READILY CONVERTIBLE AIRCRAFT PASSENGER SEATS

Abstract: Aircraft passenger seat frames (62) having legs (56) fixed in place in the aircraft and with the seat frames. Each seat frame has generally horizontal supporting members (66, 68, 74, 76) having their opposite ends secured in seat end webs (70, 72, 78, 80). Tubes (84, 86) are associated with each of the seat end webs of the plurality of seat frames in a supporting relationship, the legs (56) being connected to the tubes to support the seat frames. The tubes have a tube-in-tube slip joint (88, 90) at least at one outside end of one seat frame on which the seat can be moved toward or away from an adjacent seat frame to change the fare class size of the seat frames.

Description: Technical Field The invention relates to easily convertible passenger seating arrangements whereby tourist class seats may be converted to business class seats, and vice versa, as needed depending upon the specific passenger mix make-up for an individual flight. Background Art In the prior art aircraft passenger seats have been converted to different fare class sizes making substantial changes in the seats, including adding parts, and/or removing the entire seats and replacing them with seats of different sizes. Such changes required excessive time and usually could not be made by the flight crew. In the present flight operations there is a need to frequently change tourist class seats and business class seats. This type of change has been accomplished physically by removing one class and installing the other, usually during overnight maintenance. Such a lengthy change requirement is not practical in present flying operations. A search of the patent literature discloses a number of seating arrangements. For example, U.S. Patent No. 3,893,729 to Sherman et al. teaches a combination of adjacent passenger seats for an aircraft which are convertible to different fare class sizes. This known combination comprises a support frame carrying a plurality of juxtaposed seats, presumably having frames. The support frame comprises two parallel inner small diameter tubes and a plurality of pairs of outer large diameter tubes, the outer tubes carrying the seats and each outer tube having two lugs that are connectable to supporting legs fixed in place in the aircraft. The inner end outer tubes form tube-in-tube slip joints, on which adjacent seats can be moved toward or away from each other, to change the fare class size of the seats. The inner and outer tubes are locked with respect to each other by connecting one of the lugs of each outer tube to one of the fixed legs, and released by disconnecting the lugs from their associated legs. During conversion from a coach configuration into a first class configuration, two seats in an eight seat row are removed and the remaining adjacent seats are moved further apart, and short segments of cushion are added between adjacent seats. The removed seats may be stored in the aircraft's cargo compartment. The following other patents found in the search disclose other seating arrangements: U.S. Patent No. Inventor 3,374,032 F.J. Del Giudice 3,480,240 F.J. Del Giudice 3,637,253 Maule et al. 3,743,351 Harris 3,877,747 Brennan et al. 3,910,632 Marechal 4,533,175 Brennan Disclosure of the Invention The invention has for its object to provide a combination of adjacent passenger seats for an aircraft which are easily convertible to different fare class sizes, without the need of having to remove and store entire seats. To this end, the invention includes a combination of adjacent passenger seats for an aircraft, said seats being convertible to different fare class sizes, said combination comprising: a plurality of juxtaposed seat frames, each having generally horizontal supporting members having their opposite ends secured in seat frame end webs, and at least one generally horizontal tube; said tubes forming a tube-in-tube slip joint at least at one outside end of one seat frame on which the one seat frame can be moved toward or away from an adjacent seat frame to change the fare class size of the seat frames; said tube-in-tube slip joint having an outer large diameter tube and an inner small diameter tube in slidable engagement therewith; said inner tube being in connective support with a seat end web at said one outside end of the one seat frame, and said outer tube being connected to supporting legs fixed in place in said aircraft; an inner web of said one seat frame having at least one collar attached thereto in which said outer tube is in slidable supportive engagement; and a locking and releasing mechanism at said one end of said one seat frame to lock and release said inner and outer tubes with respect to each other. Particularly advantageous embodiments of the invention form the subject matter of the dependent claims 2-8. Further advantages of the invention may be brought out in the following part of the specification wherein small details have been described for the competence of the disclosure, without intending to limit the scope of the invention which is set forth in the appended claims. Brief Description of the Drawings Referring to the accompanying drawings which are for illustrative purposes: Fig. 1 is a front elevational view of a row of seven tourist class seats in an aircraft, there being two combinations of outer pairs of seats and a combination of three center seats spaced from the outer seats by two aisles; Fig. 2 is a front elevational view of a conversion of the tourist seats in Fig. 1 to business class seats in which there are two pairs of outer business class seats and a pair of centered business class seats spaced from the outer seats by two aisles; Fig. 3 is a front elevational view of two tourist class seats and their frames; Fig. 4 is a front elevational view of the seats in Fig. 3 spaced apart to be in the form of business class seats; Fig. 5 is a pictorial view of a combination of two tourist seats as shown in Fig. 3; Fig. 6 is a pictorial view of a combination of two business class seats as shown in Fig. 4; Fig. 7 is a pictorial schematic view of the seat frames of the seats shown in Fig. 6; Fig. 8 is a side elevational view of the combination of two seats as shown in Figs. 5 or 6. Fig. 9 is a side elevational fragmentary detail view of a locking and release mechanism as used in converting the seats from one fare class to another; Fig. 10 is a fragmentary plan view of the locking and releasing mechanism shown in Fig. 9; Fig. 11 is a fragmentary view taken along the lines 11--11 in Fig. 10; Fig. 12 is a front elevational view of a combination of three center seats and their seat frames in the tourist class arrangement; Fig. 13 is a front elevational view of the seats shown in Fig. 12 converted into two business class seats; Fig. 14 is a pictorial view of three center tourist class seats as shown in Fig. 12; Fig. 15 is a pictorial view of two centered business class seats as shown in Fig. 13; Fig. 16 is a pictorial view of the seat frame details of the three centered sheets substantially as shown in Fig. 12; Fig. 17 is a side elevational view of the seats as shown in Fig. 12; Fig. 18 is a side elevational view of the inner seat, taken along lines 18--18 in Fig. 13; and Fig. 19 is a fragmentary view of the details of the outer armrest as shown in Fig. 12. Best Mode for Carrying Out the Invention Referring again to the drawings, there is shown in Figs. 1 and 2 an aircraft body 10 in cross section having a row of aircraft passenger seats, convertible from tourist class to business class and vice versa. In Fig. 1 there are seven seats comprised of two pairs of outer seats 12A and 14A and a combination of three center seats 16A, the outer seats being adjacent the aircraft sidewalls and spaced from the center seats by aisles 18A and 20A. These seats are in the form of low fare seats such as tourist class and each seat and back have the same widths. In Fig. 2 the seats in Fig. 1 have been converted to a higher fare-type such as business class seats. Here the two pairs of outer seats 12B and 14B are the same size as those in Figs. 1 but are spaced apart to provide more room outwardly of the center armrest 24. The combination of center seats 16B has been converted from three seats into two seats with the inner armrests 26, Fig. 1, removed and a center armrest 30 being provided by having a portion of the center back 32 being folded downwardly. For example, in Fig. 1 the outer seats measured from the outer ends of the armrests 36 and 38, occupy 1,09 metres (forty-three inches) and the center seats measured from the outer ends of the armrests 42 and 44 occupy 1,50 metres (fifty-nine inches). In Fig. 2 the distance between the outer ends of the armrests 36 and 38 has been increased to 1,22 metres (forty-eight inches), and the center seats, having been reduced to two, the outer ends of the armrests having been reversed to extend over the aisle seats, have a distance of 1,30 metres (fifty-one inches) therebetween. Thus, the pairs of outer seats have been increased by 12,7 cm (five inches) in width and the two center seats in Fig. 2 have been reduced 20,3 cm (eight inches) from the three center seat requirement to 1,30 metres (fifty-one inches). The aisles in Fig. 2 are 2,5 cm (one inch) smaller in width than the aisles in Fig. 1. In Figs. 3-11 the outer seats in the form of 14A and 14B are shown in detail. The seats 14A and 12A are identical except that they are reversed in that they expand and are contracted toward and away from the aisles. All of the seat cushions 48 and the back cushions 50 are the same and move with the seat frames on which they are positioned and in which the conversion occurs. Each of the individual seats in combination form, as shown in Figs. 3, 4 and 7 are substantially identical. The conversion mechanism, generally indicated as 52, is best seen in Figs. 7, 9 and 11. In Figs. 5 and 6, outside combination seats 12A and 12B are shown in pictorial view destinct from the same combination shown in Figs. 1 and 2. In Fig. 7 the seat frame combination 12C is shown in the expanded or extended form and illustrates the result of the frame movement as indicated in 12B in Figs. 2, 4, and 6, the movement or extension having been toward the aisle 18B. The combination of seat frames as 12C are supported on two sets 5 of legs 54 and 56, fixed in place with respect to the frames and fixed in place in tracks 58, Figs. 3 and 4 in the aircraft. The frames as 12C are comprised of a combination of a plurality of seat frames, generally designated as 60 and 62, the latter being an aisle frame. The combination of frames 60 and 62 thus supports two convertible seats. Seat frame 60, Figs. 3, 4, 6, and 7, has a pair of tubular horizontal supporting members 66 and 68 secured to inner and outer generally vertical seat webs 70 and 72, and in the same manner seat frame 62 has a pair of tubular generally horizontal supporting members 74 and 76 secured to inner and outer generally vertical end webs 78 and 80, also Figs. 9 and 10. Associated with each of the end webs 70, 72, 78 and 80 are a pair of juxtaposed first tubes 84. The first tubes 84 are comprised of outer large diameter tubes 88 and inner small diameter tubes 90 to form tube-in-tube slip joints on which an outside end or aisle end of the seat frames may be moved toward or away from the juxtaposed seat frame to change the fare class size of the seats from tourist to business class and vice versa. The outer large diameter tubes 88 are fixed to the seat legs in a conventional manner at 92 and 94. The outer large diameter tubes 88 are also secured to the seat frame 60 by means of collars 96 and 98 which are secured to end webs 72 and 70, Figs. 3 and 4. Collars 100 and 102 are fixed to end web 78, Fig. 7. The end web 78 and the collars 100, 102 are slidably engaged with the large diameter tubes 88 so as to be able to slip over them. The collars 100, 102 on the web 78 provide additional support for the seat frame 62. Small diameter inner tubes 90 are secured to the end web 80, Figs. 3, 4, and 10, and provide additional support in the collars 104 and 106 secured to the end web. Thus, the legs directly support the first tubes 84, comprised of the tubes 88 and 90, and in turn support the four end webs. In Figs. 7 and 9-11 the locking and releasing mechanism 52 is shown in detail. In the inner tubes 90 there are slots 110 and 112, and extending through the outer tubes and the slots are bolts 114 and 116, respectively, which limit the movement of the inner tubes in the outer tubes. As shown in Fig. 10, the inner tubes and the slots have been moved outwardly as far as possible, and when the inner tubes are moved inwardly to convert the seats to tourist class, the slots are moved so that their other ends abut the bolts 114 and 116. On the inside of the outer tubes there are two cylindrical openings 118, 120, and 122 and 124 and each of the inner tubes has a cylindrical opening 126 and 128 which are adapted to mate with cylindrical openings in the outer tubes depending upon the position of the inner tubes with respect to the outer tubes. The locking and release mechanism has a handle 132 which is normally fitted within a seat end plate 134 outwardly of the end web 80 and attached to the handle and extending inwardly therefrom is an actuating rod 136. Inwardly of the handle there is a generally cylindrical stop 140 to position the handle in place with the stop against the end web 80 where it is normally held by a coil spring 142, surrounding the rod 136 and adapted to abut the end web 80, having its other end abut a pin held washer 144. The rod 136 extends into a housing 146 of the mechanism 52. As shown in Fig. 10 the housing 146 is supported by the outer tubes 88 and slides on these tubes when the configuration is changed. The inner end of the rod 136 is pivotally connected to a crank 150, having a cylindrical opening 152 so as to be secured around a cylinder 154 supported for rotation within the housing 146. Extending outwardly from the opposite ends of the cylinder are pins 158 and 160, adapted to extend into the cylindrical openings 118, 120, 122, 124, 126 and 128 in the inner and outer tubes. The pins extend outwardly from plugs 162 and 164 which are slidably engaged in and adjacent the opposite ends of the cylinder 154. In the space between the plugs is a coil spring 166 which holds the pins in their positions outwardly of the cylinder and in the holes to lock the seat frames in their retracted and extended positions. The cylinder 154 has two generally spirally directed slots 170, only one shown, radially outwardly of the plugs 164 and 162 and connected to the plugs extending into the slots are pins 172, one shown. When the handle 132 is pulled away from the seat, the rod 162, Fig. 11, is moved linearly to rotate the cylinder 154 counterclockwise to move the pins 172 downwardly in Fig. 10 so as to withdraw the pins 158, 160 from the inner and outer tubes. The seats then may be converted from one class to the other and in Fig. 4, the inner tubes 90 may be moved inwardly so as to retract the seats and change them into the tourist class. As the tubes are moved inwardly until the outer end of the slots 110 and 112 move into abutment with the bolts 114, 116, the pins 158, 160 will then be in register with the cylindrical holes 118 and 120 and the holes in the inner tubes. At this time the handle 132 will be moved inwardly so as to rotate the cylinder 154 to cause the pins 158 and 160 to enter the holes 118 and 120 in the outer tubes and the holes 126 and 128 in the inner tubes so as to lock the seat frames in the retracted position, as shown in Fig. 3. The spring 166 holds the pins in a locked position and the spring 142 holds the handle 132 in a locked position. As shown in Figs. 3-8, the center armrest 24 is supported on a plate 176 and adjacent its lower end it has two openings in which sleeves 178 and 180 extend. Sleeves 178 and 180 are slidably supported in the tubular supporting members 68, 76, and 66 and 74, respectively. Sleeves 180 and 178 have slots 182 and extending into the slots are pins 184 fitted in the supporting tubes 66 and 68. In the tubes 66 and 68, inwardly of the sleeves 178 and 180 are coil springs 186, only one shown, abutting the sleeves on their inner ends. Pins 188 extend through each of the tubes 66 and 68 to retain the springs. As shown in Fig. 4, where the seat frames are in the extended position, the spring 186 is holding the sleeves 178 and 180 in the supporting tubes 74 and 76 so that one end of the slot abuts the pin 184. The armrest supporting plate 176 is then moved to a central position on the sleeve where it fits snugly and is held in place by the spring 186. When the seat frames are retracted as shown in Fig. 3, the inner tubes 90 slide in the outer tubes 88 and the inner end web 78 and the collar 100, attached thereto, slide on the outer tubes 88 so as to move the supporting plate 176 of the armrest into abutment with the inner end of the seat frame 60 so as to move the sleeves 178 and 180 into the supporting tubes 66 and 68 and the slot 182 so that its other end is in abutment with the pin 184. The outer armrests 36 and 38 are secured to the respective seat frames 60 and 62 and to supports 192 inwardly of outer plates 134. The supports 192 are secured to the end webs by conventional means as shown. As shown in Figs. 3-5, 7 and 8, extending downwardly from the outer ends of the seat frames are luggage restraining rails 200 which are telescoped at 202 so as to be extendible and retractable inaccordance with the conversion of the seat frames to different fare classes. The seat frames 60 and 62, Fig. 7, have identical back frames 204 on which the back cushions are fitted. As shown, the back frames move with the seat frames when the seats are converted from one fare class to another. The frame backs are adjusted by devices 206. The centered three-to-two seat combination is shown in Figs. 12-19. The three seat tourist class arrangement is shown in Figs. 12, 14 and partially in Fig. 16 where conversion has taken place in part, note the withdrawn handle 132. Two sets of seat frame legs 210 and 212 are fixed in place and are fixed in supporting engagement with a second set of seat frame tubes, generally designated as 214, and comprised of two outer large diameter tubes 216 having inner tubes 218 slidably engaged therein at the opposite outer ends of the outer tubes. The combination of second tubes 214 support three combined seat frames, generally designated as 220, 222 and 224. Frame 220 has an aisle web 226 and an inner web 228; frame 222 has outer webs 230 and 232 and two internal webs 234 and 236; and frame 224 has an internal end web 238 and an aisle web 240. The two pairs of inner tubes 218 are fixed to aisle web 226 and collars thereon 244 and aisle web 240 and collars 246 thereon, respectively. The two outer tubes 216 are fixed to the outer webs 230 and 232 of inner frame 222 and to collars 250 and 252 attached thereto, respectively. The outer tubes are also fixed to internal webs 234 and 236 and to collars 256 and 258 attached thereto, respectively. The outer tubes 216, are slidably engaged in internal webs 228 and 238 and to collars 260 and 262 attached thereto, respectively. The latter collars add to the supporting arrangement of the slidable engagement of the tubes with the webs. Extending between and secured to the end webs 226 and 228 are two horizontal tubular supporting members 264 and 266, Fig. 16. Horizontal support members 268 and 270 are secured to end webs 232 and 230 and extend through webs 234 and 236. Horizontal support members 272 and 274 extend between end webs 238 and 240 and are secured thereto. Secured within one end of supporting tubes 268 and 270 are a pair of armrest support sleeves 276. The support sleeves extend into supporting members 264 and 266 in which they are slidably engaged. At the other end of supporting members 268 and 270 are identical support sleeves 280, slidably engaged in supporting members 272 and 274. Center armrests 26, shown in Figs. 12, 14, and 17, in the tourist class arrangement, are supported by posts 286 and 288, having plugs 290 which are removably engaged in sleeves 276, and 280. The extension and locking mechanism 52 shown in Figs. 10 and 11, as used in the combination of outside seat frames, is of the same type used in the center combination of three seat frames and operates in the same manner but has different dimensions as necessary for the different embodiments. In Figs. 12 and 13, holes 292 adapted to receive the outer pins as 158 and 160, Fig. 10, are shown at both ends of the large diameter second tubes 216. In Fig. 12 in the three seat arrangement, the seat frames are in the extended position, the inner tubes 218 extending substantially more outwardly than in Fig. 13. The seat webs 238 and 232 and the seat webs 230 and 228 are spaced whereas in Fig. 13 they have been moved closely together so that the outer seat cushions 48, which are the same as those in the two frame combination, are in contact with inner seat cushion 48. In Fig. 13 the inner armrests 26 have been removed and the sleeves 276 and 280 have been extended farther into the supporting tubes 264, 266 and 272, 274, respectively. The outer or aisle seat back frames 204, Fig. 16, are the same as those shown in Fig. 7 in the two seat frame combination. The center seat back frame 32A has a different configuration in that part folds downwardly and forms a center armrest 30, Figs. 1, 13, 15, 16 and 18. As in the two seat combination, the seat back frames move with the seat frames. As shown in Figs. 12 and 13, at the upper end of the center seat there are horizontally movable pins 300. When the outer or aisle seats are moved inwardly to generally abut the inner seat, the pins 300 are moved into the seat back cushions 50 of the outer seats to adjoin the spaced elements 302 of the center seat back to the outer seat backs 50. As stated, to move the outer seat frames 220, 224 inwardly to form the business class double seats, the armrests 26 must be removed and stored. They may be stored in an arranged storage under the seat frames or in the backs thereof. As best seen in Fig. 18, the center armrest 30 for the business class seats is moved downwardly from the back on a hinge 304. The center seats also have mechanisms 206 for adjusting the seat backs. To change the seats from one fare class to the other, the handles 132 may be pulled outwardly into the aisles 18A, 18B and 20A, 20B by members of the flight crew and the seat frames may be moved inwardly and outwardly to retract or extend as the case may be. This operation is made clear in Figs. 10 and 11. It should be noted that when the outer seats 12A and 12B are extended from the positions, shown in Fig. 1 and Fig. 3, to the extended positions, shown in Fig. 2 and Fig. 4, aisle space 18B and 20B would tend to be reduced but when the inner seats 16A are moved to make two business class seats 16B, the position is changed from that shown in Fig. 12 to that shown in Fig. 13. This conversion from three seats to two seats tends to make the aisles 18B and 20B larger. To add additional space to the aisles, the armrests 42A and 44A, Fig. 19, have removable U-shaped caps 306 supported on a hinged plate 308, engaged with armrest support 310. When the caps 306 are removed, the hinge plate 308 may be lifted and moved inwardly so as to be rotated 180°. The result of this adjustment is illustrated in Figs. 2 and 13 where the armrest 42B and 44B extend inwardly with the caps 306 having been placed on top of the adjusted hinge 308 extending inwardly over the seats. As stated, this results in increasing the aisles 18B and 20B by 5,1 cm (two inches) and has a final result of making each of the aisles 2,5 cm (one inch) smaller than 18A and 20A as shown in Fig. 1. The invention and its attendant advantages will be understood from the foregoing description and it will be apparent that various changes may be made in form, construction, and arrangements of the parts of the invention without departing from the spirit and scope thereof or sacrificing its material advantages, the arrangements hereinbefore described being merely by way of example. I do not wish to be restricted to the specific form shown or uses mentioned except as defined in the accompanying claims.

Claims: A combination (12,14;16) of adjacent passenger seats for an aircraft, said seats being convertible to different fare class sizes, said combination (12,14;16) comprising: a plurality of juxtaposed seat frames (60,62;220-224), each having generally horizontal supporting members (66,68,74,76;264-274) having their opposite ends secured in seat frame end webs (70,72,78,80,226-240), and at least one generally horizontal tube (88,90;216,218); said tubes (88,90;216,218) forming a tube-in-tube slip joint at least at one outside end of one seat frame (62;220,224) on which the one seat frame (62,220,224) can be moved toward or away from an adjacent seat frame (60;222) to change the fare class size of the seat frames (60,62;220-224), said tube-in-tube slip joint having an outer large diameter (88;216) tube and an inner small diameter tube (80,218) in slidable engagement therewith; said inner tube (90;218) being in connective support with a seat end web (80;226,240) at said one outside end of the one seat frame (62;220,224), and said outer tube (88;216) being connected to supporting legs (54,56;210,212) fixed in place in said aircraft; an inner web (78;228,238) of said one seat frame (62;220,224) having at least one collar (100,102;260,262) attached thereto in which said outer tube (88;216) is in slidable supportive engagement; and a locking and releasing mechanism (52) at said one end of said one seat frame (62;220,224) to lock and release said inner and outer tubes (90,88,218,216) with respect to each other. The passenger seat combination (12,14;16) according to claim 1, including: a translatable armrest (24) being fitted between and for two of said juxtaposed seat frames (60,62); said armrest (24) being fitted on an upper end of a translatable plate (176) and the lower end of said plate (176) being fitted to sleeves (178,180) slidably engaged in said supporting members (66,74,68,76) of said two seat frames (60,62); said armrest (24) and plate (176) being translatable to be closely adjacent to said seat frames (60,62) when a seat frame (62) has been moved toward a juxtaposed seat frame (60) so as to be proximate thereto and said sleeves (178;180) have been moved in said supporting members (66,74,68,76) towards said juxtaposed seat frame (60); said plate (176) being translatable to be spaced between said two seat frames (60,62) when a seat (62) has been moved away from a juxtaposed seat frame (60) and said sleeves (178,180) have been moved in said supporting members (66,74,68,76) away from said juxtaposed seat frame (60); and means (182-188) in said supporting members (66,74,68,76) to maintain said plate (176) to be spaced between said seat frames (60,62). The passenger seat combination (12,14;16) according to claim 1 or 2, in which: said locking and releasing mechanism (52) has an operating handle (132) adjacent said one end of said one seat frame (62,220,224); one end of an operating rod (136) is connected to said handle (132) and the other end of the rod (136) is connected to rotary means (150-154) and locking pins (158,160); said rotary means (150-154) being rotatable by linear movement of the rod (136) when the handle (132) is pulled outwardly of the one end of the seat frame (62;220,224) to withdraw the locking pins (158,160) from the tubes (88,90;216,218) so as to release the inner and outer tubes (90,88;218,216) from each other to permit the inner tubes (90;218) to be slidable within the outer tubes (88,216); said locking pins (158,160) being movable to a locking position with respect to the innner and outer tubes (90,88;218,216) when the handle (132) is moved inwardly to its position adjacent said one end of said one seat frame (62;220,224). The passenger seat combination (12,14;16) according to any of the preceding claims, wherein said plurality of seat frames (60,62;220-224) is a combination of three seat frames (220-224) in a row, having two sets of legs (210,212) fixed thereto. The passenger seat combination (12,14;16) according to claim 4, in which: said outer seat frames (220,224) in the three seat combination are spaced from the inner seat frame (222) in a smaller seat frame, lower fare arrangement; inner armrests (26) being positioned in the spaces between inner (222) and outer seat frames (220,224); inner armrest supports (276,280) being fixed in the supporting members (268,270) in the inner seat frame (222), said inner armrest supports (276,280) extending from the inner seat frame (222) into respective outer seat frame supporting members (264,266,272,274); said inner armrest supports (276,280) being in relative slidable and supported engagement in said outer seat supporting members (264,266,272,274); said inner armrest supports (276,280) between the seat frame having openings to receive pins (290) attached to the inner armrests (26) and to secure the inner armrests (26) positioned between the seat frames (220-224). The passenger seat combination (12,14;16) according to claim 5 in which: said inner armrest (26) and pins (290) are removable from said inner armrest supports (276,280) to permit the three seat frame combination (16A) to be changed to a two seat frame combination (16B); said supporting members (264,266,272,274) of said outside seat frames (220,224) sliding on said inner armrest supports (276,280) when said outer seat frames (220,224) are moved inwardly to form the two seat frame combination (16B); said outer seat frames (220,224) being closely adjacent said inner seat frame (222) in the two seat combination (16B). The passenger seat combination (12,14;16) according to claim 6 in which: an inner seat armrest (30) is formed as a part (32A) of a back of the inner seat frame (222); said inner seat frame armrest (30) being centered in said back (32A) and hinged so as to be foldable downwardly to form a center armrest (30) for the two seat frames (220,224) in the two seat combination (16B). The passenger seat combination (12,14;16) according to any one of the claims 4-7 in which: outer armrests (42,44) are secured to supports (310) on outer ends of the outer seat frames (220,224) said outer armrests (42,44) having upper caps (306) upon which a passenger's arm may be positioned; said caps (306) being removable: generally horizontal hinged plates (308) on said supports (310) on said outer ends forming flat supports for inner upper surfaces of said caps (308); said plates (308) being hingedly movable from outer flat positions to inner flat positions relative to said seat frames (220,224); whereby when a three seat frame combination (16A) is changed to a two seat frame combination (16B) the plates (308) may be moved inwardly to receive the caps (306) thereon to increase aisle space (18B,20B) outwardly of the outer seat frames (220,224).

Inventors: SLETTEBAK, RICHARD JOHN
Applicants: THE BOEING COMPANY
Application year: 1988
Main classification: B64D11
IPC codes: B64D11