EP4408747A1 - Air hose - Google Patents
Air hoseInfo
- Publication number
- EP4408747A1 EP4408747A1 EP22800866.0A EP22800866A EP4408747A1 EP 4408747 A1 EP4408747 A1 EP 4408747A1 EP 22800866 A EP22800866 A EP 22800866A EP 4408747 A1 EP4408747 A1 EP 4408747A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- component
- hose
- air hose
- air
- condition
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
- B64F1/362—Installations for supplying conditioned air to parked aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L11/00—Hoses, i.e. flexible pipes
- F16L11/04—Hoses, i.e. flexible pipes made of rubber or flexible plastics
- F16L11/12—Hoses, i.e. flexible pipes made of rubber or flexible plastics with arrangements for particular purposes, e.g. specially profiled, with protecting layer, heated, electrically conducting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L11/00—Hoses, i.e. flexible pipes
- F16L11/24—Hoses, i.e. flexible pipes wound from strips or bands
Definitions
- the invention relates to an air hose.
- the invention relates to an air hose for delivering air, for example pre-conditioned air, to an aircraft.
- Pre-conditioned air systems are used to bring cooled or heated air into a parked aircraft. Air is supplied from a pre-conditioned air unit to cabins of the aircraft via air hoses, which are referred to as pre-conditioned air hoses, when the aircraft is grounded and an auxiliary power unit is not operational. Such air hoses are often around 18 metres in length, and the pre-conditioned air unit is typically mounted to a passenger boarding bridge at an airport.
- pre-conditioned air hoses There are two types of pre-conditioned air hoses, each of which requires a different storage system at a passenger boarding bridge.
- the first type known as flat hoses
- This is advantageous as a reel of flattened and rolled hose is relatively small, as compared to other airport equipment.
- the reel is compact and can be stored easily on the bridge, which is busy with other equipment.
- the entire hose must be unrolled from the reel in order to get air through the hose.
- the hose may be too long to be laid in a straight line, flat hoses are prone to kinking. Kinking in the hose may reduce or prevent the flow of air through the hose, reducing the capacity of the entire preconditioned air system.
- spiral hoses have a wire reinforcement.
- the spiral wire located in or around the circumference of the hose allows the hose to be axially compressed for storage.
- Spiral hoses are stored in big, bulky and costly hose retrievers.
- spiral hoses do not need to be fully extended in order for air to flow through the hose. This means that only the length of hose necessary to reach the aircraft from the storage position needs to be extracted from the hose retriever.
- the risk of kinking of spiral hoses is reduced or eliminated as the hose length can be laid in a straight line and the nature of the hose itself reduces the risk of kinking.
- an air hose for example a pre-conditioned air hose, the air hose comprising a first component and a second, elastic component, wherein the second component is fastened to the first component at a plurality of fastening positions along the axial direction of the air hose, such that the air hose is operable between a first, e.g. retracted and/or deflated, condition in which the first component is slack between axially adjacent fastening positions and is collapsible in a radial direction, and a second, e.g. extended and/or inflated, condition in which axially adjacent fastening positions are separated against a biasing force of the second component.
- a first e.g. retracted and/or deflated
- the biasing force of the second, elastic component prevents or obviates kinking, twisting or other entanglement of the hose.
- the second component remains in an extended state, wherein it applies the biasing force, even when the hose is bent or curved, thereby reducing or eliminating the likelihood and severity of kinking or twisting of the hose.
- the supply of air for example pre-conditioned air
- the capacity of the air system for example the pre-conditioned air system
- the air hose may be a flat air hose.
- the hose In the first condition the hose may be flat or flattenable.
- the first component In the second condition, the first component may be in a radially uncollapsed or expanded condition. That is, the first component may not be collapsed when in the second condition.
- the first component may be elongate.
- the first component may, for example, be tubular.
- the elongate and/or tubular first component may have a first end, for example a first open end, and a second end, for example a second open end.
- the axial direction of the hose may be defined between the first open end and the second open end of the first component.
- An axial distance or length of the first component may be defined between the first open end and the second open end of the first component.
- the first component may be less slack between adjacent fastening positions when the hose is in the second, extended, condition than when the hose is in the first, retracted, condition.
- the axial distance or length between the first open end of the first component and the second open end of the first component may be greater when the hose is in the second, extended, condition than when the hose is in the first, retracted, condition.
- the adjacent fastening positions may be further apart along the axial direction of the hose when the first component of the hose is extended in the second condition than when the first component of the hose is retracted in the first condition.
- the fastening positions may be discrete fastening positions.
- the fastening positions may be spaced apart.
- the fastening positions may be evenly distributed along the axial direction of the hose.
- the fastening positions may be distributed along the entire length of the first component, between a first end and a second end of the first component.
- There may be two fastening positions for example a first fastening position at a first end of the first component and a second fastening position at a second end of the first component.
- the fastening of the second component to the first component may be via stitching, pins, rivets, ties, zip-ties, staples, hook and loop fasteners, snap-fit fasteners, bonding (for example using adhesive), adhesive tape, welding, crimping or buttons, or any other suitable fastening means.
- the fastening positions may be spaced along the axial direction by 180 mm.
- the fastening positions may also be distributed around the circumference of the first component.
- the fastening positions may be at discrete positions around the circumference of the first component.
- the fastening positions may be evenly distributed around the circumference of the first component.
- One of the first end for example the first open end, or the second end, for example the second open end, may be connectable or connected to an air supply, for example a pre-conditioned air supply.
- the other of the first open end or the second open end may be connected or connectable to an apparatus or device which is configured to receive air, for example pre-conditioned air.
- the first component may be air-tight.
- the first component may be sufficiently air tight to transport air, for example pre-conditioned air, from an air supply, for example a preconditioned air supply, to the apparatus or device which is configured to receive air.
- the first component may be sufficiently air tight to deliver air to the apparatus or device which is configured to receive air at a desired pressure and/or flow rate.
- the second, extended, condition may be an inflated condition.
- air may flow through the hose, for example air may be pumped through the hose.
- the first, retracted, condition may be a deflated condition. In the deflated condition, no, or minimal, air may be supplied to and/or flow through the hose.
- the second component may be elongate.
- the second component may comprise at least one resilient member.
- the second component may comprise a plurality of resilient members. Each resilient member may extend along the axial direction of the hose.
- the plurality of resilient members may be distributed around the circumference of the hose.
- the fastening positions may each correspond to a separate resilient member.
- the fastening positions may, for example, be in the form of a spiral stich, wherein a pitch of the spiral defines the distance between axially adjacent fastening positions.
- the hose may further comprise a plurality of fastening points or fasteners via which the second component can be connected, attached or fastened to the first component.
- the plurality of fastening points or fasteners may be distributed along the axial direction of the hose.
- the plurality of fastening points may be distributed around the circumference of the hose. There may be two fastening points, for example a first fastening point at a first end of the hose and a second fastening point at a second end of the hose. There may be more than two fastening points between the first end of the hose and the second end of the hose.
- the first component may be less elastic than the second component.
- the first component may be inelastic, for example relatively inelastic compared to the second component.
- the air hose may be for supplying air to an aeroplane, helicopter, or other aircraft.
- the first component In the second, extended, condition the first component may be taut, or held in tension, between axially adjacent fastening positions.
- the first component may be stretched between fastening positions which are adjacently positioned along the axial length of the first component of the hose. Tension in the first component, when the hose is in the second, extended, condition, may prevent further extension of the second component.
- the second component may be located on the outside of the first component, for example on an outer surface of the first component. Alternatively, the second component may be located on the inside of the first component, for example on an inner surface of the first component.
- the first component may comprise a plurality of layers.
- the second component may be located between two layers of the first component.
- the plurality of layers of the first component may be tubular.
- the plurality of layers of the first component may be substantially concentric.
- the first component may comprise three layers.
- the second component may be located between an innermost layer and a middle layer of the first component. Alternatively, the second component may be located between a middle layer and an outermost layer of the first component.
- the second component may comprise at least one elastic cord, for example an elastic shock cord.
- the at least one elastic cord may be substantially axially aligned with the first component of the hose.
- a plurality of elastic cords may be distributed, for example evenly distributed, around the circumference of the hose.
- the second component may comprise at least one spring.
- the at least one spring may be substantially axially aligned with the hose.
- a plurality of springs may be distributed, for example evenly distributed, along the length of the hose.
- a plurality of springs may be distributed, for example evenly distributed, around the circumference of the hose.
- the second component may comprise an elastic material, for example a rubber material or an elasticated fabric.
- the second component may comprise an elastic tube, for example a rubber material in a tubular shape, or an elastic material in a tubular shape.
- the elastic tube may be substantially concentric with the first component.
- a method of manufacturing the aforementioned air hose wherein the second component is extended before being fastened to the first component, and axial tension is applied to the first component to reduce the slack to below that present when the hose assembly is in the first condition, before being fastened to the second component.
- the second component may be extended by at least 100%, for example at least 120%, preferably at least 150% before being fastened to the first component.
- the percentage extension of the second component is defined as the extended length of the second component (L2) divided by the length of the second component immediately before extension (LI), multiplied by 100%.
- Figure 1 illustrates a first example of an air hose in a deflated condition
- Figure 2 illustrates the air hose of Figure 1 in an inflated condition
- Figure 3 illustrates a second example of an air hose in a deflated condition
- Figure 4 illustrates the air hose of Figure 3 in an inflated condition.
- the illustrative embodiments relate to air hoses, which may be pre-conditioned air hoses.
- the air hose is intended for use with an aeroplane. However, the air hose can be used with any suitable aircraft.
- the hose 1 is shown in a retracted or deflated condition in Figure 1, and in an extended or inflated condition in Figure 2.
- the hose 1 has a first open end 13 and a second open end 14.
- the first end 13 is connectable to an air supply (not shown).
- the second end 14 is connectable to apparatus for receiving air (not shown).
- the hose 1 has a first component 11 and a second component 12.
- the first component 11 is a tubular material which is suitable for use in an air hose. In this example, the first component 11 comprises three, concentric layers.
- the first component 11 provides a conduit which is sufficiently air-tight to transfer air from the first end 13 to the second end 14 at the desired pressure and/or flow rate.
- the second component 12, in this example, comprises a plurality of elastic cords 12.
- the elastic cords may be of any suitable diameter, for example 6 mm or 8 mm.
- the elastic cords 12 are substantially aligned with the axial direction of the hose 1. In this example four equally spaced elastic cords 12 are provided around the circumference of the hose (although only two are visible in Figures 1 and 2). However, any number of elastic cords 12 may be provided, for example two, three, five or six.
- the elastic cords 12 are located between an innermost layer of the first component 11 and a middle layer of the first component 11. However, it will be appreciated that the elastic cords 12 may be located inside of the first component 11, on the outside of the first component 11, or between the middle layer and an outermost layer of the first component 11.
- the elastic cords 12 are fastened to the first component 11 at discrete, spaced fastening positions 15 along the axial direction X of the hose 1.
- the fastening positions 15 are spaced along the axial direction by 180 mm. Fastening is via any suitable means, such as stitching, pins, rivets, ties, zip-ties or staples. Between the fastening positions 15 the elastic cords 12 are not fastened to the first component 11. Between the fastening positions 15 the first component 11 is slack when in the retracted or deflated condition as shown in Figure 1.
- the elastic cords 12 have an unstretched length LI, as is shown in Figure 1, in which the elastic cords are held in a straight configuration, immediately before any extension to the elastic cords
- the first component has a length L2, as shown in Figure 2, when the first component 11 is held taut.
- the elastic cords 12 are extended to a length L2, and the hose 1 is straight.
- the hose 1 may be bent or curved, for example if the hose 1 is too long once it is fully unrolled for use.
- the hose 1 is assembled by first holding the first component 11 at length L2, and by extending the elastic cords 12 to a length of L2.
- the elastic cords 12 are fastened to each of the fastening positions on the first component 11 when the elastic cords 12 and the first component 11 have a length of L2.
- the elastic cords 12 are allowed to return to a length of LI such that the slack is provided in the first component 11 between the fastening positions due to the biasing force of the elastic cords 12 contracting, or crimping, the first component 11.
- the elastic cords 12 are extended by 150% before being fastened to the first component 11.
- the length of the second component immediately before extension (LI) is 12 m using the following formula:
- the hose 1 is operable between the deflated or retracted condition and the inflated or extended condition.
- the hose 1 When in the deflated condition the hose 1 is collapsible, such that it is flat or flattenable, and is able to be rolled, or folded, for storage. This means that the hose 1 can be stored compactly, easily and efficiently.
- the hose 1 is unrolled or unfolded, and inflated to the inflated or extended condition, by pumping air through the hose 1.
- When inflated the hose 1 is not collapsed and axially adjacent fastening positions are separated against the biasing force of the elastic cords 12.
- the elastic cords 12 are able to extend until the first component 11 is taut between fastening positions.
- the elastic cords 12 extend to 150% of the unstretched length, when the hose 1 is in a straight configuration in the inflated or extended condition.
- the second component 12 may, in some cases, also extend axially and/or circumferentially in the inflated condition.
- the biasing forces acting on the first component 11 by the elastic cords 12 reduce, or eliminate, the severity and likelihood of kinking of the hose 1. This means that the correct pressure and/or flow rate of air can be maintained.
- the hose 1 When the supply of air to the hose 1 is stopped, the hose 1 deflates and returns to the deflated or retracted condition.
- the elastic cords 12 contract to introduce the slack into the first component 11, and the hose 1 returns to a length of LI. This means that the hose 1 offers no resistance to rolling, or folding, for efficient storage, for example on a reel on the passenger boarding bridge.
- Figure 3 shows the hose 10 in a deflated or retracted condition
- Figure 4 shows the hose 10 in an inflated or extended condition.
- This example is the same as the hose 1 described with reference to Figure 1, with the exception that the second component is an elastic hose (not shown).
- the elastic hose 10 is tubular in shape and is manufactured from an elastic material such as an elastic fabric.
- the first component 110 comprises two layers, but it will be appreciated that the first component 110 could be the same as that in the previous example.
- the elastic hose is located between the layers of the first component 110 and is stitched thereto, the stitching being a spiral shape with respect to the axial direction of the hose. It will be appreciated that the elastic hose could be located on the inside, or outside, of the first component 11 instead. It will also be appreciated that multiple elastic hoses could be provided at different positions. For example, elastic hoses could be provided in any combination of being inside of the first component 110, outside of the first component 110, or between any number of a plurality of layers of the first component 110. The spacing of axially adjacent fastening positions is provided by the pitch of the spiral stitching. When the elastic hose is unstretched, the first component 110 is slack between any two axially adjacent positions on the stitching.
- the hose 10 is manufactured in a similar way to the hose 1 of the previous example, whereby the elastic hose is stretched to a length of L20, the first component 110 is held taut at a length of L20, and the elastic hose is stitched to the first component 110 while both the elastic hose and the first component 110 are at a length of L20. The elastic hose is then allowed to return to an unstretched length of L10, thereby slackening the first component 110 between axially adjacent fastening positions 150. As in the previous example, the extension of the elastic hose is 150%, as provided by the following formula:
- the hose 10 of this example is operable between an inflated or extended condition and a deflated or retracted condition.
- the elastic hose In the inflated condition the elastic hose is stretched, and the slack in the first component 110 between axially adjacent fastening positions 150 is reduced to reduce, or eliminate, the likelihood and severity of kinking of the hose 10. This enables the correct pressure and/or flow rate of air to be supplied.
- the elastic hose contracts and reintroduced slack into the first component 110 between axially adjacent fastening positions 150.
- the hose 10 In the deflated condition the hose 10 can be rolled or folded into storage, such that it can be stored efficiently on the passenger boarding bridge.
- springs may be provided instead of elastic cords.
- a plurality of springs may be located along the axial direction of the hose.
- the elastic tube may be stitched to the first component with parallel lines of stitching around the circumference of the hose, instead of spiral stitching.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB2113838.3A GB202113838D0 (en) | 2021-09-28 | 2021-09-28 | Air hose |
| PCT/US2022/043066 WO2023055550A1 (en) | 2021-09-28 | 2022-09-09 | Air hose |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP4408747A1 true EP4408747A1 (en) | 2024-08-07 |
Family
ID=91640408
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP22800866.0A Pending EP4408747A1 (en) | 2021-09-28 | 2022-09-09 | Air hose |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20250128829A1 (en) |
| EP (1) | EP4408747A1 (en) |
| CN (1) | CN118284559A (en) |
-
2022
- 2022-09-09 EP EP22800866.0A patent/EP4408747A1/en active Pending
- 2022-09-09 US US18/694,299 patent/US20250128829A1/en active Pending
- 2022-09-09 CN CN202280077055.5A patent/CN118284559A/en active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| US20250128829A1 (en) | 2025-04-24 |
| CN118284559A (en) | 2024-07-02 |
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