CN209617515U

CN209617515U - A kind of aircraft bottom plate and the aircraft seat with the aircraft bottom plate

Info

Publication number: CN209617515U
Application number: CN201822223602.XU
Authority: CN
Inventors: 许良
Original assignee: Shenzhen Fuxiang Aviation Technology Co Ltd
Current assignee: Shenzhen Fuxiang Aviation Technology Co Ltd
Priority date: 2018-12-28
Filing date: 2018-12-28
Publication date: 2019-11-12
Anticipated expiration: 2028-12-28

Abstract

A kind of aircraft bottom plate and the aircraft seat with the aircraft bottom plate, the aircraft seat includes an aircraft bottom plate and a seat, engine room inside of the aircraft bottom plate to be set to an aircraft, specifically, the aircraft bottom plate has one first inclined-plane, it is incorporated on first inclined-plane for the seat, and the seat is moved between a first position and a second position along first inclined-plane, and all have displacement in the horizontal direction and the vertical direction when seat movement.By above-mentioned design, user can adjust the seat to ride comfort according to the body type of oneself or be suitble to operate the position of aircraft, preferably take experience to reach.

Description

A kind of aircraft bottom plate and the aircraft seat with the aircraft bottom plate

Technical field

The utility model is related with aircraft seat structure；It particularly relates to a kind of for the aircraft bottom plate and tool of seat to be arranged There is the aircraft seat of the aircraft bottom plate.

Background technique

On existing light aerocraft, the seat in cabin is adopted affixed mode mostly and is set on aircraft, however each The height of aircraft occupant, figure are different, if aircraft occupant can not adjust seat to the position for meeting oneself body type, be easy because One is in for a long time for body to restrain uncomfortable posture and feel tired, uncomfortable；If aircraft occupant is driver, have Probably due to seat can not be adjusted to suitable position, and that causes that the visual field is bad, operation is not easy etc. and be unfavorable for driving an airplane asks Topic, if being bound to a small space for a long time, is held for example, the air vehicle operator that body type is taller and bigger, needs biggish seating space Muscular fatigue is easily led to, is unfavorable for flight operation, and the air vehicle operator that body type is shorter and smaller, then it is too low to tend to have seat position, leads The problem for causing the operation visual field bad.

Therefore, a kind of aircraft bottom plate conducive to adjustment seat position is developed, seat is enabled to be suitble to the people of different body types Member, which takes, its necessity.

Summary of the invention

In view of this, the utility model is designed to provide a kind of aircraft bottom plate, can according to the demand of different users, Adjustment seat feels position appropriate to user.

Edge is to reach above-mentioned purpose, a kind of aircraft bottom plate provided by the utility model, to be set to the cabin of an aircraft Inside, for combining a seat on the aircraft bottom plate, it is characterised in that: the aircraft bottom plate has one first inclined-plane, which combines In on first inclined-plane, and the seat can move between a first position and a second position along first inclined-plane, and in The seat all has displacement when mobile in the horizontal direction and the vertical direction.

Wherein, which has a connecting piece, which is incorporated on first inclined-plane by the connecting piece.

Wherein, which has one first plate and one second plate that are connected, which has this first tiltedly Face；Second plate is connect with a lateral margin of first plate, and the angle between second plate and first plate is in 90 to 160 degree Between.

Wherein, the structure that first plate and second plate are one of the forming.

Wherein, on first plate of the aircraft bottom plate and a second hardened cabin floor together in the aircraft, and this One plate, second plate and the cabin floor surround and form an accommodating space.

Wherein, the intersection of first plate and second plate is equipped with one first opening.

Wherein, which is equipped with one second opening.

Wherein, the intersection of first plate and second plate is equipped with one first opening, the first open communication accommodating sky Between；Second plate is equipped with one second opening, second open communication accommodating space.

Wherein, which is greater than first opening.

Wherein, the width of second plate is tapered toward the direction away from first plate.

The utility model separately provides a kind of aircraft seat, includes above-mentioned aircraft bottom plate and a seat, the wherein seat It is incorporated on first inclined-plane, which can move between a first position and a second position along first inclined-plane, and The seat all has displacement when mobile in the horizontal direction and the vertical direction.

The effect of the utility model is that the seat moves between a first position and a second position along first inclined-plane When dynamic, which all has displacement simultaneously in the horizontal direction and the vertical direction, and user can adjust according to the body type of oneself should Seat is to ride comfort or is suitble to operate the position of aircraft, preferably takes experience to reach.

Detailed description of the invention

Fig. 1 is the schematic diagram of the aircraft seat of the preferred embodiment in the utility model；

Fig. 2A is the side view of the aircraft seat of above preferred embodiment；

Fig. 2 B is the side view of the aircraft seat of above preferred embodiment；

Fig. 3 is the schematic diagram of the aircraft seat of above preferred embodiment.

Description of symbols

[the utility model]

100 aircraft seats

10 aircraft bottom plate, 12 first plate, 122 first inclined-plane

124 connector, 14 second plate, 142 second inclined-plane

16 first opening, 18 second opening 18a upper cover

20 seats

200 engine room insides

202 driver's seat, 204 passenger seat, 206 cabin floor

208 accommodating space, 210 control stick

θ angle

X horizontal direction

Y vertical direction

Specific embodiment

For that can be illustrated more clearly that the utility model, hereby lifts with next preferred embodiment and attached drawing is cooperated to be described in detail such as Afterwards.It please join shown in Fig. 1 to Fig. 3, be the aircraft seat 100 of the preferred embodiment of the utility model.

The aircraft seat 100 includes aircraft bottom plate 10 and seat 20, machine of the aircraft bottom plate 10 to be set to aircraft 200 inside cabin, the aircraft is light aerocraft in this present embodiment, and the aircraft bottom plate 10 may be disposed inside the aircraft cabin 200 driver's seat 202 and the position of passenger seat 204, in other embodiments, which can be other kinds of aircraft, should Aircraft bottom plate 10 may be disposed at the position that inside aircraft cabin 200 other staff take, without being limited with above-mentioned.

The aircraft bottom plate 10 has the first plate 12 and the second plate 14 being connected, which has the first inclined-plane 122, Second plate 14 has the second inclined-plane 142, which connect with one of first inclined-plane 122 lateral margin；The seat 20 Be incorporated on first inclined-plane 122, and the angle theta of first plate 12 and second plate 14 90 to 160 degree between, preferably Between 140 degree to 160 degree, the selection of this angle can have both the convenience that user adjusts height before and after seat, and in accident Accident occur when or when aircraft abrupt deceleration, can effectively reduce or buffer user toward advancing slip punching active force.Therefore when use When person is ridden on the seat 20, foot can be placed on second inclined-plane 142, which can provide a support force In user leg, it is more comfortable when taking to make user, and the angle theta is 150 degree in this present embodiment, in addition, Yu Benshi The structure that the first plate of this in example 12 and second plate 14 are one of the forming is applied, has many advantages, such as to be not easy to separate mutually, stabilized structure.

Wherein, which is equipped with a connecting piece 124, the seat 20 by the connecting piece 124 be incorporated into this On one inclined-plane 122, in this present embodiment, which is a rail structure, which is incorporated into the rail structure, and Moved by the rail structure on first inclined-plane 122, the rail structure can be set in reversible manner this first tiltedly On face 122, design which can also be one of the forming with first plate 12.

The seat 20 can move between first position and the second position along first inclined-plane 122, and the seat 20 moves All there is displacement on X and vertical direction Y in the horizontal direction when dynamic, as shown in Figure 2 A and 2 B, when the seat 20 is by Fig. 2A institute When the first position shown is moved to the second position shown in Fig. 2 B, which all generates on X and vertical direction Y in the horizontal direction Have a positive-displacement, and vice versa, therefore when the body type of user is shorter and smaller, can adjust the seat 20 in the horizontal direction X with Have the direction of a positive-displacement mobile simultaneously on vertical direction Y, improvement cause the operation visual field bad because height is shorter and smaller or It is and the user that body type is taller and bigger because too far from operation instrument lead to inconvenient problem, then can adjust the seat 20 The direction for having a negative sense to be displaced simultaneously on X and vertical direction Y in the horizontal direction is mobile, allows a user in limited aircraft Engine room inside 200 adjusts out a biggish seating space and is adjusted simultaneously to a flight visual field appropriate.And because seat 20 are incorporated on first inclined-plane 122, therefore while accident impact occurs for aircraft, which can provide an anti-work Firmly, prevent user to advancing slip punching.

First plate 12 and second plate 14 respectively in connection with inside aircraft cabin on 200 cabin floor 206, and this One plate 12, second plate 14 and the cabin floor 206 around an accommodating space 208 is formed, wherein first plate 12 and this The intersection of two plates 14 is equipped with one first opening 16, which is connected to the accommodating space 208, which is equipped with one Second opening 18, second opening 18 are connected to the accommodating space 208, which is greater than first opening 16, this first Opening 16 and the accommodating space 208 are to be arranged control stick 210, and the control stick 210 is to manipulate the aircraft, second opening 18 Equipped with a upper cover 18a to close the accommodating space 208, this second opening 18 and the accommodating space 208 to place article or The relevant apparatus of aircraft is set, and first opening 16 passes to the accommodating space with second opening 18 in succession in this present embodiment 208, in other embodiments, first opening 16 and second opening 18 can be respectively communicated to individual independent not interconnect Accommodating space.In addition, the width of second plate 14 is tapered toward the direction away from first plate 12, the tapered design of plate face is not only The setting that 200 spaces are tapered inside aircraft cabin is complied in the design for meeting human body figure, also can avoid in waste aircraft cabin 200 space of portion, or increase the weight bearing of aircraft.

It according to the above, should when which moves between a first position and a second position along first inclined-plane 122 Seat 20 all has displacement on X and vertical direction Y in the horizontal direction simultaneously, and user can adjust the chair according to the body type of oneself Seat is to ride comfort or is suitble to operate the position of aircraft, preferably takes experience to reach.

The foregoing is merely the preferred possible embodiments of the utility model, apply the utility model specification and Shen such as Please the scope of the patents institute equivalence changes for it, ought to be included in the scope of the patents of the utility model.

Claims

It is special for combining a seat on the aircraft bottom plate to be set to the engine room inside of an aircraft 1. a kind of aircraft bottom plate Sign is that the aircraft bottom plate has one first inclined-plane, and the seat is incorporated on first inclined-plane, and the seat being capable of edge First inclined-plane moves between a first position and a second position, and when the seat is mobile in the horizontal direction with hang down Histogram all has displacement upwards.
2. aircraft bottom plate according to claim 1, characterized in that first inclined-plane has a connecting piece, the seat It is incorporated on first inclined-plane by the connecting piece.
3. aircraft bottom plate according to claim 1, characterized in that the aircraft bottom plate have one first plate that is connected with And one second plate, first plate have first inclined-plane；Second plate is connect with a lateral margin of first plate, and institute The angle between the second plate and first plate is stated between 90 to 160 degree.
4. aircraft bottom plate according to claim 3, characterized in that first plate was one of the forming with second plate Structure.
5. aircraft bottom plate according to claim 3, characterized in that first plate and described second of the aircraft bottom plate On a hardened cabin floor together in the aircraft, and first plate, second plate and the cabin floor surround shape At an accommodating space.
6. aircraft bottom plate according to claim 3, characterized in that the intersection of first plate and second plate is equipped with One first opening.
7. aircraft bottom plate according to claim 3, characterized in that second plate is equipped with one second opening.
8. aircraft bottom plate according to claim 5, characterized in that the intersection of first plate and second plate is equipped with One first is open, accommodating space described in first open communication；Second plate is equipped with one second opening, second opening It is connected to the accommodating space.
9. aircraft bottom plate according to claim 8, characterized in that second opening is greater than first opening.
10. aircraft bottom plate according to claim 3, characterized in that the width of second plate is toward away from first plate Direction it is tapered.
11. a kind of aircraft seat, characterized in that include:

One aircraft bottom plate according to any one of claim 1 to 10；And

One seat, the seat are incorporated on first inclined-plane, and the seat can be along first inclined-plane in one first It sets and is moved between a second position, and all have displacement in the horizontal direction and the vertical direction when seat movement.