CN214402961U - Aircraft storehouse and aircraft external member - Google Patents
Aircraft storehouse and aircraft external member Download PDFInfo
- Publication number
- CN214402961U CN214402961U CN202120349684.1U CN202120349684U CN214402961U CN 214402961 U CN214402961 U CN 214402961U CN 202120349684 U CN202120349684 U CN 202120349684U CN 214402961 U CN214402961 U CN 214402961U
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- aircraft
- roll
- clamping
- over stand
- garage
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Abstract
The utility model provides an aircraft storehouse and aircraft external member relates to aircraft technical field, the utility model provides an aircraft storehouse, include: the device comprises a clamping assembly, a turnover frame and a storage box; the clamping assembly is arranged on the turnover frame and used for clamping the aircraft; the roll-over stand rotates to be connected in the storage box, and the pivot of roll-over stand extends along the horizontal direction. The utility model provides an aircraft storehouse can the fixed aircraft of centre gripping, and can overturn the aircraft and accomodate.
Description
Technical Field
The utility model belongs to the technical field of the aircraft technique and specifically relates to an aircraft storehouse and aircraft external member are related to.
Background
The projected area of the aircraft in the direction of the plumb is large, so that the floor area of the aircraft garage on a horizontal plane is generally large. Due to the small height dimensions of the aircraft. Although area can be reduced through the upset aircraft when accomodating the aircraft, the aircraft of turning on one's side is difficult to fix, has the risk that produces the bruise.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aircraft storehouse and aircraft external member can the fixed aircraft of centre gripping, and can overturn the aircraft and accomodate.
In a first aspect, the present invention provides an aircraft garage, including: the device comprises a clamping assembly, a turnover frame and a storage box;
the clamping assembly is arranged on the turnover frame and is used for clamping the aircraft;
the roll-over stand rotate connect in the storage box, just the pivot of roll-over stand extends along the horizontal direction.
With reference to the first aspect, the present disclosure provides a first possible implementation manner of the first aspect, wherein the roll-over stand has two stations;
at a first station, the turnover frame is turned to be in a vertical state and drives the aircraft to enter an inner cavity of the storage box;
and at the second station, the turnover frame is turned to be in a horizontal state.
With reference to the first possible implementation manner of the first aspect, the present invention provides a second possible implementation manner of the first aspect, wherein the flip frame is in the horizontal state, and the bearing surface of the clamping assembly is higher than the top surface of the storage box.
In combination with the first aspect, the present invention provides a third possible implementation manner of the first aspect, wherein the roll-over stand comprises: a support rod, an inclined rod and a bearing piece;
the clamping assembly is arranged on the bearing piece, and the support rod is perpendicular to the bearing surface of the clamping assembly;
one end of the diagonal rod is mounted on the storage box through the rotating shaft, and the other end of the diagonal rod is connected with the bearing piece;
when the roll-over stand overturns to the horizontal state, the down tube inclines upwards from the end connected with the support rod to the end connected with the bearing piece.
In combination with the first aspect, the present invention provides a fourth possible implementation manner of the first aspect, wherein the aircraft garage further includes a turnover driving assembly, and the turnover driving assembly is connected to the roll-over stand in a transmission manner.
In combination with the first aspect, the present invention provides a fifth possible implementation manner of the first aspect, wherein the clamping assembly includes: the clamping driving piece is arranged on the tray;
the clamping pieces are respectively connected to the tray in a sliding manner and are respectively in transmission connection with the clamping driving piece;
and a clamping area is formed by enclosing the clamping pieces.
With reference to the fifth possible implementation manner of the first aspect, the present invention provides a sixth possible implementation manner of the first aspect, wherein the clamping driving member includes: the driving ring, the gear ring and the rotary driving piece;
the gear ring is connected with the driving ring, and the rotary driving piece is in transmission connection with the gear ring;
the driving ring is provided with a sliding groove, the clamping piece is connected with a sliding column, and the sliding column is connected in the sliding groove in a sliding mode.
With reference to the sixth possible implementation manner of the first aspect, the present invention provides a seventh possible implementation manner of the first aspect, wherein the clip is provided with a first plane and a second plane;
any one of the clamping pieces is connected between the two clamping pieces in a sliding manner, and the first plane of any one of the clamping pieces slides along the second plane of the other clamping piece.
With reference to the seventh possible implementation manner of the first aspect, the present invention provides an eighth possible implementation manner of the first aspect, wherein the tray is provided with a plurality of guiding surfaces, and the plurality of guiding surfaces correspond to the plurality of clamping pieces one to one;
any one of the clips is slidably connected between the second plane of the other clip and the guide surface.
In a second aspect, the present invention provides an aircraft kit, comprising: aircraft and the aircraft storehouse that the first aspect provided, the bottom of aircraft is installed with the by the holder that the centre gripping subassembly is fit for.
The embodiment of the utility model provides a following beneficial effect has been brought: adopt centre gripping subassembly to install on the roll-over stand, through centre gripping subassembly centre gripping aircraft, the roll-over stand rotates to be connected in the storage box, and the pivot of roll-over stand extends along the horizontal direction, revolves the rotation of axes through the roll-over stand to can make the aircraft overturn between horizontality and vertical state.
In order to make the aforementioned and other objects, features and advantages of the present invention comprehensible, preferred embodiments accompanied with figures are described in detail below.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention or the related art, the drawings required to be used in the description of the embodiments or the related art will be briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic view of an aircraft garage and aircraft provided by an embodiment of the present invention;
fig. 2 is a schematic view of a roll-over stand of an aircraft garage provided by an embodiment of the present invention;
fig. 3 is a schematic view of a clamping assembly of an aircraft garage provided in an embodiment of the present invention;
fig. 4 is a schematic view of an aircraft kit provided in an embodiment of the present invention.
Icon: 100-a clamping assembly; 101-a bearing surface; 110-a tray; 111-a guide surface; 120-a clamp drive; 121-a drive coil; 1211-chute; 122-ring gear; 123-a rotary drive; 130-a clip; 131-a strut; 132-a first plane; 133-a second plane; 140-a clamping zone; 200-a roll-over stand; 201-a rotating shaft; 210-a strut; 220-diagonal rod; 230-a carrier; 300-a storage box; 301-top surface; 400-an aircraft; 410-clamped piece.
Detailed Description
The technical solution of the present invention will be described clearly and completely with reference to the accompanying drawings, and obviously, the described embodiments are some, but not all embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. The term "physical quantity" in the formula, unless otherwise noted, is understood to mean a basic quantity of a basic unit of international system of units, or a derived quantity derived from a basic quantity by a mathematical operation such as multiplication, division, differentiation, or integration.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Example one
As shown in fig. 1 and 4, an embodiment of the present invention provides an aircraft garage, including: a clamping assembly 100, a roll-over stand 200 and a storage box 300; the clamping assembly 100 is installed on the roll-over stand 200, and the clamping assembly 100 is used for clamping the aircraft 400; the roll-over stand 200 is rotatably connected to the storage box 300, and the rotating shaft 201 of the roll-over stand 200 extends in a horizontal direction.
Specifically, the clamping assembly 100 can clamp the clamped piece 410 at the bottom of the aircraft 400, so that a support frame does not need to be arranged at the bottom of the aircraft 400, and the height dimension of the aircraft 400 is reduced. Under the state that the aircraft 400 is clamped and fixed by the clamping assembly 100, the overturning frame 200 drives the aircraft 400 to overturn around the rotating shaft 201, so that the aircraft 400 can be overturned to a side overturning state, and the occupied area of an aircraft warehouse can be reduced.
In the embodiment of the present invention, the roll-over stand 200 has two stations;
at the first station, the roll-over stand 200 is turned over to be vertical and drives the aircraft 400 to enter the inner cavity of the storage box 300;
at the second station, the roll-over stand 200 is turned over to a horizontal position.
Specifically, the roll-over stand 200 may be manually powered to roll over and locked when the roll-over stand 200 is in a horizontal position so that the aircraft can be vertically lifted from the holding assembly 100. In addition, a mechanical transmission can be used to drive the roll-over stand 200 to roll over around the axis of the rotating shaft 201, so that the roll-over stand 200 can be switched back and forth between the first station and the second station.
Further, the loading surface 101 of the clamping assembly 100 is higher than the top surface 301 of the bin 300 when the roll-over stand 200 is in the horizontal state.
When aircraft 400 is landed on clamp assembly 100 and is supported by clamp 410 by clamp assembly 100, the rotor of aircraft 400 is positioned above load-bearing surface 101. In addition, in the landing process of the aircraft 400, the arm support position of the aircraft 400 is higher than the top surface 301 of the storage box 300, so that the aircraft 400 can be prevented from colliding with the storage box 300 in the landing process. In addition, the positions of the electronic devices in the aircraft 400 are always higher than the storage box 300, so that the storage box 300 can be prevented from interfering with the electric signals, and the positioning signals of the aircraft 400 are further ensured to be stable.
As shown in fig. 1 and 2, the roll-over stand 200 includes: strut 210, diagonal rod 220, and bearing 230;
the clamping assembly 100 is mounted on the bearing member 230, and the supporting rod 210 is perpendicular to the bearing surface 101 of the clamping assembly 100;
one end of the diagonal rod 220 is mounted to the storage box 300 through the rotating shaft 201, and the other end of the diagonal rod 220 is connected to the bearing member 230;
when the roll-over stand 200 is rolled over to the horizontal position, the diagonal bar 220 is inclined upward from the end of the connecting strut 210 to the end of the connecting carrier 230.
In the horizontal state of the roll-over stand 200, the supporting rod 210 extends along the plumb direction, the bearing piece 230 extends along the horizontal direction, and the clamping assembly 100 is supported by the bearing piece 230; in the vertical state of the roll-over stand 200, the pole 210 extends in the horizontal direction toward the inside of the storage box 300, and the carrier 230 extends in the plumb direction, so that the clip assembly 100 and the aircraft 400 can be rolled over to a roll-over state.
Further, the aircraft garage further comprises a turnover driving assembly, and the turnover driving assembly is in transmission connection with the turnover frame 200.
In one embodiment, the flipping driving assembly comprises a motor, which drives the rotating shaft 201 to rotate through a gear transmission, so as to drive the flipping frame 200 and the clamping assembly 100 to synchronously rotate around the axis of the rotating shaft 201.
In another embodiment, the turnover driving assembly comprises a telescopic driving cylinder, one end of the telescopic driving cylinder is hinged with the storage box 300, the other end of the telescopic driving cylinder is hinged with the turnover frame 200, and the turnover frame 200 can be driven to rotate around the axis of the rotating shaft 201 by the telescopic driving cylinder.
As shown in fig. 1, 3 and 4, the clamping assembly 100 includes: a tray 110, a grip driving member 120, and a plurality of clips 130; the plurality of clamping pieces 130 are respectively connected to the tray 110 in a sliding manner, and the plurality of clamping pieces 130 are respectively connected with the clamping driving member 120 in a transmission manner; a clamping area 140 is defined between the plurality of clips 130.
Specifically, the clamped member 410 at the bottom of the aircraft 400 can be inserted into the clamping area 140, and the plurality of clips 130 are driven by the clamping driving member 120 to respectively slide relative to the tray 110, so that the opening degree of the clamping area 140 can be adjusted. When the opening degree of the clamping area 140 is increased and the roll-over stand 200 and the clamping assembly 100 are horizontally mounted, the aircraft 400 can take off and land vertically; when the aircraft is lowered onto clamping assembly 100, clamping actuator 120 actuates plurality of jaws 130, thereby causing clamping area 140 to contract and clamp clamped element 410.
Further, the clamp drive 120 includes: a drive ring 121, a ring gear 122, and a rotary driver 123; the gear ring 122 is connected with the driving ring 121, and the rotary driving piece 123 is in transmission connection with the gear ring 122; the driving ring 121 is provided with a sliding slot 1211, the clip 130 is connected with a sliding column 131, and the sliding column 131 is slidably connected in the sliding slot 1211.
Specifically, the rotary driving member 123 includes a driving gear and a servo motor, the servo motor is in transmission connection with the driving gear, the driving gear is driven to rotate by the servo motor, and the driving gear is meshed with the gear ring 122 and is driven, so that the driving ring 121 is driven to rotate around the axis of the driving ring. The extending direction of the sliding slot 1211 forms an acute angle with the radial direction of the driving ring 121, and the sliding column 131 slides along the sliding slot 1211 during the rotation of the driving ring 121, so that the clamping pieces 130 move along the sliding slot 1211, thereby adjusting the opening degree of the clamping area between the plurality of clamping pieces 130.
Further, the clip 130 is provided with a first plane 132 and a second plane 133;
either clip 130 is slidably connected between the two clips 130 and the first planar surface 132 of either clip 130 slides along the second planar surface 133 of the other clip 130.
Specifically, during the sliding of the sliding post 131 along the sliding slot 1211, the first plane 132 of any one of the clamping pieces 130 slides along the second plane 133 of the other clamping piece 130, thereby ensuring the smooth sliding of the plurality of clamping pieces 130.
Further, the tray 110 is provided with a plurality of guide surfaces 111, and the plurality of guide surfaces 111 correspond to the plurality of clamping pieces 130 one to one; either jaw 130 is slidably coupled between the second plane 133 of the other jaw 130 and the guide surface 111, thereby ensuring that the jaw 130 can smoothly slide between the second plane 133 and the guide surface 111.
Example two
As shown in fig. 1, an embodiment of the present invention provides an aircraft kit, including: aircraft 400 and the first embodiment provide an aircraft garage, and a clamped piece 410 matched with clamping assembly 100 is installed at the bottom of aircraft 400.
The embodiment of the utility model provides an in, the aircraft external member possesses the technological effect in aircraft storehouse, can reduce aircraft 400's height dimension, and when aircraft 400 was fixed by the centre gripping of centre gripping subassembly 100 centre gripping, roll-over stand 200 drove aircraft 400 and revolutes 201 upset of axle, can overturn aircraft 400 to the state of turning on one's side, has reduced the area in aircraft 400 storehouse.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention.
Claims (10)
1. An aircraft garage, comprising: the device comprises a clamping assembly (100), a turnover frame (200) and a storage box (300);
the clamping assembly (100) is installed on the overturning frame (200), and the clamping assembly (100) is used for clamping an aircraft (400);
the roll-over stand (200) is rotatably connected to the storage box (300), and a rotating shaft (201) of the roll-over stand (200) extends along the horizontal direction.
2. The aircraft garage of claim 1, wherein the roll-over stand (200) has two stations;
at a first station, the overturning frame (200) is overturned to be in a vertical state and drives the aircraft (400) to enter an inner cavity of the storage box (300);
at a second station, the roll-over stand (200) is turned over to a horizontal state.
3. The aircraft garage of claim 2, wherein the loading surface (101) of the gripping assemblies (100) is higher than the top surface (301) of the storage bin (300) in the horizontal position of the roll-over stand (200).
4. The aircraft garage of claim 1, wherein the roll-over stand (200) comprises: a strut (210), a diagonal (220), and a carrier (230);
the clamping assembly (100) is mounted on the bearing piece (230), and the supporting rod (210) is perpendicular to the bearing surface (101) of the clamping assembly (100);
one end of the diagonal rod (220) is mounted on the storage box (300) through the rotating shaft (201), and the other end of the diagonal rod (220) is connected with the bearing piece (230);
when the roll-over stand (200) is turned over to be in a horizontal state, the inclined rod (220) is inclined upwards from one end connected with the supporting rod (210) to one end connected with the bearing piece (230).
5. The aircraft garage of claim 1, further comprising a roll-over drive assembly in driving connection with the roll-over stand (200).
6. The aircraft garage of claim 1, wherein the clamping assembly (100) comprises: a tray (110), a gripping drive (120), and a plurality of clips (130);
the clamping pieces (130) are respectively connected to the tray (110) in a sliding manner, and the clamping pieces (130) are respectively connected with the clamping driving piece (120) in a transmission manner;
a clamping area (140) is formed by enclosing among the clamping pieces (130).
7. The aircraft garage of claim 6, wherein the clamp drive (120) comprises: a drive ring (121), a ring gear (122) and a rotary drive (123);
the gear ring (122) is connected with the driving ring (121), and the rotary driving piece (123) is in transmission connection with the gear ring (122);
the driving ring (121) is provided with a sliding groove (1211), the clamping piece (130) is connected with a sliding column (131), and the sliding column (131) is connected in the sliding groove (1211) in a sliding mode.
8. The aircraft garage of claim 7, wherein the clip (130) is provided with a first plane (132) and a second plane (133);
any one of the clips (130) is slidably connected between two of the clips (130), and the first plane (132) of any one of the clips (130) slides along the second plane (133) of the other clip (130).
9. The aircraft garage of claim 8, wherein the tray (110) is provided with a plurality of guide surfaces (111), the plurality of guide surfaces (111) corresponding one-to-one to the plurality of clips (130);
any one of the clips (130) is slidably connected between the second plane (133) of the other clip (130) and the guide surface (111).
10. An aircraft kit, comprising: aircraft (400) and aircraft garage according to any one of claims 1 to 9, the bottom of the aircraft (400) being fitted with a gripped piece (410) adapted to the gripping assembly (100).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120349684.1U CN214402961U (en) | 2021-02-07 | 2021-02-07 | Aircraft storehouse and aircraft external member |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120349684.1U CN214402961U (en) | 2021-02-07 | 2021-02-07 | Aircraft storehouse and aircraft external member |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214402961U true CN214402961U (en) | 2021-10-15 |
Family
ID=78024643
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120349684.1U Active CN214402961U (en) | 2021-02-07 | 2021-02-07 | Aircraft storehouse and aircraft external member |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214402961U (en) |
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2021
- 2021-02-07 CN CN202120349684.1U patent/CN214402961U/en active Active
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