CN106114897B - A kind of slide-type helicopter Intelligent lifting conveying arrangement - Google Patents
A kind of slide-type helicopter Intelligent lifting conveying arrangement Download PDFInfo
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- CN106114897B CN106114897B CN201610643686.5A CN201610643686A CN106114897B CN 106114897 B CN106114897 B CN 106114897B CN 201610643686 A CN201610643686 A CN 201610643686A CN 106114897 B CN106114897 B CN 106114897B
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- platform
- lifting
- halfpace
- cylinder
- helicopter
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- 230000003028 elevating effect Effects 0.000 claims description 15
- 238000009434 installation Methods 0.000 claims description 6
- 229910000831 Steel Inorganic materials 0.000 claims description 5
- 238000000034 method Methods 0.000 claims description 5
- 239000010959 steel Substances 0.000 claims description 5
- 230000001360 synchronised effect Effects 0.000 claims description 5
- 230000008569 process Effects 0.000 claims description 4
- 239000002131 composite material Substances 0.000 claims description 3
- 238000009826 distribution Methods 0.000 claims description 3
- 230000000630 rising effect Effects 0.000 claims description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- 229910045601 alloy Inorganic materials 0.000 claims description 2
- 229910052799 carbon Inorganic materials 0.000 claims description 2
- 230000008878 coupling Effects 0.000 claims description 2
- 238000010168 coupling process Methods 0.000 claims description 2
- 238000005859 coupling reaction Methods 0.000 claims description 2
- 239000000835 fiber Substances 0.000 claims description 2
- 230000008901 benefit Effects 0.000 abstract description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 241000209140 Triticum Species 0.000 description 1
- 235000021307 Triticum Nutrition 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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- 230000006872 improvement Effects 0.000 description 1
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- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
- B64F1/222—Ground or aircraft-carrier-deck installations for handling aircraft for storing aircraft, e.g. in hangars
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Escalators And Moving Walkways (AREA)
Abstract
Description
Claims (2)
- A kind of 1. slide-type helicopter Intelligent lifting conveying arrangement, it is characterised in that including:Stage apparatus (1), lifting device (2), halfpace device (3), driving device, spacing regulator (5), air cushion (6);The stage apparatus includes:Platform I (11), platform II (12), mobile platform (13), the platform I (11) and the platform II (12) are symmetrical structure, by described Spacing regulator (5) links together, the platform I (11) and the platform II (12) welded using high intensity I-steel and Into;The mobile platform (13) has four sets, and the mobile platform (13) is respectively symmetrically installed on described by line slideway (16) The both ends of platform I (11) and the platform II (12), often cover and a cylinder block slideway are provided with the mobile platform (13) (14) and two lifting bracket slideways (15), locking device is carried on the line slideway (16);The lifting device (2) has four Set, is separately mounted on the mobile platform (13), the lifting device (2) includes:Lifting bracket (21), cylinder block (22), oil cylinder cylinder rod (23), the lifting bracket (21) have three, and the cylinder block (22) is supported in 120 ° of distributions, described For the floor installation of lifting bracket (21) in the lifting bracket slideway (15), the cylinder block (22) is installed on the oil cylinder In cylinder body slideway (14), the oil cylinder cylinder rod (23) is connected with the cylinder block (22), and the oil cylinder cylinder rod (23) is using high Strength alloys steel, the top of the oil cylinder cylinder rod (23) is frustum structure, easy to position the lifting hole of fuselage, realizes carrying for fuselage Rise;The cylinder block (22) is adjusted in the position of the cylinder block slideway (14), adjusts the bottom of the lifting bracket (21) Seat is realized that the lateral position of the lifting device is adjusted, is led by the straight line in the position of the lifting bracket slideway (15) Rail (16) adjusts the mobile platform (13) in the platform I (11) and the position of the platform II (12), realizes the lifting The lengthwise position of device is adjusted, and is adjusted the height of the oil cylinder cylinder rod (23), is finally realized different model slide-type helicopter machine The lifting of body;The halfpace device (3) has two sets, respectively in the platform I (11) and the platform II (12) Portion;The driving device includes Direct wheel drives and Mecanum wheel (4), and totally eight sets of the Mecanum wheel (4), every two sets are one Group is connected with the Direct wheel drives, and respectively four sets of Mikes of installation receive for the bottom of the platform I (11) and the platform II (12) Nurse wheel (4), realizes the comprehensive automatically walk of the stage apparatus (1);The halfpace device (3) includes:Put down on centre Platform (31), scissors fork elevating device (32), lift oil tank, middle lower platform;The middle lower platform is fixed on the platform On device (1), the middle lower platform and the middle upper mounting plate (31) are connected by the scissors fork elevating device (32), One end of the scissors fork elevating device (32) and the middle upper mounting plate (31) are fixedly connected, the scissors fork elevating dress The other end for putting (32) is installed in the slideway of the middle lower platform, and the lift oil tank is fixed on the middle lower platform On, the piston rod of the lift oil tank and the middle upper mounting plate (31) are fixedly connected, and pass through the lift oil tank piston rod It is flexible, coordinate the scissors fork elevating device (32) to realize the lifting of the middle upper mounting plate (31);Put down on the centre Platform (31) carries sensor, when detecting the skid of helicopter, stops rising;The halfpace dress of the platform I (11) The halfpace lock I is fixed in the side for putting (3), and the side of the halfpace device (3) of the platform II (12) is fixed The halfpace locks II, and the halfpace locks I and halfpace lock II is sealed, and auxiliary realizes the platform I (11) With being synchronized with the movement for platform II (12);Equidistant air cushion groove is provided with the middle upper mounting plate (31), is installed in the air cushion groove The air cushion (6);The air cushion (6) uses carbon fibre composite, and the inside of the air cushion (6) is distributed equidistant filament and connects The levels of the air cushion (6) are connect, the air cushion (6) is smooth when realizing inflation, while increases its reliability, the air cushion (6) end equipped with rotation button, open rotation button can automatic inflating, it is simple to operate;Slide-type helicopter and institute When stating middle upper mounting plate (31) contact, air cushion (6) automatic inflating described in rotation button is opened, the air cushion (6) is smooth after inflation The reliable slide-type helicopter that reduces impacts in transportational process caused by jolting whole device;The spacing regulator (5) include:The fixed leading screw in one end (51), scalable connecting rod (52), guide rod (53), motor, constant speed gear-box, leading screw spiral shell It is female;The motor is fixed on the bottom of described platform I (11) one end, and the fixed leading screw in one end (51) has two sets, the silk Thick stick nut has two sets, and two sets of feed screw nuts are fixed on the bottom of described platform II (12) one end, consolidate respectively with described one end Fixed pattern leading screw (51) coordinates;The output shaft of the motor and the input axis connection of constant speed gear-box, two of constant speed gear-box are defeated Shaft is connected with two sets of fixed leading screws in one end (51) respectively by shaft coupling, the described fixed leading screw in one end (51) one end The bottom of described platform I (11) one end is fixed on by bearing block, one end passes through the feed screw nut and the platform II (12) The bottom of one end is connected, and the guide rod (53) is connected between the platform I (11) and the platform II (12);The motor Rotate, drive the fixed leading screw in described one end (51) to rotate, the fixed leading screw in one end (51) drives the feed screw nut to move It is dynamic, the movement of the platform II (12) is realized, so as to fulfill the tune of distance between the platform I (11) and the platform II (12) It is whole;Described scalable connecting rod (52) one end is fixed on the bottom of one end of the platform I (11), the other end and the platform II (12) it is flexibly connected, the scalable connecting rod (52) uses retractable structure, as the platform I (11) and the platform II (12) when distance adjusts between, the scalable connecting rod (52) realizes guiding role, while realizes platform I (11) peace Platform II (12) are synchronized with the movement;According to the characteristics of the slide-type helicopter fuselage of different model, the position of adjustment lifting device (2) And hoisting depth, the spacing of stage apparatus and the lifting altitude of halfpace device (3) are adjusted, is realized to different model slide-type The fully-automatic intelligent transport of helicopter;After being transported to hangar, halfpace lock I and halfpace lock II are opened, Control the halfpace device (3) to carry out raising, adjust the cylinder block (22) in the cylinder block slideway (14) Position, adjusts the base of the lifting bracket (21) in the position of lifting bracket slideway (15), makes the oil cylinder cylinder rod (23) Top is withstood in the lifting hole of fuselage, controls the halfpace device (3) to carry out back drop, while control the platform I (11) It is gradually disengaged between the platform II (12), until helicopter skid completely disengages the middle upper mounting plate (31), adjusting institute The height of oil cylinder cylinder rod (23) is stated, the skid of fuselage is contacted with ground.
- 2. a kind of slide-type helicopter Intelligent lifting conveying arrangement as claimed in claim 1, it is characterised in that further include a control System processed, the control system control coordinated operation between whole device all parts;According to different model slide-type helicopter The characteristics of fuselage, the control system control the distance between the platform I (11) and described platform II (12) to adjust, and make described After platform I (11) and the platform II (12) are separated by a distance, scalable connecting rod (52) is retracted to the platform I (11) Bottom;The control system control driving device realizes the comprehensive automatically walk of the stage apparatus (1), the control System processed controls the stage apparatus (1) through the fuselage of slide-type helicopter;The cylinder block (22) is adjusted in the oil The position of cylinder cylinder body slideway (14), adjusts the base of the lifting bracket (21) in the position of lifting bracket slideway (15), makes institute The top for stating oil cylinder cylinder rod (23) is withstood in the lifting hole of fuselage, is adjusted the height of the oil cylinder cylinder rod (23), is realized helicopter The lifting of fuselage, makes the skid of fuselage depart from ground;The control system controls the platform I (11) and the platform II (12) The distance between adjust, the platform I (11) and the platform II (12) is gradually drawn close, the cylinder block (22) is along described Cylinder block slideway (14) is moved to both sides;The halfpace device (3) is controlled to carry out raising, according to the middle upper mounting plate (31) sensor feedback information, when the skid of middle upper mounting plate (31) the contact helicopter, stops raising;Described in reduction The height of the oil cylinder cylinder rod (23) of lifting device (2), controls the halfpace device (3) to carry out back drop, returns drop and stablizes The halfpace lock I and halfpace lock II are sealed afterwards, and the scalable connecting rod (52) is elongated to the platform II (12) in;The control system controls the Mecanum wheel (4) comprehensive automatically walk of the driving device;Finally control Whole device leaves hangar.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201610643686.5A CN106114897B (en) | 2016-08-08 | 2016-08-08 | A kind of slide-type helicopter Intelligent lifting conveying arrangement |
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CN201610643686.5A CN106114897B (en) | 2016-08-08 | 2016-08-08 | A kind of slide-type helicopter Intelligent lifting conveying arrangement |
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CN106114897A CN106114897A (en) | 2016-11-16 |
CN106114897B true CN106114897B (en) | 2018-04-17 |
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CN201610643686.5A Active CN106114897B (en) | 2016-08-08 | 2016-08-08 | A kind of slide-type helicopter Intelligent lifting conveying arrangement |
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Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108609197B (en) * | 2018-06-25 | 2023-12-15 | 青岛科技大学 | Skid type helicopter ground omnidirectional moving device |
CN109665115A (en) * | 2018-12-29 | 2019-04-23 | 飞智控(天津)科技有限公司 | Helicopter transport system and transportation resources |
CN110406454B (en) * | 2019-06-29 | 2022-04-01 | 芜湖航翼集成设备有限公司 | Quick carrying equipment for emergency rescue of airplane |
CN113147560B (en) * | 2021-04-22 | 2022-05-20 | 江阴秋钧机电设备有限公司 | Road transport vehicle for airplane fuselage parts |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE202007006340U1 (en) * | 2006-09-28 | 2007-09-06 | Bünning, Thorsten | Universal tow bar for the helicopter Sea Lynx |
CN203684118U (en) * | 2013-12-04 | 2014-07-02 | 海丰通航科技有限公司 | Lifting platform for ascending and descending of helicopter |
CN205931304U (en) * | 2016-08-08 | 2017-02-08 | 青岛科技大学 | Skid formula helicopter intelligence promotes conveyer |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3938417B2 (en) * | 1997-07-29 | 2007-06-27 | 多摩川精機株式会社 | Transport device |
GB0915831D0 (en) * | 2009-09-10 | 2009-10-07 | Tlc Handling Ltd | Transport cradle for a skid-supported helicoper |
US8607905B2 (en) * | 2011-05-13 | 2013-12-17 | Dan Johnson | Apparatus for moving wheeled loads |
-
2016
- 2016-08-08 CN CN201610643686.5A patent/CN106114897B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE202007006340U1 (en) * | 2006-09-28 | 2007-09-06 | Bünning, Thorsten | Universal tow bar for the helicopter Sea Lynx |
CN203684118U (en) * | 2013-12-04 | 2014-07-02 | 海丰通航科技有限公司 | Lifting platform for ascending and descending of helicopter |
CN205931304U (en) * | 2016-08-08 | 2017-02-08 | 青岛科技大学 | Skid formula helicopter intelligence promotes conveyer |
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CN106114897A (en) | 2016-11-16 |
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Effective date of registration: 20231114 Address after: 1337, 13th Floor, Building 2, No. 38 Kechuangwu Street, Beijing Economic and Technological Development Zone, Daxing District, Beijing, 100000 (Yizhuang Cluster, High end Industrial Zone, Beijing Pilot Free Trade Zone) Patentee after: Beifei Blueprint (Beijing) Aeronautical Engineering Technology Research Institute Co.,Ltd. Address before: 230000 floor 1, building 2, phase I, e-commerce Park, Jinggang Road, Shushan Economic Development Zone, Hefei City, Anhui Province Patentee before: Dragon totem Technology (Hefei) Co.,Ltd. Effective date of registration: 20231114 Address after: 230000 floor 1, building 2, phase I, e-commerce Park, Jinggang Road, Shushan Economic Development Zone, Hefei City, Anhui Province Patentee after: Dragon totem Technology (Hefei) Co.,Ltd. Address before: 266000 Qingdao University of Science & Technology, 99 Songling Road, Laoshan District, Qingdao, Shandong Patentee before: QINGDAO University OF SCIENCE AND TECHNOLOGY |
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Effective date of registration: 20240314 Address after: 335400 Fazhan Road, economic development zone, Guixi City, Yingtan City, Jiangxi Province intersects National Highway 320 (in Guixi science and Technology Innovation Center) Patentee after: Beifei blueprints Aviation Technology Co.,Ltd. Country or region after: China Address before: 1337, 13th Floor, Building 2, No. 38 Kechuangwu Street, Beijing Economic and Technological Development Zone, Daxing District, Beijing, 100000 (Yizhuang Cluster, High end Industrial Zone, Beijing Pilot Free Trade Zone) Patentee before: Beifei Blueprint (Beijing) Aeronautical Engineering Technology Research Institute Co.,Ltd. Country or region before: China |