section of a second embodiment of the invention taken at Section 6-6 of Figure 8, Figure 7 represents Section 7-7 of Figure 8, Figure 8 represents Section 8-8 of the structure of Figure 5 6, Figure 9 is a schematic longitudinal section of another embodiment of the invention, Figure 10 is a section taken at line 10-10 of Figure 9, Figure 11 is a section taken along line 11-11 ln Figure 9, Figure 12 is a partial sectional view of a further embodiment of the invention, Figure 13 is a schematic view of another embodiment, Figure 14 is a sectional view taken along line 14-14 in Figure 13, Figure 15 is a sectional view taken along line 15-15 in Figure 14, and Figure 16 is a fragmentary view of a compressor piston having two shafts for driving auxiliary pumps.
In Figures 1-5, piston 10 on shaft 11 operates within a cylinder 12 in a housing section 9a and actuates a sub-shaft 13 connected to a piston 14 of a sub-ambient or vacuum pump 15. Bellows 16, within a chamber 17, is sealed at its upper end to shaft 11 and at its l.ower end to a wall extending between chamber 17 and housing wall ~b and forms a hermetic seal between chamber 12b and the ambient A ~ ~

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atmosphere in the bellows which through its open end, is exposed to ambient pressure in housing section 9c. The bellows operates concurrently with the shaft, which extends through a gland type of seal lla in the wall 12c, the maximum mechanical stress due to expansion and contraction of the convolutions of the bellows are drastically reduced by a lever and tube apparatus 18 in housing section 9c, as described in my U.S. Patent No. 4,424,008.
Stresses normally introduced by diEferential pressure are -2a -. .

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neutralized in accordance with one of the principles of this invention, as will now be described.
The pu~lp 15 is connected to sub-ambient pressure or vacuum chamber or chambers 19 through passageway or line 15a, valve 22 and a check valve 14a. Vacuum established during operation of the the machine is maintained in chamber 19 during shutdown by closing valve 22. The chamber 19 need be only large enough to provide for the starting of the engine, as described hereinafter.
The pump needs only to have enough capacity to provide sufficient 10 vacuum to relieve excessive pressure in chamber 17 during oper-ation of the engine and to quickly store a vacuum in chamber 19 for starting purposes in case the compressor is subject to short periods of operation. A line 20 connects chamber 19 to a sleeve or plunger valve 21. Valve 21 connects with the bellows 15 chamber 17 through a maniEold 23 and line 17a and with cylinder chamber 12b through line 24 which is restricted by an orifice 25.
A plunger or piston 26, which has at least one bore 26a there-through, is self-adjusting to variations in pressure around bellows 16 through bore or bores 26a by a rod connection with a 20 control bellows 27 located in housing section 9b or 9c or in the atmosphere.
During rest periods, piston 10 is forced to the expansion or lower position by the pressure of the gas or refrigerant in chamber 12a, and the bellows 16 is compressed and may be exposed 25 to full gas or vapor pressure, due to leaking by seal lla and plunger 26. At startup, valve 22 is opened causing the pressure around bellows 16 to be immediately reduced appro~imately to ambient. During operation of the compressor, high pressure in the bellows 27 causes the valve 21 to open line 20a to the vacuum 30 chamber, which is kept evacuated by the pump 15; low pressure in bellows 27 conversely causes valve 21 to shut off or close line 20a and connect chamber 17 through manifold 23, line 24 and orifice 25 to the higher pressure chamber 12b, and the pressure around bellows 16 is thus maintained substantially ambient.
The lines 15a and 20 in Figure 1 connect with the lines l5a . ~ ,............. . .

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and 20 in Figure 5 and the valve 26 is illustrated as being in its neutral position across both lines 20a and 24. In operation, plunger or piston 26 will constantly move back and forth as the bellows 27 responds to increases and decreases in pressure in chamber 17. The pressure in 12b will always be somewhat higher than ambient or atmospheric, inside of bellows 16 and housing section 9c, due to vapor pressure of the refrigerant being pumped, the principle use of the invention. However, the line 24 could be connec-ted to chamber 12a rather than chamber 12b.
While the primary function of the pump and vacuum chambers is to relieve pressure in chamber 17 to approximately that in the bellows, residual vacuum in the chambers 19 is also useful in starting the engine/compressor. A line (not shown) to chamber 12a frorn the vacuum chambers may be briefly opened to lower the cylinder pressure and draw the piston 10 toward its compressor top dead center position, which action also puts a charge in the cylinder of the prime mover. The closing of the line, thus allowing the vapor pressure in chamber 12a to build up again, will aid in the return of piston lO back toward its bottom dead center position, thereby compressing the charge in the prime mover sufficiently for firing. Means may be pro-vided to move the piston in either or both directions for starting purposes, and a positive (soft) seal may be provided around shafts ll and 13 and check valve 14c and line 24 to prevent leakage when the compressor is at rest to reduce the size or eliminate the need for chambers 19.
It will be seen that the entire apparatus may be self-contained with vacuum pump, plunger valve and vacuum chambers all located within the housing of the compressor which, however, is of somewhat extended length in the form of Figures 1-5. A
more compact modification is shown in Figures 6-8. Here the bellows 116 is sealed dlrectly to the piston 110 and to the lower end wall 112c of the cylinder 112. The action of the bellows is controlled by a lazytongs 130 of crossed links 130a, 130b and 130c, attached to a support ring 131, extending from convolutions of the bellows. Crossed links 130a are normally ?3~7~1 long for large intervals and links 130c are short Eor shorter intervals. ~acuum pump 115 evacuates vacuum chambers 119, which may have connections through appropriate valves and lines (not shown) to the cylinder 112 above and below piston 110 in a manner and for purposes already described with respect to Figures 1-6.
A second principle of the invention lies in having the number of identical convolutions in each of a plurality of sections of the bellows seal decrease sequentially from the fixed end of the bellows to the movable end-thereof according to the formula:
~2 = 52 NT ST
Where N2 is the number of convolutions in one of a plural-ity of sections oE a bellows, NT :is the total number of identical convolutions in the entire bellows, S2 is the amount of elon-gation or contraction of the section, ST is the total elongationor contraction of the entire bellows during operation of the machine in which the seal is used.
Another advantage of the system of Figures 6-~ lies in the reduced diameter of the bellows, made possible by placing the mechanism for actuating the intermediate portion or portions of the bellows on the outside of the bellows.
Since the pressure on the outside and inside surfaces of the bellows is regulated by the action of the plunger valve 21 to approximately ambient and since a significantly lower pressure is maintained by the pump 115 in the vacuum chambers, startup is easily accomplished as previously indicated.
; Another embodiment of the invention is shown in Figures 9-11. It has a bellows seal arrangement similar to that of Figures 1-5 but having unequal length bellows sections 216a, 216b and 216c with unequal length levers 230a, 230b and 230c for the actuating mechanism between the piston rod and the cylinder.
The intermediate portions of the bellows are connected to , ~3~3~7~

short guide sleeves 231 that are slidable on guide rods 232.
A still further embodiment of the inVentiOn is shown in Figure 12 wherein bellows 316 is connected to the compressor piston, and intermediate portions of the bellows are connected to externally located driving links through short guide sleeves around movable guide rods 332 connected to piston 310 on opposite sides of the bellows. This provides a more compact arrangement than in the modification of Figures 9~
The modification of Figures 13-15 makes use of a pair of racks, one, 418, connected to piston 410 and the other9 419, connected to intermediate portion 431 of the bellows 416 and a large diameter gear 430a engaging rack 418 and an integral or attached smaller diameter gear 430b engaging the rack 419.
This arrangement provides the same relative movements between the bellows sections as in the other modifications.
Figure 16 shows how a compressor piston 510 may be designed to actuate pump shafts 513 through a cylinder end wàll 512c and seat on a soft pad 512d to prevent leakage through the wall around the shafts and piston rod.
It is to be understood that other modifications of the invention could have the ambient pressure on the outside of the bellows seal with the inside being exposed to the variable pressure and controlled in a similar manner. Also, in some applications of the invention, it may be desirable to have a differential in pressures other than ambient on opposite sides of the bellows seal so long as they are controlled p'essures.

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Claims (18)

1. Control apparatus for a bellows-type of hermetic seal around a reciprocable shaft, said seal having a fixed open end and a movable end and having an inside surface exposed to ambient pressure around said apparatus and an outside surface and being contained within a pressure chamber providing external pressure on said seal and being subject to potentially harmful differentials between external pressures and internal pressures, said apparatus comprising a first means for establishing a sub-ambient pressure and valve means for connecting said sub-ambient pressure in said first means to one of said surfaces when pressure thereon is higher than desired with respect to the pressure on the other side, whereby the pressure differential between the pressures inside and outside of said bellows seal is maintained at the desired level and means to concurrently actuate said movable end and an intermediate portion of the seal.
2. Control apparatus as defined in Claim 1, wherein said first means comprises an evacuating pump.
3. Apparatus as defined in Claim 1, wherein said shaft is attached to a piston of a compressor and said valve means is movable to connect said one surface to a source of higher pressure when the pressure on said one surface is lower than a desired pressure with respect to the other side.
4. The apparatus of Claim 3, wherein said first means comprises a reciprocating evacuating pump having a shaft parallel to and reciprocating with said reciprocating shaft and being connected to a lower than ambient pressure chamber.
5. The apparatus of Claim 1, wherein said shaft is attached to a piston in a compression cylinder and said cylinder serves as said chamber.
6. Apparatus as defined in Claim 3, wherein said piston serves as said first means.
7. The apparatus system of Claim 1, wherein said bellows includes a plurality of intermediate concurrently actuated portions dividing said bellows into sections of convolutions.
8. The apparatus as defined in Claim 7, wherein said reducing means comprises a lazytongs type of mechanism extending between said piston and a partition wall of said cylinder and being attached to at least one of the intermediate portions of said bellows.
9. Control apparatus as defined in Claim 1, wherein said one of said surfaces is the outside surface of said seal.
10. Control apparatus as defined in Claim 1, wherein said shaft extends through a gland-type of seal into said pressure chamber.
11. Control apparatus as defined in Claim 8, wherein axially spaced pairs of lazytong links are of different lengths.
12. Control apparatus for a bellows seal on a reciprocable shaft comprising means for substantially balancing gas pressures on the inside and the outside surfaces of the bellows seal, means for dividing convolutions of the bellows seal into a plurality of sections of unequal numbers of convolutions which sections decrease in number of convolutions sequentially from a fixed end of the bellows seal to a movable end thereof, and movable driving means extending between said shaft and said movable end and between said shaft and the means dividing the convolution sections to concurrently actuate said movable driving means when said shaft is moved so as to elongate or shorten the length of each section an amount substantially proportional to the number of convolutions in each section.
13. Control apparatus as defined in Claim 12, wherein the ratio of the number of convolutions in any bellows section to the total number of convolutions is substantially equal to the ratio of the elongation or contraction of any bellows section to the total elongation or contraction of the bellows.
14. Control apparatus as defined in Claim 12, wherein said means for actuating intermediate sections of said bellows includes racks and pinions.
15. Control apparatus as defined in Claim 12, wherein said bellows seal has one end thereof sealingly connected to a compressor piston and the other end thereof sealingly connected to the wall of a cylinder surrounding said piston.
16. Control apparatus as defined in Claim 12, wherein said means for balancing gas pressures includes means for varying the pressure on at least the higher pressure side of said bellow's convolutions.
17. Control apparatus as defined in Claim 1, wherein said valve means is controlled by means responsive to pressure on said one side of said bellows.
18. Control apparatus as defined in Claim 17, wherein said valve means is operable to connect said one side of said seal to either said first means or to a higher than ambient pressure source.
CA000496653A 1985-12-02 1985-12-02 Bellows seal Expired - Lifetime CA1303578C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA000496653A CA1303578C (en) 1985-12-02 1985-12-02 Bellows seal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA000496653A CA1303578C (en) 1985-12-02 1985-12-02 Bellows seal

Publications (1)

Publication Number Publication Date
CA1303578C true CA1303578C (en) 1992-06-16

Family

ID=4131993

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000496653A Expired - Lifetime CA1303578C (en) 1985-12-02 1985-12-02 Bellows seal

Country Status (1)

Country Link
CA (1) CA1303578C (en)

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