阅读说明：本技术 引导交通工具乘员通风的方法和设备及相关座椅 (Method and device for guiding the ventilation of a vehicle occupant and associated seat ) 是由 道格拉斯·D·马本 于 2021-06-18 设计创作，主要内容包括：公开了引导交通工具乘员通风的方法和设备及相关座椅。公开的示例性设备包括交通工具的舱室的空气供应管道；歧管,流体地耦接到空气供应管道,歧管延伸到舱室的乘员座椅；以及喷嘴,流体地耦接到歧管,喷嘴定位成当乘员占用乘员座椅中的一个时,面向乘员的面部的前方。(Methods and apparatus for directing ventilation of a vehicle occupant and associated seats are disclosed. A disclosed example apparatus includes an air supply duct of a cabin of a vehicle; a manifold fluidly coupled to the air supply conduit, the manifold extending to a passenger seat of the cabin; and a nozzle fluidly coupled to the manifold, the nozzle positioned to face forward of a face of an occupant when the occupant occupies one of the occupant seats.)

1. An apparatus for guiding ventilation of a vehicle occupant, comprising:

an air supply duct of a cabin of a vehicle;

a manifold fluidly coupled to the air supply conduit, the manifold extending to a passenger seat of the cabin; and

a nozzle fluidly coupled to the manifold, a plurality of the nozzles positioned to face forward of a face of one of the passenger seats when the respective passenger occupies the passenger seat.

2. The apparatus of claim 1, further comprising a conduit extending between the manifold and the nozzle, and

wherein the conduit extends from a base of the passenger seat to a headrest of the passenger seat.

3. The apparatus of claim 1, further comprising a nozzle mount for supporting a respective nozzle, wherein the nozzle mount curves away from a headrest of the passenger seat.

4. The apparatus of claim 1, wherein the nozzle is to be directed toward the mouth or nose of the occupant.

5. The apparatus of any one of claims 1 to 4, wherein the manifold extends between a plurality of the passenger seats in a same row of the cabin.

6. A seat for a vehicle, the seat comprising:

a manifold fluidly coupled to the air supply conduit;

a conduit fluidly coupled to the manifold, the conduit extending from the manifold and toward a headrest of the seat; and

a nozzle fluidly coupled to the manifold, the nozzle positioned to face forward of a face of an occupant when the occupant occupies the seat.

7. A seat as claimed in claim 6, further comprising a nozzle mount for supporting the nozzle, the nozzle mount being curved away from the headrest.

8. A seat according to claim 7, wherein the nozzle mount is pivotable along a vertical height.

9. A seat as claimed in claim 7, in which the nozzle mount is flexible to adjust the position of the nozzle relative to the occupant.

10. The seat of claim 6, wherein the conduit extends from a base of the seat to the headrest.

11. A seat as claimed in any one of claims 6 to 10, in which the manifold extends across the rear of the seat.

12. A method of guiding ventilation of a vehicle occupant, comprising:

providing air to an air supply duct associated with a cabin of a vehicle, the air supply duct being fluidly coupled to a manifold that extends to a passenger seat of the cabin; and

directing air from the manifold to nozzles positioned to face forward of a face of an occupant when the occupant occupies a respective one of the occupant seats.

13. The method of claim 12, further comprising pivoting a nozzle mount supporting the nozzle based on a height of an occupant.

14. The method of claim 12, wherein the manifold extends between a plurality of the occupant seats in a row of the cabin.

15. The method of any of claims 12 to 14, further comprising filtering the air of the air supply duct.

16. A method of guiding ventilation of a vehicle occupant, comprising:

coupling a manifold to a seat of a cabin of a vehicle, the manifold to be fluidly coupled to an air supply duct associated with the cabin;

fluidly coupling a nozzle to the manifold; and

the nozzles are positioned such that when an occupant occupies the seat, air from the air supply duct is directed towards the front of the occupant's face.

17. The method of claim 16, further comprising coupling a conduit between the manifold and the nozzle, the conduit extending along a height of the seat.

18. The method of claim 16, further comprising coupling a filter to the air supply conduit.

19. The method of any of claims 16-18, wherein the manifold is positioned rearward of the seat.

Technical Field

The present disclosure relates generally to vehicles and, more particularly, to methods and apparatus for directing ventilation of vehicle occupants.

Background

Typically, Cabin Air Systems (CAS) are applied on aircraft to provide clean filtered air to the aircraft occupants. Specifically, the CAS provides outside air to a cabin of an aircraft and simultaneously circulates the air within the cabin. The resulting airflow pattern within the cabin may result in substantial mixing of the air within the cabin. Therefore, air discharged by one occupant may be circulated to other occupants, thereby increasing the risk of infection or the like.

Disclosure of Invention

An exemplary device comprises: an air supply duct of a cabin of a vehicle; a manifold fluidly coupled to the air supply conduit, the manifold extending to a passenger seat of the cabin; and a nozzle fluidly coupled to the manifold, the nozzle positioned to face forward of one of the occupant seats when the occupant is occupying the occupant seat.

An exemplary seat for a vehicle includes: a manifold fluidly coupled to the air supply conduit; a conduit fluidly coupled to the manifold, the conduit extending from the manifold and toward a headrest of the seat; and a nozzle fluidly coupled to the manifold, the nozzle positioned to face forward of a face of an occupant when the occupant occupies the seat.

An exemplary method comprises: providing air to an air supply duct associated with a cabin of a vehicle, the air supply duct being fluidly coupled to a manifold that extends to a passenger seat of the cabin; and directing air from the manifold to a nozzle positioned to face forward of a face of an occupant when the occupant occupies a respective one of the occupant seats.

An exemplary method comprises: coupling a manifold to a seat of a cabin of a vehicle, the manifold to be fluidly coupled to an air supply duct associated with the cabin; fluidly coupling a nozzle to a manifold; and positioning the nozzle such that air from the air supply duct is directed towards the front of the occupant's face when the occupant occupies the seat.

Drawings

Fig. 1 illustrates an example aircraft in which examples disclosed herein may be implemented.

Figure 2 illustrates an exemplary ventilation system according to the teachings of the present disclosure.

Figure 3 illustrates an exemplary seat embodiment of the ventilation system shown in figure 2.

Fig. 4A-4C depict exemplary nozzle types that may be employed in examples disclosed herein.

Fig. 5 is a flow chart representing an exemplary method of implementing examples disclosed herein.

Fig. 6 is a flow chart representing an exemplary method of implementing examples disclosed herein.

The figures are not drawn to scale. Alternatively, the thickness of layers or regions may be exaggerated in the figures. Generally, the same reference numbers will be used throughout the drawings and the accompanying written description to refer to the same or like parts. As used herein, unless otherwise specified, the term "above" describes a relationship with respect to two parts of the earth. The first portion is above the second portion if the second portion has at least one portion between the earth and the first portion. Also, as used herein, a first portion is "below" a second portion when the first portion is closer to the earth than the second portion. As above, the first portion may be above or below the second portion and have one or more of the following: there is no other portion between the first portion and the second portion, the first portion and the second portion are in contact, or the first portion and the second portion are not in direct contact with each other. As used in this application, a statement that any part is on another part in any way (e.g., positioned …, located …, disposed …, formed …, etc.) indicates that the referenced part is in contact with the other part or that the referenced part is on the other part with one or more intervening parts therebetween. As used herein, a connection reference (e.g., attached, coupled, connected, and engaged) may include intermediate members between elements referenced by the connection reference and/or relative movement between those elements, unless otherwise indicated. Thus, joinder references do not necessarily imply that two elements are directly connected and/or in fixed relation to each other. As used herein, the statement that any part is "in contact with" another part is defined to mean that there is no intervening part between the two parts.

Unless specifically stated otherwise, descriptors such as "first," "second," "third," etc., used herein do not imply or otherwise indicate any of a priority, a physical order, an arrangement in a list, and/or an order in any way, but rather are used merely as labels and/or as arbitrary names to distinguish elements to facilitate understanding of the disclosed examples. In some examples, the descriptor "first" may be used to refer to one element in a particular embodiment, while different descriptors such as "second" or "third" may be used in the claims to refer to the same element. In such cases, it should be understood that such descriptors are used only to clearly identify those elements that might otherwise share the same name, for example. As used herein, "approximate" and "approximately" refer to dimensions that may not be accurate due to manufacturing tolerances and/or other real-world imperfections.

Detailed Description

Methods and apparatus for guiding ventilation of a vehicle occupant are disclosed. Known aircraft employ Cabin Air Systems (CAS) to provide clean filtered air to the occupants of the aircraft. However, when the nacelle is used as a circulation volume, the air within the nacelle may mix in large amounts. Specifically, air discharged by one occupant may be circulated to other occupants, thereby increasing the risk of infection or the like.

Examples disclosed herein enable increased relative isolation of ventilation between occupants of a vehicle, which may be an aircraft, spacecraft, land vehicle, boat, submarine, bus vehicle, and the like. Thus, examples disclosed herein may reduce the likelihood of infection (e.g., due to viruses, bacteria, etc.) and/or the spread of bad odors throughout the vehicle. Alternatively, examples disclosed herein may be implemented in connection with buildings and other fixed structures where people are adjacent to each other.

Examples disclosed herein utilize a manifold that is fluidly coupled to an air supply conduit. The manifold may extend between a plurality of passenger seats of the vehicle. The at least one nozzle is fluidly coupled to the manifold. The nozzle and/or the outlet of the nozzle is directed towards the front of the face of the seat occupant. For example, the nozzle may be positioned in front of the occupant and mounted to a nozzle mount that exhibits a curvature to orient the nozzle to face the front of the occupant. In particular, the nozzle may face the mouth and/or nose of the occupant.

In some examples, the nozzle mount includes a plurality of curved portions such that the nozzle faces the front of the occupant. In some examples, the conduit extends between the manifold and the nozzle and/or nozzle mount. In some such examples, the conduit extends substantially vertically between a base of the seat and a headrest of the seat. In some examples, the nozzle mount may pivot relative to the vertical height of the seat. Additionally or alternatively, the nozzle mount and/or the nozzle are pliable (flexible) to adjust the position and/or orientation of the nozzle relative to the occupant.

Fig. 1 illustrates an exemplary aircraft 100 in which examples disclosed herein may be implemented. In the example shown, the aircraft 100 includes a horizontal tail 102, a vertical tail 103, and wings 104 (e.g., fixed wings) attached to a fuselage 106. The wing 104 of the illustrated example has an engine 107 and control surfaces 108 (e.g., flaps, ailerons, patches, etc.), some of which are located at the trailing or leading edge of the wing 104. The control surface 108 may be displaced or adjusted (e.g., deflected, etc.) to provide lift during takeoff, landing, and/or flight maneuvers.

In the illustrated example, an occupant of the aircraft 100 (e.g., a passenger, flight crew, pilot, etc.) is located in a fuselage 106 of the aircraft 100. In other words, the fuselage 106 provides a pleasant environment for the occupants of the aircraft 100. In this example, the aircraft 100 receives air external to the aircraft 100 and also circulates the air within the fuselage 106. Examples disclosed herein enable relative isolation and/or separation of air circulating between the above-described occupants.

Figure 2 illustrates an exemplary ventilation system 200 according to the teachings of the present disclosure. In the example shown in FIG. 2, nacelle 202 is shown within fuselage 106. The ventilation system 200 includes an air supply duct 204 fluidly coupled to a distribution duct 206. The distribution pipe 206, in turn, is fluidly coupled to a manifold 210 (e.g., a seat manifold, a seat air distribution manifold, etc.). The example manifold 210 extends across and/or through seats 212 (hereinafter referred to as seats 212a, 212b, 212c, etc.), all of which are arranged in a single row in this example. However, in other examples, the seats 212a, 212b, 212c may be positioned in different rows.

In the example shown, the manifold 210 is fluidly coupled to nozzles 214 (hereinafter nozzles 214a, 214b, 214c, etc.) via respective conduits 218 (e.g., respective air conduits, fluid conduits, risers, etc.) (hereinafter conduits 218a, 218b, 218c, etc.). Further, the nozzles 214a, 214b, 214c are supported and positioned by respective nozzle mounts 220 (e.g., nozzle positioners, nozzle guides, etc.) (hereinafter referred to as nozzle mounts 220a, 220b, 220c, etc.).

To supply air to at least one occupant on a seat 212a, 212b, 212c, air is supplied to the air supply duct 204 and, in turn, to the distribution duct 206. The air is then supplied to a manifold 210 that extends across the seats 212a, 212b, 212 c. The air from the manifold 210 then moves through the conduits 218a, 218b, 218c and exits from the respective nozzles 214a, 214b, 214 c. Air is thus provided directly to the occupants of the seats 212a, 212b, 212 c. In this example, the nozzles 214a, 214b, 214c are oriented to face in front of the occupant's face (e.g., the occupant's mouth and/or nose). Specifically, the example nozzle mounts 220a, 220b, 220c are curved to direct air output from the nozzles 214a, 214b, 214c toward the front of the occupant's face. In other words, the nozzles 214a, 214b, 214c are located in front of the seats 212a, 212b, 212c, and the curvature is implemented such that the nozzles 214a, 214b, 214c face the occupant's face. In this example, the nozzles 214a, 214b, 214c are positioned directly in front of one or more respective occupants and are substantially horizontal (e.g., within 15 degrees of horizontal).

Figure 3 illustrates an exemplary seat embodiment of the ventilation system 200 shown in figure 2. In this example, an occupant 301 is shown supported by the aforementioned seat 212, which includes a base 302 (e.g., a seat bottom), a seat back 304, and a headrest 306. As seen in the view shown in fig. 3, the nozzle 214 is located in front of the occupant 301 and faces the occupant 301 in the region near the mouth and nose of the occupant 301. Further, the nozzle mount 220 extends away from the headrest 306 and curves to direct air toward the occupant 301. In other words, the nozzle 214 is directed towards the occupant 301 in a manner similar to a microphone and/or a head-mounted microphone. In this example, the conduit 218 of the illustrated example extends substantially vertically relative to the seat back 304 and/or the seat 212.

To position the nozzle 214 in front of the occupant 301 and direct the nozzle 214 towards the front of the face of the occupant 301, the nozzle mount 220 and/or the nozzle 214 includes a longitudinal extension 305 that extends towards the front of the seat 212, and one or more curved portions 307 (e.g., one or more arcuate portions) that orient the nozzle 214 towards the occupant 301. In other words, the combination of the one or more curved portions 307 and the longitudinal extension 305 results in the nozzle 214 facing the front side of the occupant 301, thereby functioning in a similar manner as, for example, a microphone boom. However, any suitable geometry that directs the nozzle 214 in front of the face of the occupant 301 may alternatively be applied.

In some examples, the nozzle 214 may pivot to adjust the height at which air is provided to the occupant 301. For example, the catheter 218 may pivot about a pivot 310, as generally indicated by the double arrow 312. Additionally or alternatively, the nozzle 214, nozzle mount 220, and/or conduit 218 are pliable (e.g., plastically deformable) to adjust a position and/or height at which the nozzle 214 provides air to the occupant 301. In some examples, the nozzle 214 is integral with the seat 212. In some examples, the nozzle 214 moves and/or pivots (e.g., via a linkage or cam mechanism, etc.) in response to height adjustment of the seat 212.

Fig. 4A-4C depict exemplary nozzle types that may be implemented in examples disclosed herein. Turning to FIG. 4A, a top view of the nozzle 214 and occupant 301 is shown. As can be seen in fig. 4A, the nozzle 214 extends over the entire width of the head of the occupant 301.

Fig. 4B is a detailed view of the nozzle 214. In this example, the nozzle 214 includes a plurality of orifices 401 spaced apart at equal intervals, thereby defining a grid pattern (e.g., a whistling pattern). In this example, the apertures 401 all have equal diameters. However, in other examples, the apertures 401 may vary in size and/or spacing. For example, the size of the orifice 401 may gradually increase in a direction toward the center of the occupant 301.

Fig. 4C is a detailed view of an alternative exemplary nozzle 402. In contrast to the exemplary nozzle 214, the nozzle 402 exhibits a grid or mesh-like opening with vanes 404. In some examples, the blades 404 may be angled and/or adjusted by the occupant 301.

The exemplary nozzle types described herein are merely examples, and any suitable nozzle type may alternatively be implemented. For example, convergent nozzles, divergent nozzles, and the like may be alternatively implemented.

Fig. 5 is a flow chart representing an exemplary method 500 of implementing examples disclosed herein. In this example, the ventilation system 200 will operate in the aircraft 100 during flight. Specifically, ventilation system 200 provides pressurized air to occupants of fuselage 106.

At block 502, air is provided from an air supply source to the air supply conduit 204.

At block 504, in some examples, the air is filtered (e.g., via a sub-micron filter, HEPA filter, etc.). Specifically, the air may be filtered as it recirculates through nacelle 202.

At block 506, air is directed to the nozzle 214. In this example, the nozzles 214 are positioned and/or rotated to direct air in front of the occupant's face.

At block 508, in some examples, the nozzle mount 220 and/or the nozzle 214 are pivoted. For example, the nozzle 214 may be moved by the occupant such that the nozzle 214 is directed toward the occupant's mouth and/or nose.

At block 510, it is determined whether to repeat the process. If the process is to be repeated (block 510), control returns to block 502. Otherwise, the process ends. The determination may be based on whether ventilation is needed (e.g., whether the aircraft 100 is in flight).

Fig. 6 is a flow chart representing an exemplary method 600 of implementing examples disclosed herein. In this example, the ventilation system 200 is mounted and/or retrofitted to the fuselage 106 of the aircraft 100.

At block 602, a filter is coupled to the air supply conduit 204. The filter may be used to filter air provided to an occupant.

At block 604, the manifold 210 is coupled to the seat 212. For example, the manifold 210 may be positioned behind, across, and/or across a plurality of seats 212. Additionally or alternatively, the manifold 210 extends below the seat 212. In some examples, the manifold 210 extends across a plurality of seats 212 in a single row of the aircraft 100.

At block 606, the nozzle 214 is fluidly coupled to the manifold 210. The nozzle 214 may be coupled to the manifold via a conduit or tube (e.g., a flexible tube). In this particular example, the conduit 218 is coupled between the manifold 210 and the nozzle 214 (e.g., fluidly coupled between the manifold and the nozzle).

At block 608, in some examples, the conduit 218 is operably coupled between the nozzle 214 and the manifold 210.

At block 610, the nozzle 214 is positioned toward the face of the occupant. Specifically, when an occupant is present, the nozzle 214 is positioned to face forward of the occupant.

At block 612, it is determined whether to repeat the process. If the process is to be repeated (block 612), control returns to block 602. Otherwise, the process ends.

From the foregoing, it will be appreciated that exemplary methods, apparatus, and articles of manufacture have been disclosed that enable the reduction (e.g., elimination) of infections (e.g., bacterial infections, viral infections, etc.) that are transmitted between occupants of a vehicle, such as an aircraft. Further, examples disclosed herein may reduce the spread of pathogens (e.g., viruses, bacteria, etc.) between occupants of a vehicle.

Although certain example methods, apparatus and articles of manufacture have been disclosed herein, the scope of coverage of this disclosure is not limited thereto. On the contrary, this disclosure covers all methods, apparatus, and articles of manufacture fairly falling within the scope of the appended claims. Although the examples disclosed herein are shown in the context of an aircraft, the examples disclosed herein may be implemented in any suitable type of vehicle or building structure that requires ventilation.

Clause 1: an apparatus, comprising: an air supply duct of a cabin of a vehicle; a manifold fluidly coupled to the air supply conduit, the manifold extending to a passenger seat of the cabin; and a nozzle fluidly coupled to the manifold, the plurality of nozzles positioned to face forward of a face of the occupant when the respective occupant occupies one of the occupant seats.

Clause 2: the apparatus defined in clause 1 further comprising a conduit extending between the manifold and the nozzle.

Clause 3: the apparatus defined in clause 2 wherein the conduit extends from the base of the passenger seat to the headrest of the passenger seat.

Clause 4: the apparatus defined in any one of clauses 1-3 further comprising a nozzle mount to support the respective nozzle, wherein the nozzle mount curves away from a headrest of the passenger seat.

Clause 5: the apparatus defined in any one of clauses 1-4 wherein the nozzle is to be directed toward the mouth or nose of the occupant.

Clause 6: the apparatus defined in any one of clauses 1-5 wherein the manifold extends between a plurality of passenger seats in the same row of the cabin.

Clause 7: a seat for a vehicle, the seat comprising: a manifold fluidly coupled to the air supply conduit; a conduit fluidly coupled to the manifold, the conduit extending from the manifold and toward a headrest of the seat; and a nozzle fluidly coupled to the manifold, the nozzle positioned to face forward of a face of an occupant when the occupant occupies the seat.

Clause 8: the seat defined in clause 7 further comprising a nozzle mount for supporting the nozzle, the nozzle mount curving away from the headrest.

Clause 9: the seat defined in clause 8, wherein the nozzle mount is pivotable along a vertical height.

Clause 10: the seat defined in clause 8, wherein the nozzle mount is pliable (pliable) to adjust a position of the nozzle relative to the occupant.

Clause 11: the seat defined in any one of clauses 7-10 wherein the conduit extends from the base of the seat to the headrest.

Clause 12: the seat defined in any one of clauses 7-11 wherein the manifold extends across a rear portion of the seat.

Clause 13: a method, comprising: providing air to an air supply duct associated with a cabin of a vehicle, the air supply duct being fluidly coupled to a manifold that extends to a passenger seat of the cabin; and directing air from the manifold to a nozzle positioned to face forward of a face of an occupant when the occupant occupies a respective one of the occupant seats.

Clause 14: the method defined in clause 13, further comprising pivoting a nozzle mount supporting the nozzle based on the height of the occupant.

Clause 15: the method defined in clause 13 or 14, wherein the manifold extends between a plurality of passenger seats in a row of the cabin.

Clause 16: the method defined in any one of clauses 13-15 further comprising filtering air of the air supply duct.

Clause 17: a method, comprising: coupling a manifold to a seat of a cabin of a vehicle, the manifold to be fluidly coupled to an air supply duct associated with the cabin; fluidly coupling a nozzle to a manifold; and positioning the nozzle such that air from the air supply duct is directed towards the front of the face of the occupant when the occupant occupies the seat.

Clause 18: the method defined in clause 17, further comprising coupling a conduit between the manifold and the nozzle, the conduit extending along a height of the seat.

Clause 19: the method defined in clause 17 or 18, further comprising coupling a filter to the air supply conduit.

Clause 20: the method defined in any one of clauses 17-19, wherein the manifold is positioned rearward of the seat.

The following claims are hereby incorporated by reference into this detailed description, with each claim standing on its own as a separate embodiment of the disclosure.