CN104690525A - Aircraft cabin section disassembling device - Google Patents
Aircraft cabin section disassembling device Download PDFInfo
- Publication number
- CN104690525A CN104690525A CN201410751509.XA CN201410751509A CN104690525A CN 104690525 A CN104690525 A CN 104690525A CN 201410751509 A CN201410751509 A CN 201410751509A CN 104690525 A CN104690525 A CN 104690525A
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- cabin section
- connects
- connecting rod
- rotating shaft
- handwheel
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/02—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for connecting objects by press fit or for detaching same
- B23P19/025—For detaching only
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
- B23P2700/01—Aircraft parts
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Transmission Devices (AREA)
Abstract
The invention provides an aircraft cabin section disassembling device. The aircraft cabin section disassembling device comprises a base, a connecting rod mechanism, a tackle, a carrying mechanism and a fine adjusting mechanism, wherein the connecting rod mechanism is connected with the base and the tackle and used for converting rotation of the connecting rod mechanism into displacement between the base and the tackle; the base is used for fixing a cabin section A; the tackle is used for fixing a cabin section B; the carrying mechanism is arranged on the inner side of the base and used for lifting, dropping and carrying the cabin section A; the fine adjusting mechanism is arranged on the lower side of the tackle and used for lifting and dropping the cabin section B. According to the aircraft cabin section disassembling device, a first slider, a first guide rail and a connecting rod machine on the tackle jointly constitute a crank-slider mechanism, rotation of a long connecting rod is converted into linear movement of the tackle along the first guide rail, and the cabin section disassembly is easily realized according to the lever principle; a cushion block can protect the cabin sections and prevent abrasion during assembling; the aircraft cabin section disassembling device is applicable to the cabin section disassembly of a large length-diameter ratio aircraft adopting a non-metallic O-ring static sealing structure.
Description
Technical field
The present invention relates to Design of Mechanical Structure technical field, specifically a kind of big L/D ratio aircraft cabin section disassembling apparatus.
Background technology
For ease of manufacturing and general assembly, the aircraft of big L/D ratio is made up of some cabins section usually.At present, user improves day by day for the storage life of aircraft and non-maintaining time requirement.Therefore, course of new aircraft generally adopts nonmetal O type circle static seal in the design of cabin section disassemblying structure, reduces the humiture, salt fog, mould etc. of external environment to precision components performance impact in cabin.Fig. 1 is shown in by O type circle static seal structure schematic diagram.The cylindrical or inner circle of section end, cabin are designed with the groove that cross section is rectangle, and nonmetallic O type circle is arranged in groove, seals.
Need each cabin section to disassemble when daily test and periodic maintenance, what O type circle increased aircraft greatly disassembles difficulty.When cabin section is disassembled in the past, only need that workman is free-hand to be separated two adjacent compartment sections.And there is very large force of sliding friction between O type circle in new disassemblying structure and cabin section, cannot rely on manually to complete and disassemble.
In addition, the design feature of aircraft determines that disassembling operation must complete under level.The fine structure that aircraft outer surface gathers also further increases separating difficulty.Above-mentioned two aspect factors cause market not have ripe equipment to purchase or existing structure can be used.
Do not find explanation or the report of similar techniques at present, not yet collect similar data both at home and abroad yet.
Summary of the invention
For defect of the prior art, the object of this invention is to provide a kind of big L/D ratio aircraft cabin section disassembling apparatus.
According to aircraft cabin provided by the invention section disassembling apparatus, comprise base, linkage, coaster, carrying mechanism 5 and micro-adjusting mechanism;
Wherein, described linkage connects described base and described coaster, and own rotation is converted to the displacement between described base and described coaster by linkage; Described base is used for sealed cabin section A; Described coaster is used for sealed cabin section B;
Described carrying mechanism is arranged on the inner side of described base, for lifting and the carrying of cabin section A; Described micro-adjusting mechanism is arranged on the downside of described coaster, for the lifting of cabin section B.
Preferably, described base 1 comprises lathe bed 7 and the first fixture;
Described first fixture connects described lathe bed 7, and described first fixture is used for cabin section A to be fixed on lathe bed 7;
Described first fixture comprises the first handwheel 8, first screw rod 9, first portal frame 10 and the first briquetting 11; Described first screw rod 9 runs through and described first portal frame 10 that is threaded, and one end of described first screw rod 9 connects described first handwheel 8, and the other end connects the first briquetting 11; Described first portal frame 10 connects described lathe bed 7;
Described lathe bed 7 upper end is provided with first connecting rod installing hole; One end of described linkage 2 connects described first connecting rod installing hole; The inner side of described lathe bed 7 upper end is provided with cushion block installation portion.
Preferably, cushion block 3 is also comprised; Described cushion block 3 is arranged on described cushion block installation portion.
Preferably, linkage 2 comprises rotating shaft A12, short connecting rod 13, rotating shaft B14, rotating shaft C 15 and long connecting rod 16;
Wherein, short connecting rod 13 connects described long connecting rod 16 by described rotating shaft B14; Described rotating shaft A12 is arranged in described first connecting rod installing hole; Described rotating shaft C 15 connects described coaster 4.
Preferably, coaster 4 comprises the second fixture, U-type groove 18, first slide block 19, backing plate 23 and the first guide rail 24;
Described U-type groove 18 connects described first guide rail 24 by described first slide block 19; The both sides of described U-type groove 18 are provided with second connecting rod installing hole, and described rotating shaft C 15 is arranged in described second connecting rod installing hole;
Described backing plate 23 is arranged on the both sides of described U-type groove 18 bottom land; Described second fixture connects described U-type groove 18, for being fixed on by cabin section B in described U-type groove 18;
Described second fixture comprises the second handwheel 20, second screw rod 21, second portal frame 17 and the second briquetting 22; Described second screw rod 21 runs through and described second portal frame 17 that is threaded, and one end of described second screw rod 21 connects described second handwheel 20, and the other end connects the second briquetting 22; Described second portal frame 17 connects described U-type groove 18.
Preferably, carrying mechanism 5 comprises the second guide rail, the rotating shaft 29 of supporting plate 25, first worm and wormwheel lift 26, second slide block 27, first shaft coupling 28, first, the 3rd handwheel 30, first commutator 31, rectangular slab 32;
Described rectangular slab 32 connects described second guide rail by described second slide block 27; Described worm and wormwheel lift 26 is arranged on the upside of described rectangular slab 32; Described 3rd handwheel 30 connects described first worm and wormwheel lift 26 by described first commutator 31, first rotating shaft 29, first shaft coupling 28 successively; Described supporting plate 25 connects described first worm and wormwheel lift 26;
Wherein, 3rd handwheel 30 drives the first commutator 31 to rotate, passing to the first worm and gear lift 26, first worm and gear lift 26 by the first shaft coupling 28 and the first rotating shaft 29 drives supporting plate 25 to move up and down, thus cabin section A and the first cushion block 3 are departed from;
The side of described lathe bed 7 is provided with the opening that the length direction along described second guide rail extends; Described 3rd handwheel 30 connects described commutator 31 through described opening.
Preferably, micro-adjusting mechanism 6 comprises link slot 33, second worm and gear lift 34, second shaft coupling 35, the 4th handwheel 36, second commutator 37 and the second rotating shaft 38;
Wherein, described 4th handwheel 36 connects described second worm and gear lift 34 by described second commutator 37, described second rotating shaft 38, second shaft coupling 35 successively; Described second worm and gear lift 34 connects described link slot 33;
First guide rail 24 is arranged on the both sides cell wall of described link slot 33;
4th handwheel 36 drives the second commutator 37, rotation is passed to the second worm and gear lift 34, realizes the elevating movement of cabin section B vertical direction; Described second worm and gear lift 34 is arranged on the base plate of described lathe bed 7.
Compared with prior art, the present invention has following beneficial effect:
1, in the present invention, supratrochlear first slide block, the first guide rail and connecting rod machine form slider-crank mechanism in the lump, the rotation of long connecting rod are changed into the rectilinear movement of coaster along the first guide rail, utilize lever principle, easily realize cabin section and disassemble;
2, in the present invention, cushion block can protect cabin section, weares and teares when preventing from disassembling;
3, the present invention is applicable to adopt the cabin section of the big L/D ratio aircraft of nonmetal O type circle static seal structure to disassemble.
Accompanying drawing explanation
By reading the detailed description done non-limiting example with reference to the following drawings, other features, objects and advantages of the present invention will become more obvious:
Fig. 1 is O type circle static seal structure schematic diagram in the present invention;
Fig. 2 is structural representation of the present invention;
Fig. 3 be of the present invention in partly cut open structural representation;
Fig. 4 is the structural representation of base in the present invention;
Fig. 5 is the structural representation of linkage in the present invention;
Fig. 6 is the structural representation of cushion block in the present invention;
Fig. 7 is the structural representation of coaster in the present invention;
Fig. 8 is the structural representation of carrying mechanism in the present invention;
Fig. 9 is the structural representation of micro-adjusting mechanism in the present invention.
In figure: 1 is base, 2 is linkage, 3 is cushion block, 4 is coaster, 5 is carrying mechanism, 6 is micro-adjusting mechanism, 7 is lathe bed, 8 is the first handwheel, 9 is the first screw rod, 10 is the first portal frame, 11 is the first briquetting, 12 is rotating shaft A, 13 is short connecting rod, 14 is rotating shaft B, 15 is rotating shaft C, 16 is long connecting rod, 17 is the second portal frame, 18 is U-type groove, 19 is the first slide block, 20 is the second handwheel, 21 is the second screw rod, 22 is the second briquetting, 23 is backing plate, 24 is the first guide rail, 25 is supporting plate, 26 is the first worm and gear lift, 27 is the second slide block, 28 is the first shaft coupling, 29 is the first rotating shaft, 30 is the 3rd handwheel, 31 is the first commutator, 32 is rectangular slab, 33 is link slot, 34 is the second worm and gear lift, 35 is the second shaft coupling, 36 is the 4th handwheel, 37 is the second commutator, 38 is the second rotating shaft, 39 is cushion block installation portion, 100 is cabin section A, 200 is cabin section B, 300 is O type circle.
Detailed description of the invention
Below in conjunction with specific embodiment, the present invention is described in detail.Following examples will contribute to those skilled in the art and understand the present invention further, but not limit the present invention in any form.It should be pointed out that to those skilled in the art, without departing from the inventive concept of the premise, some distortion and improvement can also be made.These all belong to protection scope of the present invention.
In the present embodiment, aircraft cabin provided by the invention section disassembling apparatus, comprises base 1, linkage 2, coaster 4, carrying mechanism 5 and micro-adjusting mechanism 6;
Wherein, described linkage 2 connects described base 1 and described coaster 4, for the rotation of linkage 2 being converted to the displacement between described base 1 and described coaster 4; Described base 1 is for sealed cabin section A; Described coaster 4 is for sealed cabin section B; Described carrying mechanism 5 is arranged on the inner side of described base 1, for lifting and the carrying of cabin section A; Described micro-adjusting mechanism 6 is arranged on the downside of described coaster 4, for the lifting of cabin section B.
Base 1, for installing each parts and assembly, adopts grey cast-iron casting, described base 1 bag lathe bed 7 and the first fixture; Described first fixture connects described lathe bed 7, and described first fixture is used for cabin section A to be fixed on lathe bed 7; Described first fixture comprises the first handwheel 8, first screw rod 9, first portal frame 10 and the first briquetting 11; Described first screw rod 9 runs through and described first portal frame 10 that is threaded, and one end of described first screw rod 9 connects described first handwheel 8, and the other end connects the first briquetting 11; Described first portal frame 10 connects described lathe bed 7; Described lathe bed 7 upper end is provided with first connecting rod installing hole; One end of described linkage 2 connects described first connecting rod installing hole; The inner side of described lathe bed 7 upper end is provided with cushion block installation portion.The quantity of described first fixture is two, is separately positioned on the correspondence position of both ends on lathe bed 7 of cabin section A.Driving the first screw rod 9 to rotate by rotating the first handwheel 8, making the first briquetting 11 compress cabin section, preventing cabin section A from when disassembling, axial float occurring.
Aircraft cabin provided by the invention section disassembling apparatus also comprises cushion block 3; Described cushion block 3 is arranged on described cushion block installation portion.Cushion block 3 adopts nonmetal making, and for the protection of cabin section, weares and teares when preventing from disassembling.
Linkage 2 comprises rotating shaft A12, short connecting rod 13, rotating shaft B14, rotating shaft C 15 and long connecting rod 16; Wherein, short connecting rod 13 connects described long connecting rod 16 by described rotating shaft B14; Described rotating shaft A12 is arranged in described first connecting rod installing hole; Described rotating shaft C 15 connects described coaster 4.
Coaster 4 comprises the second fixture, U-type groove 18, first slide block 19, backing plate 23 and the first guide rail 24; Described U-type groove 18 connects described first guide rail 24 by described first slide block 19; The both sides of described U-type groove 18 are provided with second connecting rod installing hole, and described rotating shaft C 15 is arranged in described second connecting rod installing hole; Described backing plate 23 is arranged on the both sides of described U-type groove 18 bottom land; Described second fixture connects described U-type groove 18, for being fixed on by cabin section B in described U-type groove 18; Described second fixture comprises the second handwheel 20, second screw rod 21, second portal frame 17 and the second briquetting 22; Described second screw rod 21 runs through and described second portal frame 17 that is threaded, and one end of described second screw rod 21 connects described second handwheel 20, and the other end connects the second briquetting 22; Described second portal frame 17 connects described U-type groove 18.U-type groove 18 adopts steel plate butt welding to form.Backing plate 23 is specially nylon back plate, for the protection of cabin section B, weares and teares when preventing from disassembling.Driving the second screw rod 21 to rotate by rotating the second handwheel 20, making the second briquetting 22 compress cabin section B, preventing cabin section B from when disassembling, axial float occurring; The first slide block 19, first guide rail 24 on coaster 4 forms slider-crank mechanism in the lump with above-mentioned linkage 2, the rotation of long connecting rod 16 is changed into the rectilinear movement of coaster 4 along the first guide rail 24, thus realizes cabin section and disassemble.The quantity of described second fixture is two, is separately positioned on the both ends of described U-type groove 18.The quantity of the first slide block 19 is six, distributes in the bilateral symmetry of U-type groove 18.
The cabin section reach of carrying mechanism 5 for disassembling, to carry out disassembling of follow-up cabin section.Carrying mechanism 5 comprises the second guide rail, the rotating shaft 29 of supporting plate 25, first worm and wormwheel lift 26, second slide block 27, first shaft coupling 28, first, the 3rd handwheel 30, first commutator 31, rectangular slab 32; Described rectangular slab 32 connects described second guide rail by described second slide block 27; Described worm and wormwheel lift 26 is arranged on the upside of described rectangular slab 32; Described 3rd handwheel 30 connects described first worm and wormwheel lift 26 by described first commutator 31, first rotating shaft 29, first shaft coupling 28 successively; Described supporting plate 25 connects described first worm and wormwheel lift 26; Wherein, 3rd handwheel 30 drives the first commutator 31 to rotate, the first worm and gear lift 26 is passed to by the first shaft coupling 28 and the first rotating shaft 29, first worm and gear lift 26 drives supporting plate 25 to move up and down, thus cabin section A and the first cushion block 3 are departed from, more manually promotion cabin section moves forward along guide rail; The side of described lathe bed 7 is provided with the opening that the length direction along described second guide rail extends; Described 3rd handwheel 30 connects described commutator 31 through described opening.The quantity of the second slide block 27 is 8, is uniformly distributed in the both sides of the second guide rail.The quantity of the first worm and wormwheel lift 26, first shaft coupling 28, first rotating shaft 29 is two, and the two ends of the first commutator 31 connect described first rotating shaft 29, first shaft coupling 28, first worm and wormwheel lift 26 respectively in turn.
Micro-adjusting mechanism 6, for the height of adjusting cabin section B, makes the dead in line of its theoretical axis and cabin section A.Micro-adjusting mechanism 6 comprises link slot 33, second worm and gear lift 34, second shaft coupling 35, the 4th handwheel 36, second commutator 37 and the second rotating shaft 38; , described 4th handwheel 36 connects described second worm and gear lift 34 by described second commutator 37, described second rotating shaft 38, second shaft coupling 35 successively; Described second worm and gear lift 34 connects described link slot 33; First guide rail 24 is arranged on the both sides cell wall of described link slot 33, is specially, and the upper surface of described link slot 32 is for installing the guide rail of coaster 4; 4th handwheel 36 drives the second commutator 37, rotation is passed to the second worm and gear lift 34, realizes the elevating movement of cabin section B vertical direction; Described second worm and gear lift 34 is arranged on the base plate of described lathe bed 7.The quantity of the second worm and gear lift 34, second shaft coupling 35 and the second rotating shaft 38 is two; The two ends of described second commutator 37 connect the second rotating shaft 38, second shaft coupling 35 and the second worm and gear lift 34 respectively in turn.
The present invention is applicable to adopt the cabin section of the big L/D ratio aircraft of nonmetal O type circle static seal structure to disassemble.
Aircraft cabin provided by the invention section disassembling apparatus, job step is as follows:
The first step, is placed on the section disassembling apparatus of aircraft cabin provided by the invention by aircraft, rotate the handwheel of micro-adjusting mechanism 6, and the backing plate 23 in coaster 4 is fitted with aircraft surface;
Second step, rotates the handwheel above portal frame, and cabin section is compressed by briquetting, ensures that cabin section play can not occur when disassembling.
3rd step, rotation linkage assembly, makes cabin section disassemble.
4th step, rotates the handwheel above portal frame, unclamps pressing plate; Independent cabin section under dismounting is taken out;
5th step, rotates the handwheel in carrying mechanism, rises supporting plate, cabin section and cushion block 3 are departed from, and manually promotes the slide of cabin section along carrying mechanism to next station.
Repeat the first step to the 5th step, complete each cabin section successively and disassemble.
Above specific embodiments of the invention are described.It is to be appreciated that the present invention is not limited to above-mentioned particular implementation, those skilled in the art can make various distortion or amendment within the scope of the claims, and this does not affect flesh and blood of the present invention.
Claims (7)
1. an aircraft cabin section disassembling apparatus, is characterized in that, comprises base (1), linkage (2), coaster (4), carrying mechanism (5) and micro-adjusting mechanism (6);
Wherein, described linkage (2) connects described base (1) and described coaster (4), and own rotation is converted to the displacement between described base (1) and described coaster (4) by linkage (2); Described base (1) is for sealed cabin section A; Described coaster (4) is for sealed cabin section B;
Described carrying mechanism (5) is arranged on the inner side of described base (1), for lifting and the carrying of cabin section A; Described micro-adjusting mechanism (6) is arranged on the downside of described coaster (4), for the lifting of cabin section B.
2. aircraft cabin according to claim 1 section disassembling apparatus, is characterized in that, described base (1) comprises lathe bed (7) and the first fixture;
Described first fixture connects described lathe bed (7), and described first fixture is used for cabin section A to be fixed on lathe bed (7);
Described first fixture comprises the first handwheel (8), the first screw rod (9), the first portal frame (10) and the first briquetting (11); Described first screw rod (9) is run through and described first portal frame (10) that is threaded, and one end of described first screw rod (9) connects described first handwheel (8), and the other end connects the first briquetting (11); Described first portal frame (10) connects described lathe bed (7);
Described lathe bed (7) upper end is provided with first connecting rod installing hole; One end of described linkage (2) connects described first connecting rod installing hole; The inner side of described lathe bed (7) upper end is provided with cushion block installation portion.
3. aircraft cabin according to claim 2 section disassembling apparatus, is characterized in that, also comprises cushion block (3); Described cushion block (3) is arranged on described cushion block installation portion.
4. aircraft cabin according to claim 2 section disassembling apparatus, it is characterized in that, linkage (2) comprises rotating shaft A (12), short connecting rod (13), rotating shaft B (14), rotating shaft C (15) and long connecting rod (16);
Wherein, short connecting rod (13) connects described long connecting rod (16) by described rotating shaft B (14); Described rotating shaft A (12) is arranged in described first connecting rod installing hole; Described rotating shaft C (15) connects described coaster (4).
5. aircraft cabin according to claim 4 section disassembling apparatus, it is characterized in that, coaster (4) comprises the second fixture, U-type groove (18), the first slide block (19), backing plate (23) and the first guide rail (24);
Described U-type groove (18) connects described first guide rail (24) by described first slide block (19); The both sides of described U-type groove (18) are provided with second connecting rod installing hole, and described rotating shaft C (15) is arranged in described second connecting rod installing hole;
Described backing plate (23) is arranged on the both sides of described U-type groove (18) bottom land; Described second fixture connects described U-type groove (18), for being fixed on by cabin section B in described U-type groove (18);
Described second fixture comprises the second handwheel (20), the second screw rod (21), the second portal frame (17) and the second briquetting (22); Described second screw rod (21) is run through and described second portal frame (17) that is threaded, one end of described second screw rod (21) connects described second handwheel (20), and the other end connects the second briquetting (22); Described second portal frame (17) connects described U-type groove (18).
6. aircraft cabin according to claim 2 section disassembling apparatus, it is characterized in that, carrying mechanism (5) comprises the second guide rail, supporting plate (25), the first worm and wormwheel lift (26), the second slide block (27), the first shaft coupling (28), the first rotating shaft (29), the 3rd handwheel (30), the first commutator (31), rectangular slab (32);
Described rectangular slab (32) connects described second guide rail by described second slide block (27); Described worm and wormwheel lift (26) is arranged on the upside of described rectangular slab (32); Described 3rd handwheel (30) connects described first worm and wormwheel lift (26) by described first commutator (31), the first rotating shaft (29), the first shaft coupling (28) successively; Described supporting plate (25) connects described first worm and wormwheel lift (26);
Wherein, 3rd handwheel (30) drives the first commutator (31) to rotate, the first worm and gear lift (26) is passed to by the first shaft coupling (28) and the first rotating shaft (29), first worm and gear lift (26) drives supporting plate (25) to move up and down, thus cabin section A and the first cushion block (3) are departed from;
The side of described lathe bed (7) is provided with the opening that the length direction along described second guide rail extends; Described 3rd handwheel (30) connects described commutator (31) through described opening.
7. aircraft cabin according to claim 5 section disassembling apparatus, it is characterized in that, micro-adjusting mechanism (6) comprises link slot (33), the second worm and gear lift (34), the second shaft coupling (35), the 4th handwheel (36), the second commutator (37) and the second rotating shaft (38);
Wherein, described 4th handwheel (36) connects described second worm and gear lift (34) by described second commutator (37), described second rotating shaft (38), the second shaft coupling (35) successively; Described second worm and gear lift (34) connects described link slot (33);
First guide rail (24) is arranged on the both sides cell wall of described link slot (33);
4th handwheel (36) drives the second commutator (37), rotation is passed to the second worm and gear lift (34), realizes the elevating movement of cabin section B vertical direction; Described second worm and gear lift (34) is arranged on the base plate of described lathe bed (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410751509.XA CN104690525B (en) | 2014-12-09 | 2014-12-09 | Aircraft cabin section disassembling device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410751509.XA CN104690525B (en) | 2014-12-09 | 2014-12-09 | Aircraft cabin section disassembling device |
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| Publication Number | Publication Date |
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| CN104690525A true CN104690525A (en) | 2015-06-10 |
| CN104690525B CN104690525B (en) | 2017-03-22 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410751509.XA Active CN104690525B (en) | 2014-12-09 | 2014-12-09 | Aircraft cabin section disassembling device |
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| CN (1) | CN104690525B (en) |
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| CN111056242A (en) * | 2019-12-06 | 2020-04-24 | 中铁隧道局集团有限公司 | Shield constructs screw conveyer detaching device |
| CN112643310A (en) * | 2020-12-18 | 2021-04-13 | 杭州智行远机器人技术有限公司 | Nuclear industry equipment dismounting robot and rapid dismounting method |
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|---|---|---|---|---|
| CN111056242A (en) * | 2019-12-06 | 2020-04-24 | 中铁隧道局集团有限公司 | Shield constructs screw conveyer detaching device |
| CN112643310A (en) * | 2020-12-18 | 2021-04-13 | 杭州智行远机器人技术有限公司 | Nuclear industry equipment dismounting robot and rapid dismounting method |
| CN112643310B (en) * | 2020-12-18 | 2022-03-11 | 杭州智行远机器人技术有限公司 | Nuclear industry equipment dismounting robot and rapid dismounting method |
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| Publication number | Publication date |
|---|---|
| CN104690525B (en) | 2017-03-22 |
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