The field of the invention relates to passenger seats or the like, and more particularly to deployable leg rests for use with passenger seats.
Many passenger seats such as those on passenger aircraft, busses, trains, and the like are designed with a recline function to allow for greater comfort to passengers, particularly on longer journeys. To increase passenger comfort, seats may be designed with complex articulations, including different motions for the seat back and seat bottom or pan.
In some instances, a passenger seat may include a leg rest to support the passenger's calves, feet, or thighs when they are in a reclined position. These leg rests are typically mounted to a solid part of the passenger seat structure. For example, a leg rest may be mounted directly to a stationary part of the seat frame or to a seat tube. It is desirable to include a leg rest on a reclining seat to increase passenger comfort. The conventional method of mounting a leg rest to a reclining passenger seat has a number of disadvantages. The addition of a leg rest mounted to the seat tube or other stationary part of the passenger seat adds additional mounting hardware and linkages that may encroach on the mounting hardware and linkages for the seat back and seat bottom. Additional hardware may also be necessary to coordinate the motion of the seat back, seat bottom, and leg rest during seat recline.
Because of the additional hardware, the addition of more moving parts to a reclining seat, like a leg rest, often times leads to compromises in the range and type of motion available to each individual seat component. Not only do the additional mechanical parts restrict motion, but allowances for complementary ranges of motion for different portions of the passenger seat further diminishes available motion to avoid impingement of the portions of the passenger seat on one another.
In certain cases, it may be desirable to provide a passenger seat with a deployable leg rest that is coupled directly to the seat bottom. This arrangement may allow the leg rest to move and articulate with the seat and pivot and/or extend away from the seat bottom during deployment. The resulting mechanism, including an actuator to initiate and deploy the leg rest, is often simpler, lighter, and more compact than existing leg rest mechanisms. Such an integrated leg rest may allow for a greater range of movement for the seat back and seat bottom by reducing the amount of hardware contained under and within the seat and moving with the seat bottom to avoid interference with other reclining mechanisms and hardware.
The terms “invention,” “the invention,” “this invention” and “the present invention” used in this patent are intended to refer broadly to all of the subject matter of this patent and the patent claims below. Statements containing these terms should be understood not to limit the subject matter described herein or to limit the meaning or scope of the patent claims below. Embodiments of the invention covered by this patent are defined by the claims below, not this summary. This summary is a high-level overview of various aspects of the invention and introduces some of the concepts that are further described in the Detailed Description section below. This summary is not intended to identify key or essential features of the claimed subject matter, nor is it intended to be used in isolation to determine the scope of the claimed subject matter. The subject matter should be understood by reference to appropriate portions of the entire specification of this patent, any or all drawings and each claim.
According to certain embodiments of the present invention, a passenger seat may comprise a deployable leg rest coupled to a seat bottom and an actuator coupled to the deployable leg rest and the seat bottom. The actuator may induce deployment of the deployable leg rest.
In some embodiments, the seat bottom is moveable during the reclining of the passenger seat.
In some embodiments, the actuator may comprise a gas-charged cylinder.
In certain embodiments, the actuator may comprise a spring.
In some embodiments, the spring may comprise a coil spring.
In certain embodiments, the spring may comprise a torsion spring.
In some embodiments, the actuator may comprise a spring in combination with a gas-charged cylinder.
In some embodiments, the passenger seat further comprises a control button to initiate deployment of the deployable leg rest.
In certain embodiments, the passenger seat further comprises a locking mechanism to maintain the position of the deployable leg rest in a deployed position, a stowed position, or any intermediate position.
In some embodiments, the locking mechanism may comprise a ratchet.
In certain embodiments, the locking mechanism may comprise a clutch.
In some embodiments, the clutch may comprise a force-limiting clutch.
In some embodiments, the clutch may comprise a one-way clutch.
In certain embodiments, the actuator may comprise an electrically powered actuator.
In some embodiments, the electrically powered actuator may comprise an electric motor and gearing system to provide a torque to the deployable leg rest.
In certain embodiments, the electrically powered actuator may comprise an electric motor and lead screw.
In certain embodiments, the actuator may provide a deploying force to deploy the deployable leg rest.
In some embodiments, the actuator may provide a retracting force to retract the deployable leg rest.
In some embodiments, the deployable leg rest may rotate and extend between a stowed position and a deployed position.
According to certain embodiments of the present invention, a passenger seat may comprise a deployable leg rest coupled to a seat bottom, a gas-charged cylinder providing a motive force, a locking mechanism, and a control button in communication with the locking mechanism. The gas-charged cylinder may be coupled to the deployable leg rest and the seat bottom and the locking mechanism may lock the deployable leg rest in a stowed position. The control button may release the locking mechanism and allow the motive force of the gas-charged cylinder to deploy the deployable leg rest.
The subject matter of embodiments of the present invention is described here with specificity to meet statutory requirements, but this description is not necessarily intended to limit the scope of the claims. The claimed subject matter may be embodied in other ways, may include different elements or steps, and may be used in conjunction with other existing or future technologies. This description should not be interpreted as implying any particular order or arrangement among or between various steps or elements except when the order of individual steps or arrangement of elements is explicitly described.
The described embodiments of the invention provide a deployable leg rest for reclining passenger seats. While the leg rests are discussed for use with aircraft seats, they are by no means so limited. Rather, embodiments of the leg rest may be used in passenger seats or other seats of any type or otherwise as desired.
In some embodiments of the present invention, as shown in
Still referring to
Still referring to
In certain embodiments, the actuator 20 may take on any number of different mechanisms or configurations. For example, the actuator 20 may be a spring mechanism. The actuator 20 may comprise a linear spring, such as a coil spring, that is mounted or attached to the deployable leg rest 10 and seat bottom 30 in a similar manner as that shown in
In some embodiments, the actuator 20 may comprise an electrically powered actuator. Electric actuators may either provide a rotational or linear force to the deployable leg rest 10. In certain embodiments, the electric actuator may comprise an electric motor coupled to the leg rest hinge 15 either directly or through a gearing system. In other embodiments, the actuator 20 may be an electrically powered linear actuator. For example, an electric motor may be coupled to a lead screw or lead screw collar. An electric motor may then rotate either the lead screw or the lead screw collar to cause an extension or retraction of the lead screw. The extension or retraction of the lead screw may provide a linear motion that deploys or stows the deployable leg rest 10. Electrically powered actuators may offer a number of advantages over other mechanical actuator systems. In some embodiments, the electrically powered actuators may not require the use of a locking mechanism or actuator release 21 because the electric motor or gearing system provides a locking function without the use of an extra component. Also, in certain embodiments, the electrically powered actuator may provide both deploying and stowing forces to move the deployable leg rest 10 in both directions without the need for a passenger to exert any pressure on the deployable leg rest 10 or overcome the force of a purely mechanical actuator 20.
In certain embodiments, the integrated deployable leg rest 1 may include a number of different locking and release mechanisms to selectively hold or allow for the movement of the deployable leg rest 10. As shown in
Additional locking mechanisms may be useful or preferable in other embodiments of the present invention. For example, a one-way clutch may be used in a similar manner as the ratchet locking mechanism described above. In some embodiments, a force-limiting clutch may provide certain advantages and additional functionality. Force-limiting clutches provide a certain degree of locking force that, once exceeded, will release the clutch or allow for slippage between clutch elements. A force-limiting clutch may be used to stabilize the deployable leg rest 10 up to a certain amount of force or pressure, but break away and allow movement if that amount of force or pressure is exceeded. In the case of a deployable leg rest 10, a force-limiting clutch may be used to lock the deployable leg rest 10 into a desired position under normal circumstances and use. However, if the amount of locking force provided by the force-limiting clutch is exceeded, like when a passenger may attempt to stand on the deployable leg rest 10, the force-limiting clutch will slip or release and allow the deployable leg rest 10 to move and prevent damage to the deployable leg rest 10, actuator 20, or other parts of the passenger seat.
In certain embodiments, the motion of the deployable leg rest 10 may not be exclusively rotational about an axis. The deployable leg rest 10 may rotate, translate, or both rotate and translate through a range of motion between a stowed and deployed position. In some embodiments, the connection between the deployable leg rest 10 and the seat bottom 30 may include a rotating element, such as a hinge, and a translating element like a carriage and track.
Any of the above described components, parts, or embodiments may take on a range of shapes, sizes, or materials as necessary for a particular application of the described invention. The components, parts, or mechanisms of the described invention may be made of any materials selected for the suitability in use, cost, or ease of manufacturing. Materials including, but not limited to aluminum, stainless steel, fiber reinforced plastics, composites, polycarbonate, polypropylene, other metallic materials, or other polymers may be used to form any of the above described components.
Different arrangements of the components depicted in the drawings or described above, as well as components and steps not shown or described are possible. Similarly, some features and sub-combinations are useful and may be employed without reference to other features and sub-combinations. Embodiments of the invention have been described for illustrative and not restrictive purposes, and alternative embodiments will become apparent to readers of this patent. Accordingly, the present invention is not limited to the embodiments described above or depicted in the drawings, and various embodiments and modifications may be made without departing from the scope of the claims below.
This application is the U.S. national phase entry of International Patent Application Serial No. PCT/US2015/024123 (“the '123 application”), filed on Apr. 2, 2015, which application is related to and claims priority benefits from U.S. Provisional Application Ser. No. 61/974,492 (“the '492 application”), filed on Apr. 3, 2014, entitled “Deployable Legrest that Moves with the Seat Pan”. The '123 and '492 applications are hereby incorporated in their entireties by this reference.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/US2015/024123 | 4/2/2015 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2015/153902 | 10/8/2015 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
1704585 | Astruc | Mar 1929 | A |
3226155 | Whiteford | Dec 1965 | A |
3339971 | Fletcher | Sep 1967 | A |
3695685 | Lamb | Oct 1972 | A |
4113311 | Reida | Sep 1978 | A |
4509795 | Brennan | Apr 1985 | A |
4521053 | de Boer | Jun 1985 | A |
4819987 | Stringer | Apr 1989 | A |
4966413 | Palarski | Oct 1990 | A |
5098158 | Palarski | Mar 1992 | A |
5352020 | Wade | Oct 1994 | A |
5447359 | Asbjornsen | Sep 1995 | A |
5507562 | Wieland | Apr 1996 | A |
5527095 | Marshall | Jun 1996 | A |
5651587 | Kodaverdian | Jul 1997 | A |
5755493 | Kodaverdian | May 1998 | A |
6045190 | Ward | Apr 2000 | A |
6194853 | Tual | Feb 2001 | B1 |
6227489 | Kitamoto | May 2001 | B1 |
6237994 | Bentley | May 2001 | B1 |
6336679 | Smuk | Jan 2002 | B1 |
6439636 | Kuo | Aug 2002 | B1 |
6441576 | Marin-Martinod | Aug 2002 | B1 |
6526643 | Renault | Mar 2003 | B1 |
6764137 | Menard | Jul 2004 | B2 |
6773074 | Flory | Aug 2004 | B2 |
6926366 | Wolters | Aug 2005 | B2 |
7004542 | Saint-Jalmes | Feb 2006 | B2 |
7293839 | Shimizu | Nov 2007 | B2 |
7597398 | Lindsay | Oct 2009 | B2 |
7614693 | Ito | Nov 2009 | B2 |
7669928 | Snyder | Mar 2010 | B2 |
7950743 | Clausen | May 2011 | B2 |
8016355 | Ito | Sep 2011 | B2 |
8167370 | Arakawa | May 2012 | B2 |
8366194 | Yamamoto | Feb 2013 | B2 |
8608240 | Marshall | Dec 2013 | B2 |
8882190 | Garland | Nov 2014 | B2 |
20020063449 | Plant | May 2002 | A1 |
20020113477 | Uchiyama | Aug 2002 | A1 |
20030075966 | Behnert | Apr 2003 | A1 |
20030080597 | Beroth | May 2003 | A1 |
20030209924 | Bauer | Nov 2003 | A1 |
20040099766 | Pratt, Jr. | May 2004 | A1 |
20040100137 | Johnson | May 2004 | A1 |
20040100138 | Johnson | May 2004 | A1 |
20040189074 | Seki | Sep 2004 | A1 |
20050012377 | Ito | Jan 2005 | A1 |
20060087158 | Kramer | Apr 2006 | A1 |
20060158015 | Tsuji | Jul 2006 | A1 |
20070262635 | Johnson | Nov 2007 | A1 |
20090322137 | Kojima | Dec 2009 | A1 |
20100052395 | Anglese | Mar 2010 | A1 |
20100187881 | Fujita | Jul 2010 | A1 |
20100194169 | Shinozuka | Aug 2010 | A1 |
20100244534 | Driessen | Sep 2010 | A1 |
20100320819 | Cohen | Dec 2010 | A1 |
20110215200 | Mejuhas | Sep 2011 | A1 |
20110240797 | Behe | Oct 2011 | A1 |
20110241391 | Lamparter | Oct 2011 | A1 |
20120228919 | Dowty | Sep 2012 | A1 |
20130249190 | Engman | Sep 2013 | A1 |
20130320139 | Cho | Dec 2013 | A1 |
20170088268 | Kinard | Mar 2017 | A1 |
20170096225 | Smith | Apr 2017 | A1 |
20170174345 | Murnan | Jun 2017 | A1 |
Number | Date | Country |
---|---|---|
2011070531 | Jun 2011 | WO |
2015153902 | Oct 2015 | WO |
Entry |
---|
International Patent Application No. PCT/US2015/024123, Search Report and Written Opinion dated Jul. 16, 2015. |
International Patent Application No. PCT/US2015/024123, International Preliminary Report on Patentability, dated Oct. 13, 2016. |
Number | Date | Country | |
---|---|---|---|
20170096225 A1 | Apr 2017 | US |
Number | Date | Country | |
---|---|---|---|
61974492 | Apr 2014 | US |