GB2541931A - Fluid transfer coupler - Google Patents

Fluid transfer coupler Download PDF

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Publication number
GB2541931A
GB2541931A GB1515737.3A GB201515737A GB2541931A GB 2541931 A GB2541931 A GB 2541931A GB 201515737 A GB201515737 A GB 201515737A GB 2541931 A GB2541931 A GB 2541931A
Authority
GB
United Kingdom
Prior art keywords
fluid transfer
coupler
transfer coupler
spindle
crank member
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.)
Withdrawn
Application number
GB1515737.3A
Other versions
GB201515737D0 (en
Inventor
Ashton Colin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fort Valve Engineering Ltd
Original Assignee
Fort Valve Engineering Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Fort Valve Engineering Ltd filed Critical Fort Valve Engineering Ltd
Priority to GB1515737.3A priority Critical patent/GB2541931A/en
Publication of GB201515737D0 publication Critical patent/GB201515737D0/en
Priority to PCT/GB2016/052689 priority patent/WO2017037447A1/en
Publication of GB2541931A publication Critical patent/GB2541931A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L37/00Couplings of the quick-acting type
    • F16L37/28Couplings of the quick-acting type with fluid cut-off means
    • F16L37/38Couplings of the quick-acting type with fluid cut-off means with fluid cut-off means in only one of the two pipe-end fittings
    • F16L37/47Couplings of the quick-acting type with fluid cut-off means with fluid cut-off means in only one of the two pipe-end fittings with a tap or cock
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03Fuel tanks
    • B60K15/04Tank inlets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B67OPENING, CLOSING OR CLEANING BOTTLES, JARS OR SIMILAR CONTAINERS; LIQUID HANDLING
    • B67DDISPENSING, DELIVERING OR TRANSFERRING LIQUIDS, NOT OTHERWISE PROVIDED FOR
    • B67D7/00Apparatus or devices for transferring liquids from bulk storage containers or reservoirs into vehicles or into portable containers, e.g. for retail sale purposes
    • B67D7/06Details or accessories
    • B67D7/36Arrangements of flow- or pressure-control valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00Actuating devices; Operating means; Releasing devices
    • F16K31/44Mechanical actuating means
    • F16K31/52Mechanical actuating means with crank, eccentric, or cam
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L37/00Couplings of the quick-acting type
    • F16L37/24Couplings of the quick-acting type in which the connection is made by inserting one member axially into the other and rotating it to a limited extent, e.g. with bayonet action
    • F16L37/244Couplings of the quick-acting type in which the connection is made by inserting one member axially into the other and rotating it to a limited extent, e.g. with bayonet action the coupling being co-axial with the pipe

Abstract

A fluid transfer coupler comprises engagement means, such as a frusto-conical flange 16, for releasable engagement with a complementarily shaped fitting and retaining means 18 configured to releasably retain the complementarily shaped fitting. It also has a valve seat 24, valve closure means 22 releasably engagable with the valve seat and a crank member (32, Fig.2b). It also has means such as a handle (36, Fig.2b) for rotatably displacing the crank member around its rotational axis and a connecting member 26 pivotally connected to the crank member and connected to the valve closure means 22. The crank member is mounted on separate first end second coaxial spindle members 34, 60 which define the rotational axis of the crank member. The coupler may be a refueling coupler for transferring fuel from a storage tank to a road tanker.

Description

FLUID TRANSFER COUPLER
The present invention relates to fluid transfer couplers. In particular, but not exclusively, the invention relates to refuelling couplers.
When transferring fuel from a storage tank to a road tanker, the fuel is dispensed along a loading arm to the outer end of which a refuelling coupler Is connected. The refuelling coupler comprises a female fitting which can be reieasabiv and sealingly coupled to a complementariiy shaped male fitting for receipt of fuel into the storage tank. The male fitting is provided with a circumferential recess Into which one or more retaining members mounted on the female fitting can be releasably located, in order to secure the male and female components together. This can be achieved by, for example, manually actuated cam locks or automatically engaging triggers mounted on the refuelling coupler. Typically, both the male and female components are also provided with a valve in order to minimise escape of fuel vapour during connection and disconnection.
One example of s known refuelling coupler is shown in Figs 5 and 8. The refuelling coupler comprises an outer generally cylindrical outer housing 210 and a generally coaxial cylindrical Inner housing 212 slidably disposed through a predetermined displacement within, and coaxially with, the outer housing 210 along the longitudinal axis of the outer housing 210. One end of the inner housing 212 is provided with a plurality of bolts 214 for attachment to an end of a fuel transfer loading arm, the other end of which is connected to a storage tank {not shown). The opposite end of the inner housing is formed into a frusto-conical flange 216 for receipt of the end of a male fitting (not shown). The inner housing 212 is also provided with four equally angularly spaced spring-loaded locking triggers 218 which, in use, are received in a circumferential recess in the male fitting (not shown). In use, as the female fitting is manoeuvred onto the male fitting, the triggers 218 snap into position and are received in the circumferential recess in the male fitting, and holds the two fittings in sealing engagement with each other. The spring-loaded locking triggers 218 ran be released by operation of a release handle 220 which is pivotally connected to the upper end of the outer housing 210 at pivots 211.
The inner housing 212 also carries a poppet valve 222 which is movable into and out of engagement with an annular valve seat 224 by means of a lever arm 226, As best seen in Fig 6, the lower end of the lever arm 226 is pivotally connected between two lugs 228 on the rear face of the poppet and the opposite end is pivotally connected between two lugs 230 of a spiined crank block 232. The spiined aperture of the crank block 232 receives a spiined portion of a spindle 234 which is pivotally mounted In the inner housing 212 and which is rotatable by means of a handle 236 attached to the end of the spindle which extends out of the inner housing 212. The opposite end of the handle Is rotatably mounted in the wall of the inner housing 212 at a location diametrically opposite the mounting of the handle 236.
As best seen in Fig 6, It is necessary for the lever arm 226 to be bent so that it extends around the spindle 234, to allow the spindle and lever arm to move without interfering with each other. However, the use of a bent lever arm has the result that the force applied to the poppet 222 from the lever arm is in a direction inclined to the opening and closing directions of the poppet. Whilst the rear face of the head of the poppet 222 is provided with three elongate extensions 238 In slidable engagement with the Inner wail of the inner housing 212 In order to guide the movement of the poppet, the bent lever arm can result in Imperfect sealing of the poppet with its valve seat and also requires an additional force to open and close the poppet.
It is an aim of the present invention to overcome or alleviate the problems associated with the prior art.
In accordance with the present invention, a fluid transfer coupler comprises: engagement means for releasable engagement with a compiementarily shaped fitting; retaining means configured to releasably retain the complemeniariiy shaped fitting; a valve seat; valve closure means releasably engageable with the valve seat; a crank member mounted on separate first and second coaxial spindle members which define the rotational axis of the crank member; means for rotatably displacing the crank member around its rotational axis; and a connecting member pivotally connected to the crank member and connected to the valve closure means.
By mounting the crank member on two separate coaxial spindle members, it is no longer necessary for a single spindle to extend across the width of the coupler. Consequently, it is not necessary for the connecting member to be bent in order to prevent interference with the spindle.
It Is therefore possible to use a straight connecting member, with the result that the forces which retain the valve closure means in the opened and closed positions are applied in substantially the direction of movement of the valve closure means. This reduces the forces required to retain the valve closure means in the opened and dosed positions, It also assists in seating the valve closure means correctly on the valve seat and reduces the likelihood of the valve closure means being displaced from the valve seat in the event of vibration.
Preferably, the connecting member is pivotally connected to the valve closure means.
Preferably, the connecting member is elongate and more preferably the connecting member is substantially straight.
Preferably, the crank member comprises a recess for receipt of a portion of the connecting member, preferably when the valve closure means is engaged with the valve seat.
The recess can be located between the inner ends of the two spindle members, with the result that is no longer necessary for the connecting member to be bent in order to fit around a spindle extending across the width of the coupler.
In one embodiment, the means for rotatably displacing the crank member around its rotational axis is connected to the first spindle.
The means for rotatably displacing the crank member around its rotational axis may comprise a handle.
In one embodiment, the first spindle member Is rotatably mounted and the crank member rotates with the first spindle member.
The second spindle member may comprise a stub spindle.
The fluid transfer coupler may further comprise a housing on which the first and second spindle members are mounted and in which the valve seat is located.
The housing may comprise an inner housing means and an outer housing means.
The first and second spindle members may be mounted on the inner housing means and the valve seat may be located in the inner housing means. in one embodiment, the valve closure means comprises a poppet valve.
By way of example only, a specific embodiment of the present invention will now be described with reference to the accompanying drawings in which:
Fig 1 is a perspective view of an embodiment of refueiiing coupler in accordance with the present invention;
Figs 2 (a) to 2 id) are a side view, cross-sectional view looking in the direction of arrows B-B, cross-sectional view looking in the direction of arrows D-D and an end view looking in the direction of arrow E of the refueiiing coupler of Fig 1, shown in a dosed configuration;
Figs 3 (a) to (d) are views corresponding to Figs 2 (a) to 2 (d). shown in an opened configuration;
Figs 4 (a) to (b) of perspective views from the front one side and above and from the rear and one side of a crank block which forms part of the refuaiiing coupler of Fig 1;
Fig 5 is a perspective view of an example of refuelling coupler known from the prior art; and
Fig 6 is a cross-section through the refuelling coupler shown in Fig 5.
The refuelling coupler shown in Figs 1 to 4 is similar in general construction to the prior art refuelling coupler shown in Figs 5 and 8. The main difference relates to the lever arm, as will be explained.
The embodiment of refuelling coupler shown In Figs 1 to 4 comprises a generally cylindrical outer housing 10 and a generally coaxial cylindrical inner housing 12 slidably disposed through a predetermined displacement within the outer housing 10 along the longitudinal axis of the outer housing 10. A plurality of bolts 14 extend perpendicularly from one end of the inner housing 12, for attachment to an end of a fuel transfer hose, the other end of which is connected to a delivery tanker (not shown). The opposite end of the inner housing is formed into an engagement means in the form of a frusto-conical flange 18 for receipt of the end of a complerneniahiy shaped male fitting (not shown). The Inner housing 12 is also provided with four equally angularly spaced spring-loaded locking triggers 18 which, in use, are received in a circumferential recess in the male fitting (not shown), In use, as the female fitting is manoeuvred onto the male fitting, the triggers 18 snap into position and are received in the circumferential recess in the male fitting, and retain the two fittings in sealing engagement with each other. The spring-loaded locking triggers 18 can he released by operation of a release handle 20 which is pivotally connected to the upper end of the outer housing 10 by means of pivots 21,
The inner housing 12 also carries a valve closure means in the form of a poppet valve 22 which is movable info and out of engagement with an annular valve seat 24 by means of a straight, elongate lever arm 26 formed from two identical plate members arranged face-to-face with each other. The use of two, thinner plates rather than one, thicker plate increases the strength of the arm, since the thinner material tends to be stronger due to work hardening of the cold roiled plate. Thinner plates can also be more accurately laser cut with less edge kerf. The rear face of the head of the poppet is provided with three elongate extensions 38 (only two of which are visible in the drawings) in slidable engagement with the inner wall of the inner housing 12 in order to guide the movement of the poppet. As best seen in Figs 2 (c) and 3 (c), the lower end of the lever arm 28 Is pivotally connected at pivot pin 27 between two lugs 28 on the rear face of the poppet and the opposite end is pivotally connected between two lugs 30 of a crank member in the form of a spliced crank block 32, A spliced aperture of the crank block 32 receives a spliced portion of a spindle 34 which is pivotally mounted in the inner housing 12 and which is rotatable by means of a handle 38 attached to the end of the spindle which extends out of the inner housing 12.
The aforementioned description is very similar to the description of the prior art refuelling coupler shown in Figs 5 and 8, However, one very important difference Is that the inner end of the spindle 34 (i.e. the end opposite to that where the handle 38 is attached) is received in, and terminates at, an Internally splined boss 50 which forms pari of the crank block 32, as best seen in Figs 4 (a) and (b). The crank block 32 is provided with a further tubular boss 52, aligned with, but separated from, the splined boss 50, As best seen in Figs 2 (e) and 3 (c), the spindle 34 is rotatably mounted In the wall of the inner housing 12 by means of a bushing 54, The two ends of the spindle 34 are splined for attachment to the complementarlly splined aperture 51 in the boss SO and to a compiementadly splined aperture 58 at the inner end of the handle 38. in addition, the further boss 52 of the crank block 32 is provided with an aperture 58 which receives one end of a stub spindle 80, the other end of the stub spindle being rotatably mounted in a recess 82 by means of a bushing 84.
Therefore, the crank block 32 is rotatably mounted on two separate, independent spindles, the first spindle 34 for rotating the crank block 32 and the second, stub spindle 80. By having two separate spindles for mounting the crank block 32. it is not necessary for a single spindle to extend across the diameter of the inner housing 12. Consequently, and as best seen in Figs 2 (c), 3 (c) and 4, the crank block 32 can be shaped to receive the lever arm 28. As shown In the Figures, the crank biock 32 comprises the two upstanding lugs 30, extending generally perpendicularly to the spindle-receiving bosses 50, 52, which are provided with aligned apertures 66 for receipt of a pivot pin 68, which is pivotally connected to the upper end of the lever arm 26, The crank block 32 also comprises a web 70 of material joining the two upstanding lugs 30, but it will be seen that an elongate recess 72 is formed between the inner faces of the upstanding lugs 30 and the spindle-receiving bosses 50, 52, for receipt of the lever arm 28; as will be explained,
By moving the handle 36. the spindle 34 connected to the handle can be rotated, which in turn causes the crank block 32 to rotate. The handle 36 can be displaced through slightly more than 180° from the position shown In Figs 1 and 2 to the position shown in Fig 3, This in turn moves the lever arm 26 which causes the poppet valve 22 to be displaced from sealing engagement with the valve seat 24 as shown in Fig 2 to a position in which it is displaced from the valve seat 24 as shown in Fig 3. As best seen in Fig 2, when the poppet valve 22 is in the dosed position, the lever arm 26 is received in the elongate recess 72 between the inner faces of the upstanding lugs 30 and the spindle-receiving bosses 50, 52, and it is therefore possible to use a straight, non-bent lever arm 26.
Since It is possible to use a straight lever arm 26, the force from the lever arm holding the poppet valve 22 open or shut as the case may be is provided substantially in the direction of travel of the poppet valve 22, in contrast to the prior art arrangements. In fact, and as can be seen in Figs 2 (b) and 3 (b), in the dosed and opened positions of the valve the lever arm is misaligned very slightly with the direction of movement of the poppet valve 22, but only so that the position of the crank block 32 has an over-centre action when the poppet valve 22 is in the dosed and opened positions, so that the valve can be held in those two positions.
In use, the refuelling coupler is attached to one end of a loading arm by means of the bolts 14, the other end of the loading arm being connected to the inlet/outiei of a delivery tanker. With the poppet valve 22 in the closed position shown in Fig 2, the coupler is ottered to a oomplernentarily shaped fitting (not shown) connected to a tanker to which fuel is to be delivered. Engagement of the refuelling coupler with the fitting causes the triggers 18 to snap into position in a circumferential recess In the male fitting. This allows the outer sleeve 10 to engage over the triggers locking them into position whilst the triggers hoid the two fittings in sealing engagement with each other. The displacement of the outer sleeve releases the handle interlock, at which point the poppet valve 22 is then displaced info the opened position shown in Fig 3 by pivoting the handle 38 and the spindle 34 to which the handle is attached through an angle of slightly greater than 180°. Fuel can then flow through the coupling and through the fitting to which the coupling is connected, and from there into the tanker.
Once the required amount of fuel has been supplied, the pumps automatically switch off and the poppet valve 22 is dosed by rotating the handle 36 to its other extreme position shown in Fig 2. in the reverse of the procedure outlined above. This causes the lever arm 28 to be received in the elongate recess 72 in the crank block 32. The spring-loaded locking triggers 18 can then be released by operation of the release handle 20, which allows the refuelling coupler to be separated from the male fitting to which it was previously attached.
As shown particularly in Figs 2 (b) and 3 (b) the pivotal mounting of the crank block 32 on two separate spindles allows the lever arm 26 to be received in the longitudinal recess 72 in the crank block 32 between the inner ends of the two spindles 34, 80 and allows a straight lever arm to be used. The use of a straight iever arm allows the force which retains the poppet valve 22 open end closed to be applied in substantially the same direction as the direction of movement of the poppet valve, without a significant bending moment. Consequently, the stresses applied to the straight lever arm 26 are significantly reduced whilst applying same forces to hold the poppet valve 22 in Its opened and dosed positions as compared with the use of a bent lever arm as in the prior art. The over centre action of the lever arm contacting the crank block results In a lockout of rotation of the primary load-bearing mechanism. This mechanism is then interlocked with the handle locating into the outer sleeve handle interlock preventing accidental operation when the valve Is not connected to the tanker.
Once refuelling is completed and the valve is closed, the undelivered fuel is retained in the loading arm. In certain circumstances, due to thermal expansion the retained fuel expands and pressurises the system. This is commonly controlled by a relief valve that releases the pressure back into the storage tank. However, in some circumstances a relief valve is not present, but the pressure can be significant, particularly with rigid piping systems. The present invention helps to prevent leakage of fuel in such circumstances.
The invention is not restricted to details of the foregoing embodiment.

Claims (17)

1. A fluid transfer coupler comprising; engagement means for releasabie engagement with a complementary shaped fitting; retaining means configured to releasably retain the complementary shaped fitting; a valve seat; valve closure means releasably engageable with the valve seat; a crank member mounted on separate first and second coaxial spindle members which define the rotational axis of the crank member; means for rotatably displacing the crank member around its rotational axis; and a connecting member pivotally connected to the crank member and connected to the valve closure means.
2. A fluid transfer coupler as claimed in claim 1, wherein the connecting member is pivotally connected to the valve closure means.
3. A fluid transfer coupler as claimed in claim 1 or claim 2, wherein the connecting member is elongate.
4. A fluid transfer coupler as claimed in claim 3, wherein the connecting member is substantially straight.
5. A fluid transfer coupler as claimed in any of the preceding claims, wherein the crank member comprises a recess for receipt of a portion of the connecting member.
6. The fluid transfer coupler as claimed in claim 5, wherein the crank member comprises a recess for receipt of a portion of the connecting member when the valve closure means is engaged with the valve seat.
7. A fluid transfer coupler as claimed In any of the preceding claims, wherein the means for rotatably displacing the crank member around its rotational axis is connected to the first spindle..
8. A fluid transfer coupler as claimed In claim 7S wherein the means for rotatably displacing the crank member around its rotational axis comprises a handle,
9. A fluid transfer coupler as claimed in any of the preceding claims, wherein the first spindle member is rotatably mounted and the crank member rotates with the first spindle member.
10. A fluid transfer coupler as claimed in any of the preceding claims, wherein the second spindle member comprises a stub spindle,
11 - A fluid transfer coupler as claimed in any of the preceding claims, further comprising a housing on which the first and second spindle members are mounted and In which the valve seat is located.
12, A fluid transfer coupler as claimed in any of the preceding claims, comprising an inner housing means and an outer housing means.
13. A fluid transfer coupler as claimed In claim 12, wherein the first and second spindle members are mounted on the Inner housing means and the valve seat is located in the inner housing means.
14, A fluid transfer coupler as claimed in any of the preceding claims, wherein the valve closure means comprises a poppet valve.
15. A fluid transfer coupler as claimed in any of the preceding claims, comprising a female fitting for releasable engagement with a complementanly shaped male fitting.
18. A fluid transfer coupler as claimed in any of the preceding claims, comprising a refuelling coupler.
17, A fluid transfer coupler substantially as herein described with reference to, and as illustrated in, the accompanying drawings.
GB1515737.3A 2015-09-04 2015-09-04 Fluid transfer coupler Withdrawn GB2541931A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB1515737.3A GB2541931A (en) 2015-09-04 2015-09-04 Fluid transfer coupler
PCT/GB2016/052689 WO2017037447A1 (en) 2015-09-04 2016-08-31 Fluid transfer coupler

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1515737.3A GB2541931A (en) 2015-09-04 2015-09-04 Fluid transfer coupler

Publications (2)

Publication Number Publication Date
GB201515737D0 GB201515737D0 (en) 2015-10-21
GB2541931A true GB2541931A (en) 2017-03-08

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB1515737.3A Withdrawn GB2541931A (en) 2015-09-04 2015-09-04 Fluid transfer coupler

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GB (1) GB2541931A (en)
WO (1) WO2017037447A1 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5904302A (en) * 1997-03-21 1999-05-18 Brown; Albert W. Aircraft fueling nozzle
GB2448707A (en) * 2007-04-24 2008-10-29 Fort Vale Eng Ltd Discharge valve assembly

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6705550B2 (en) * 2001-05-22 2004-03-16 Scot P. Bell Closed circuit fuel nozzle

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5904302A (en) * 1997-03-21 1999-05-18 Brown; Albert W. Aircraft fueling nozzle
GB2448707A (en) * 2007-04-24 2008-10-29 Fort Vale Eng Ltd Discharge valve assembly

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Publication number Publication date
GB201515737D0 (en) 2015-10-21
WO2017037447A1 (en) 2017-03-09

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