CN110963062A - Nacelle quick detach device and contain its aircraft - Google Patents
Nacelle quick detach device and contain its aircraft Download PDFInfo
- Publication number
- CN110963062A CN110963062A CN201811141656.XA CN201811141656A CN110963062A CN 110963062 A CN110963062 A CN 110963062A CN 201811141656 A CN201811141656 A CN 201811141656A CN 110963062 A CN110963062 A CN 110963062A
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- CN
- China
- Prior art keywords
- positioning groove
- elastic
- release device
- nacelle
- installation frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 238000009434 installation Methods 0.000 claims abstract description 19
- 238000003780 insertion Methods 0.000 claims description 8
- 230000037431 insertion Effects 0.000 claims description 8
- 229920001971 elastomer Polymers 0.000 description 10
- 239000000806 elastomer Substances 0.000 description 10
- 230000000694 effects Effects 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000006073 displacement reaction Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000005693 optoelectronics Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
Abstract
The invention discloses a nacelle quick-release device and an aircraft comprising the same, wherein the nacelle quick-release device comprises an installation frame, a buckling piece and at least one elastic part, the buckling piece can rotate relative to the installation frame so as to be detachably connected to the installation frame, one side, facing the installation frame, of the buckling piece is provided with at least one positioning groove, the elastic parts correspond to the positioning grooves one by one, one end of each elastic part is connected to the installation frame, and the other end of each elastic part is detachably connected to the corresponding positioning groove. The aircraft comprises a nacelle quick release device as described above. According to the invention, the clamping piece is rotated, so that the clamping piece and the mounting frame are assembled and disassembled quickly and conveniently, and the working efficiency of the nacelle quick-disassembling device is greatly improved. Meanwhile, the elastic part prevents the buckling part from moving along the circumferential direction, and the safety and stability of the nacelle quick-release device are greatly improved.
Description
Technical Field
The invention relates to a nacelle quick-release device and an aircraft comprising the same.
Background
The fuselage of aircraft is hung with photoelectric equipment such as visible light camera, infrared camera for work such as aerial photography, aim, monitoring or pursuit, according to the difference of work content, has to carry out debugging or change to the photoelectric equipment of fuselage mounting, that just means need repeatedly dismantle and assemble between fuselage and the photoelectric equipment. At present, the aircraft is mainly connected fuselage and optoelectronic device through a plurality of screws, need lock repeatedly or unscrew the screw, and the operation is inconvenient and the cost is long, and work efficiency is low.
Disclosure of Invention
The invention aims to overcome the defects of inconvenient operation, long time consumption, low working efficiency and the like in the prior art, and provides a nacelle quick-release device and an aircraft comprising the same.
The invention solves the technical problems through the following technical scheme:
the nacelle quick-release device is characterized by comprising an installation frame, a buckling piece and at least one elastic component, wherein the buckling piece is rotatable relative to the installation frame so that the buckling piece is detachably connected to the installation frame, at least one positioning groove is formed in one side, facing the installation frame, of the buckling piece, the elastic component corresponds to the positioning groove in a one-to-one mode, one end of the elastic component is connected to the installation frame, and the other end of the elastic component is detachably connected to the inside of the positioning groove.
In this scheme, adopt above-mentioned structural style, through the rotation of buckle spare for loading and unloading between buckle spare and the mounting bracket, simultaneously, prevent through elastomeric element that buckle spare from removing along the circumferencial direction, the installation is dismantled fast and conveniently, has improved nacelle quick detach device's work efficiency and safety and stability greatly.
Preferably, the fastening piece is provided with at least one clamping block, the clamping block extends and protrudes along the radial direction of the fastening piece, the mounting frame is provided with at least one notch, the notch extends and is arranged along the rotating direction of the fastening piece, the clamping block corresponds to the notch one by one, the clamping block is clamped in the notch, and the clamping block can move in the notch.
In this scheme, adopt above-mentioned structural style, realize rotatory dismouting through the cooperation between fixture block and the breach, simple structure, processing preparation is convenient.
Preferably, the both ends of breach have respectively to lean on portion and entry portion, the upper end of entry portion is the slope form.
In this scheme, adopt above-mentioned structural style, the upper end through entering the portion is the slope form, plays the guide effect, and the fixture block of being convenient for inserts to the breach in, realizes being connected of buckle spare and mounting bracket.
Preferably, the fixture block abuts against the abutting portion, so that the elastic member is inserted into the positioning groove.
In this scheme, adopt above-mentioned structural style for buckle spare buckle when being fixed in the mounting bracket and match with elastomeric element's location, structural connection intensity is high, has improved nacelle quick detach device's stability.
Preferably, the end of the fixture block has an insertion end, and the lower end of the insertion end is inclined.
In this scheme, adopt above-mentioned structural style, the lower extreme through inserting the end is the slope form, plays the guide effect, and the fixture block of being convenient for inserts to the breach in.
Preferably, the elastic component includes connecting piece, elastomer and reference column, the connecting piece connect in the mounting bracket, the bottom of connecting piece is equipped with the opening, have in the connecting piece and hold the chamber, the opening with it is linked together to hold the chamber, the elastomer is located hold the intracavity, just the one end of elastomer support lean on in the connecting piece, the other end of elastomer support lean on in the reference column, the reference column passes the opening and insert to in the positioning groove.
In this scheme, adopt above-mentioned structural style, make the reference column displacement of can floating through the elastomer for the reference column will float the displacement and break away from out positioning groove, realize the dismantlement between buckle spare and the mounting bracket. Meanwhile, the elastic component is simple in structure and convenient to manufacture.
Preferably, the mounting frame is provided with at least one connecting hole, the connecting hole extends along a direction close to the positioning groove, the connecting hole is in one-to-one correspondence with the elastic part, and the connecting piece is in threaded connection with the inside of the connecting hole.
In this scheme, adopt above-mentioned structural style, through threaded connection between connecting piece and the connecting hole for rotatory connecting piece can realize the regulation of position to elastomeric element, thereby can adjust the cooperation effort between elastomeric element and the buckle spare, has improved nacelle quick detach device's stability.
Preferably, one side of the fastening piece facing the mounting frame is provided with at least one guide groove, the guide groove extends along the rotation direction of the fastening piece, the guide grooves correspond to the elastic parts one to one, and the elastic parts are inserted into the guide grooves and move in the guide grooves.
In this scheme, adopt above-mentioned structural style, the guide way plays the guide effect for elastomeric element can remove along established orbit in the guide way, realizes that elastomeric element can insert to positioning groove accurately in, has effectively avoided elastomeric element to produce the skew dislocation phenomenon at the in-process that uses, has improved nacelle quick detach device's reliable and stable nature.
Preferably, the mounting frame comprises a frame body and a snap ring, the frame body is provided with a mounting hole, the snap ring is connected in the mounting hole, the snap member is inserted into the mounting hole and detachably connected to the snap ring, and the elastic member is connected to the frame body.
In this scheme, adopt above-mentioned structural style, insert to the mounting hole through the snap ring for buckle spare is convenient for be connected with the location of snap ring, and it is more convenient to connect. Meanwhile, the mounting frame is simple in structure and convenient to manufacture and assemble.
An aircraft characterized in that it comprises a nacelle de-taching device as described above.
In this scheme, adopt above-mentioned structural style, through the rotation of buckle spare for loading and unloading between buckle spare and the mounting bracket, the installation is dismantled fast and conveniently, has improved the dismouting efficiency of aircraft greatly. Simultaneously, prevent through elastomeric element that buckle spare from moving along the circumferencial direction, improved the safety and stability nature of aircraft greatly.
On the basis of the common knowledge in the field, the above preferred conditions can be combined randomly to obtain the preferred embodiments of the invention.
The positive progress effects of the invention are as follows:
according to the nacelle quick-release device and the aircraft comprising the same, the clamping piece and the mounting frame are assembled and disassembled quickly and conveniently by rotating the clamping piece, and the working efficiency of the nacelle quick-release device is greatly improved. Meanwhile, the elastic part prevents the buckling part from moving along the circumferential direction, and the safety and stability of the nacelle quick-release device are greatly improved.
Drawings
Fig. 1 is a schematic view of a state of use of a nacelle quick release device of an aircraft according to an embodiment of the invention.
Fig. 2 is an exploded view of a nacelle quick release of an aircraft according to an embodiment of the invention.
FIG. 3 is an exploded view of the mounting bracket and the elastic member of the nacelle quick release device of an aircraft according to an embodiment of the invention.
Fig. 4 is a schematic structural diagram of a snap fastener of a nacelle quick release device of an aircraft according to an embodiment of the invention.
Fig. 5 is a schematic structural diagram of an elastic component of a nacelle quick release device of an aircraft according to an embodiment of the invention.
Description of reference numerals:
mounting frame 1
Mounting hole 111
Snap ring 12
Notch 13
Abutting part 131
Inlet portion 132
Connecting hole 14
Latch 22
Insertion end 221
Elastic member 3
Connecting piece 31
Nacelle quick release 100
Cloud platform 200
Detailed Description
The present invention will be more clearly and completely described below by way of examples and with reference to the accompanying drawings, but the present invention is not limited thereto.
The aircraft of the embodiment of the invention comprises a nacelle quick release device 100, and the specific structure of the nacelle quick release device 100 is shown in fig. 1 to 5. The nacelle quick release device 100 comprises a mounting frame 1, a fastener 2 and at least one elastic part 3, wherein the fastener 2 is rotatable relative to the mounting frame 1 so that the fastener 2 can be detachably connected to the mounting frame 1. Mounting bracket 1 is installed and is fixed on the fuselage, buckle spare 2 is used for erection joint on cloud platform 200, buckle spare 2 detachably connects on mounting bracket 1, buckle spare 2 will be connected on mounting bracket 1 through anticlockwise rotation, buckle spare 2 will break away from in mounting bracket 1 through clockwise, make the rotation through buckle spare 2, make the loading and unloading between buckle spare 2 and the mounting bracket 1, the installation is dismantled fast and conveniently, has improved nacelle quick detach device 100's work efficiency greatly.
One side of buckle spare 2 towards mounting bracket 1 is equipped with at least one positioning groove 21, and elastic component 3 and positioning groove 21 one-to-one, elastic component 3's one end is connected in mounting bracket 1, and elastic component 3's the other end detachably connects in positioning groove 21. When the fastener 2 is to be connected to the mounting bracket 1 through counterclockwise rotation, the bottom of the elastic component 3 is to abut against the top surface of the fastener 2 and slide on the top surface of the fastener 2, the positioning groove 21 is formed in the top surface of the fastener 2, so that the elastic component 3 can slide into the positioning groove 21 in a matched manner, the elastic component 3 is inserted into the positioning groove 21, the fastener 2 is prevented from moving along the circumferential direction when being connected to the mounting bracket 1, and the fastener 2 is effectively prevented from moving along clockwise or counterclockwise rotation through the elastic component 3. The acting force is exerted by external force to rotate clockwise on the fastener 2, so that the bottom of the elastic component 3 is separated from the positioning groove 21, and the fastener 2 and the mounting rack 1 are detached. Prevent effectively through elastomeric element 3 that buckle 2 from removing along the circumferencial direction, improved the safety and stability nature of aircraft greatly.
The mounting bracket 1 may include a bracket body 11 and a snap ring 12, the bracket body 11 has a mounting hole 111, the snap ring 12 is connected to the mounting hole 111, the snap member 2 is inserted into the mounting hole 111 and detachably connected to the snap ring 12, and the elastic member 3 is connected to the bracket body 11. The snap ring 12 is inserted into the mounting hole 111 of the frame body 11, so that the snap ring 2 is conveniently connected with the snap ring 12 in a positioning manner, and the connection is more convenient. Meanwhile, the mounting frame 1 is simple in structure and convenient to manufacture and assemble.
The clamping piece 2 can be provided with at least one clamping block 22, the clamping block 22 extends and protrudes along the radial direction of the clamping piece 2, the mounting frame 1 is provided with at least one notch 13, the notch 13 extends and is arranged along the rotating direction of the clamping piece 2, the clamping blocks 22 correspond to the notches 13 one by one, the clamping blocks 22 are clamped in the notches 13, and the clamping blocks 22 can move in the notches 13. The clamping block 22 can be inserted into the notch 13 and move in the notch 13 by the anticlockwise rotation of the clamping piece 2, so that the clamping piece 2 is connected to the mounting rack 1; the clamping block 22 moves in the notch 13 and is separated from the notch 13 through clockwise rotation of the clamping piece 2, so that the clamping piece 2 is detached from the mounting frame 1. The fixture block 22 and the notch 13 are matched to realize rotary disassembly and assembly, the structure is simple, and the processing and the manufacturing are convenient. Preferably, the number of the latch blocks 22 is two, and the two latch blocks 22 are respectively arranged on two sides of the fastener 2; the number of the notches 13 is two, and the two notches 13 are respectively arranged at two ends of the inner wall surface of the clamping ring 12.
Both ends of the notch 13 may have an abutting portion 131 and an inlet portion 132, respectively, and an upper end of the inlet portion 132 is inclined. Buckle 2 is when installing to mounting bracket 1, and fixture block 22 will contact earlier and hold in place portion 132, and the upper end that holds in place portion 132 will lean on in the contact of the lower extreme of fixture block 22, is the slope form through the upper end that holds in place portion 132, plays the guide effect, and the fixture block 22 of being convenient for inserts to breach 13. The latch 22 is inserted into the notch 13 through the inlet portion 132, and the latch 22 moves in the notch 13 and abuts against the abutting portion 131, so that the latch 22 is connected with the notch 13.
The latch 22 abuts against the abutting portion 131 so that the elastic member 3 is inserted into the positioning groove 21. The fixture block 22 moves in the notch 13 and is finally abutted against the abutting portion 131, the bottom of the elastic component 3 slides on the top surface of the fastener 2 and is finally inserted into the positioning groove 21, the fixture block 22 is abutted against the abutting portion 131, at the moment, the bottom of the elastic component 3 is also inserted into the positioning groove 21 at the same time, so that the fastener 2 is fastened and fixed on the mounting frame 1 and is matched with the elastic component 3 for positioning, the structural connection strength is high, and the stability of the quick-release pod device 100 is improved.
The end of the latch 22 has an insertion end 221, and the lower end of the insertion end 221 may be inclined. When the fastening member 2 is mounted to the mounting bracket 1, the lower end of the latching block 22 will contact the inlet portion 132 first, and the lower end of the insertion end 221 is inclined to play a guiding role, so that the latching block 22 can be inserted into the notch 13 conveniently.
One side of the latch 2 facing the mounting bracket 1 may be provided with at least one guide groove 23, the guide groove 23 extends along a rotation direction of the latch 2, the guide grooves 23 correspond to the elastic members 3 one to one, and the elastic members 3 are inserted into the guide grooves 23 and move in the guide grooves 23. The buckle 2 and the mounting bracket 1 are assembled and disassembled, the bottom of the elastic component 3 slides on the top surface of the buckle 2, the guide groove 23 is formed in the top surface of the buckle 2, the guide groove 23 plays a role in guiding, the elastic component 3 can move along a given track in the guide groove 23, the elastic component 3 can be accurately inserted into the positioning groove 21, the phenomenon of offset and dislocation generated in the use process of the elastic component 3 is effectively avoided, and the stability and reliability of the pod quick-disassembling device 100 are improved.
Elastic component 3 can be including connecting piece 31, elastomer (not shown in the figure) and reference column 32, and connecting piece 31 connects in mounting bracket 1, and the bottom of connecting piece 31 is equipped with the opening, has in the connecting piece 31 and holds the chamber, and the opening is linked together with holding the chamber, and the elastomer is located and holds the intracavity, and the one end of elastomer supports and leans on in connecting piece 31, and the other end of elastomer supports and leans on in reference column 32, and reference column 32 passes the opening and inserts to positioning groove 21 in. Both ends through the elastomer lean on respectively in connecting piece 31 and reference column 32 for reference column 32 can the displacement of floating from top to bottom, and the bottom of reference column 32 is inserting to positioning groove 21 in, when buckle spare 2 and mounting bracket 1 are dismantled to needs, exerts the effort on buckle spare 2, makes reference column 32 will the rebound and break away from out positioning groove 21, realizes the dismantlement between buckle spare 2 and the mounting bracket 1. The elastic component 3 has simple structure and convenient manufacture. Meanwhile, the positioning column 32 and the elastic body move in the accommodating cavity, and the installation is convenient and the stability is high. Preferably, the elastic body may be a spring, and the positioning column 32 may be a steel ball.
The mounting bracket 1 is provided with at least one connecting hole 14, the connecting hole 14 extends along the direction close to the positioning groove 21, the connecting holes 14 correspond to the elastic parts 3 one by one, and the connecting piece 31 is screwed in the connecting hole 14. The outer peripheral surface of the connecting piece 31 is provided with threads, the connecting piece 31 is in threaded connection with the connecting hole 14, the elastic part 3 can be adjusted in the vertical position by rotating the connecting piece 31, so that the matching acting force between the elastic part 3 and the buckling piece 2 can be adjusted, and the stability of the nacelle quick-release device 100 is improved.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "top", "bottom", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are only for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention.
While specific embodiments of the invention have been described above, it will be appreciated by those skilled in the art that this is by way of example only, and that the scope of the invention is defined by the appended claims. Various changes and modifications to these embodiments may be made by those skilled in the art without departing from the spirit and scope of the invention, and these changes and modifications are within the scope of the invention.
Claims (10)
1. The nacelle quick-release device is characterized by comprising an installation frame, a buckling piece and at least one elastic component, wherein the buckling piece is rotatable relative to the installation frame so that the buckling piece is detachably connected to the installation frame, at least one positioning groove is formed in one side, facing the installation frame, of the buckling piece, the elastic component corresponds to the positioning groove in a one-to-one mode, one end of the elastic component is connected to the installation frame, and the other end of the elastic component is detachably connected to the inside of the positioning groove.
2. The nacelle quick release device as claimed in claim 1, wherein the snap member has at least one detent extending in a radial direction of the snap member, the mounting bracket has at least one notch extending in a rotational direction of the snap member, the detent corresponds to the notch, the detent is engaged with the notch, and the detent is movable in the notch.
3. The quick pod release apparatus of claim 2, wherein the notch has an abutting portion and an inlet portion at both ends thereof, and the upper end of the inlet portion is inclined.
4. The pod quick release device of claim 3, wherein the latch abuts against the abutment portion to allow the resilient member to be inserted into the positioning groove.
5. The pod quick release apparatus of claim 1, wherein the end of the latch has an insertion end, and the insertion end has a lower end that is inclined.
6. The quick-release device for the nacelle according to claim 1, wherein the elastic member comprises a connecting member, an elastic body and a positioning post, the connecting member is connected to the mounting bracket, an opening is formed in the bottom of the connecting member, a receiving cavity is formed in the connecting member, the opening is communicated with the receiving cavity, the elastic body is located in the receiving cavity, one end of the elastic body abuts against the connecting member, the other end of the elastic body abuts against the positioning post, and the positioning post passes through the opening and is inserted into the positioning groove.
7. The quick release device of claim 6, wherein the mounting bracket has at least one connecting hole extending in a direction close to the positioning groove, the connecting hole is in one-to-one correspondence with the elastic member, and the connecting member is screwed into the connecting hole.
8. The quick release device of claim 1, wherein the latch has at least one guide slot on a side thereof facing the mounting bracket, the guide slot extending in a rotation direction of the latch, the guide slot corresponding to the elastic member one by one, and the elastic member being inserted into the guide slot and moving in the guide slot.
9. The pod quick release apparatus of claim 1, wherein the mounting bracket comprises a bracket body having a mounting hole and a snap ring, the snap ring being coupled to the mounting hole, the snap ring being inserted into the mounting hole and being removably coupled to the snap ring, the resilient member being coupled to the bracket body.
10. An aircraft, characterized in that it comprises a nacelle de-rigging device according to any one of claims 1-9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811141656.XA CN110963062B (en) | 2018-09-28 | 2018-09-28 | Nacelle quick detach device and contain its aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811141656.XA CN110963062B (en) | 2018-09-28 | 2018-09-28 | Nacelle quick detach device and contain its aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110963062A true CN110963062A (en) | 2020-04-07 |
| CN110963062B CN110963062B (en) | 2023-02-17 |
Family
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| Application Number | Title | Priority Date | Filing Date |
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| CN201811141656.XA Active CN110963062B (en) | 2018-09-28 | 2018-09-28 | Nacelle quick detach device and contain its aircraft |
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| Country | Link |
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| CN (1) | CN110963062B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111664329A (en) * | 2020-06-03 | 2020-09-15 | 中国人民解放军96901部队25分队 | Integrated photoelectric turret |
| CN117446199A (en) * | 2023-12-11 | 2024-01-26 | 中国科学院长春光学精密机械与物理研究所 | Quick loading and unloading device for airborne photoelectric nacelle |
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| CN110963062B (en) | 2023-02-17 |
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