FLUID TRANSFER TUBE

Abstract

A fluid transfer tube having a probe tube having first and second ends, the first end having at least one fluid transfer entrance port, the second end having at least one fluid transfer exit port, and an anti-cavitation fin extending from said first end to said second end.

Claims

1. A fluid transfer tube comprising: a probe tube having first and second ends, said first end having at least one fluid transfer entrance port, said second end having at least one fluid transfer exit port, and an anti-cavitation fin extending from said first end to said second end.

2. The fluid transfer tube of claim 1, having at least two fluid transfer entrance ports.

3. The fluid transfer tube of claim 1, having at least two fluid transfer exit ports.

4. The fluid transfer tube of claim 1 further comprising: an air exchange tube.

5. The fluid transfer tube of claim 4 wherein said air exchange tube includes at least one entrance port and one exit port.

6. The fluid transfer tube of claim 1 wherein said anti-cavitation fin has a thickness which is in the range of 1%-5% of the diameter of the probe tube.

7. The fluid transfer tube of claim 4 wherein said air exchange tube diameter is in the range of 1%-45% of the diameter of the probe tube.

8. A fin and air tube assembly comprising: an anti-cavitation fin; and an air exchange tube.

9. The fin and air tube assembly of claim 8, wherein said anti-cavitation fin has a thickness which is in the range of 1%-5% of the probe tube.

10. The fin and air tube assembly of claim 8, wherein air exchange tube air exchange tube diameter is in the range of 1% to 45% of the diameter of the probe tube.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0014] The purposes and advantages of the present invention will be apparent from the following detailed description in conjunction with the appended drawings in which:

[0015] FIG. 1 shows a fueled device, specifically a chain saw, being refueled using a volatile fluid transfer device which includes the present fluid transfer tube;

[0016] FIG. 2 shows an isometric view of the fluid transfer tube of the present invention;

[0017] FIG. 3 shows a cut-away isometric view of the fluid transfer tube of the present invention;

[0018] FIG. 4 shows another isometric view of the fluid transfer tube of the present invention; and

[0019] FIG. 5 shows another cut-away isometric view of the fluid transfer tube of the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0020] The present invention is a fluid transfer tube 10. It is preferably used in a volatile liquids refueling apparatus as disclosed in U.S. patent application Ser. No. 15/449,985, filed Mar. 5, 2017, which is incorporated by reference herewithin, by one of the present inventors.

[0021] This apparatus has a probe which engages a fuel tank and a receiver which makes a vapor-tight connection to a fueled device, such as a chain saw, for use in situations in which volatile vapors could be ignited if not contained. Within this apparatus is a connecting tube, referred to as central tube 40 in this previous patent application. The present fluid transfer tube 10 can replace this previous central tube as a mechanism for providing faster fluid transfer rates by reducing turbulence and cavitation. It is emphasized that this present fluid transfer tube 10 is not limited to this one application and that it can be used in a variety of applications where improved fluid transfer rate is desireable. For the sake of this discussion, it will be assumed that the fluid transfer tube is being used with the previously described volatile liquids refueling apparatus. Moreover, the internal mechanism which acts to provide the improved fluid transfer rate, discussed later as fin and air exchange tube assembly 40, can be used in various other application which do not use the particular tube configuration described below.

[0022] Referring now to FIG. 1, a fueled mechanical device 1 is shown, which in this case is a chain saw 2, having a device fuel tank 3 with a device fuel tank port 4. An external fuel tank 5 has a fuel tank port 6, and a volatile liquids refueling device 7 is shown attached between the external fuel tank port 6 and the device fuel tank port 4, as refueling is conducted. The present fluid transfer tube 10 is included in the volatile liquids refueling device 7 to provide increased fluid transfer rates and faster refueling times.

[0023] Referring to FIGS. 2-5, the fluid transfer tube 10 generally includes a probe 12, having a probe tube 14. This probe tube 14 has a proximal end 16 and a distal end 18, where the proximal end 16 has male screw threads 20 which engage with female screw threads 6 on a fuel tank 5 or with an adaptor (not shown) with internal female threads and external male threads which engage female threads on a fuel tank 5. The probe tube has an exterior surface 22, and an inner bore 24 which encloses an anti-cavitation fin 26. The probe tube 14 has at least one fluid entrance port 28 located at the proximal end 16, and at least one fluid exit port 30 located at the distal end 18 of the probe tube 14.

[0024] The anti-cavitation fin 26 extends in the interior of probe tube 14 from the proximal end 16 to the distal end 18 of the fluid transfer tube 10. Cavitation is the formation of vapour cavities in a liquid, that usually occur when a liquid is subjected to rapid changes of pressure that cause the formation of cavities in the liquid where the pressure is relatively low. When subjected to higher pressure, the voids implode and can generate shock waves that cause turbulence. This opposes the smooth flow of fluid and reduces flow rates. By contrast, flow that is smooth or laminar, without turbulence, can be much more efficient in transferring fluid and produces higher flow rates. The anti-cavitation fin 26 is very effective in maintaining laminar flow and thus improving the fluid flow rate. The thickness of the fin anti-cavitation 26 is preferably in the range of 1% to 5% of the probe tube 12

[0025] The fluid transfer tube 10 also preferably includes an anti-cavitation air exchange tube 32, by which air in the fueled device's tank is allowed to escape, thus decreasing opposing pressure and aiding in the increased rate of fuel transfer. This is considered to be an optional feature, and the fluid transfer tube 10 will provide increased rate of transfer with the anti-cavitation fin 26 alone, but this is enhanced by use of the air exchange tube 32.

[0026] The air exchange tube 32 has an air flow pattern that is opposite to the incoming fluid flow, and so has one or more entrance ports 34 near the distal end 18 of the tube 12. The air flow path then leads to the exit port 36 near the proximal end 16 of the tube. This flow pattern works on a fluid exchange principle, instead of a displacement principle, which produces faster fluid transfer rates.

[0027] It has been found that a desirable diameter for this air exchange tube 32 is 1 to 45% of the main tube 12 diameter, with a thickness of 0.010 to 0.05 inches.

[0028] It is thought that the anti-cavitation fin 26 and air exchange tube 32 may be used as an fin and tube assembly 40 in other tubes in which it is desirable to maintain laminar flow with reduced turbulence and cavitation. Thus, this fin and tube assembly 40 may be fabricated as an insert that may be placed in other types of tubes or short hoses.

[0029] While various embodiments have been described above, it should be understood that they have been presented by way of example only, and not limitation.