CN117104521A - Emergency traction device for airplane - Google Patents
Emergency traction device for airplane Download PDFInfo
- Publication number
- CN117104521A CN117104521A CN202311078726.2A CN202311078726A CN117104521A CN 117104521 A CN117104521 A CN 117104521A CN 202311078726 A CN202311078726 A CN 202311078726A CN 117104521 A CN117104521 A CN 117104521A
- Authority
- CN
- China
- Prior art keywords
- arm
- frame
- lifting frame
- lower arm
- hole
- 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.)
- Pending
Links
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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
本发明涉及一种飞机应急牵引装置,其解决了应急情况下飞机地面移动作业保障问题的技术问题,其包括机架、上臂、上臂升降架、下臂、下臂升降架、液压千斤顶、挡臂,机架的底部连接有四个万向轮,机架中部左右两侧设有牵引挂钩,机架后部中间固定有液压千斤顶,机架前部设有挡臂,下臂升降架与液压千斤顶连接,下臂升降架和上臂升降架插接于机架的同一槽内,可在槽内上下移动,下臂升降架7与上臂升降架通过丝杆相连,可上下调节高度;下臂和上臂各有两件,分别插接于上臂升降架和下臂升降架的槽内,可以分别在槽内左右移动;挡臂与机架的前测连接。本发明结构简易、成本低、维护、使用方便,利用民航常见设备即可完成对飞机的牵引作业。
The invention relates to an aircraft emergency traction device, which solves the technical problem of ensuring aircraft ground movement operations in emergency situations. It includes a frame, an upper arm, an upper arm lifting frame, a lower arm, a lower arm lifting frame, a hydraulic jack, and a blocking arm. , there are four universal wheels connected to the bottom of the frame, there are traction hooks on the left and right sides of the middle of the frame, a hydraulic jack is fixed in the middle of the rear of the frame, there is a blocking arm in the front of the frame, a lower arm lifting frame and a hydraulic jack connection, the lower arm lifting frame and the upper arm lifting frame are plugged into the same slot of the frame and can move up and down in the slot. The lower arm lifting frame 7 is connected to the upper arm lifting frame through a screw rod, and the height of the lower arm and the upper arm can be adjusted up and down; There are two pieces each, which are plugged into the slots of the upper arm lifting frame and the lower arm lifting frame respectively, and can move left and right in the slot respectively; the front-end connection between the blocking arm and the frame. The invention has simple structure, low cost, easy maintenance and use, and can complete the towing operation of the aircraft by using common equipment in civil aviation.
Description
技术领域Technical field
本发明涉及飞机地面勤务保障技术领域,具体而言,涉及一种飞机应急牵引装置。The invention relates to the technical field of aircraft ground service support, and specifically to an aircraft emergency traction device.
背景技术Background technique
在机场专用设备技术领域,各种飞机在地面移动时,经常需要采用牵引车对其进行拖拉或顶推等操作,为此需要在牵引车与飞机之间配置牵引装置。现有牵引装置分为拖杆式和抱夹式两种,拖杆式是飞机牵引车与拖杆分离,拖杆与牵引车辆为两个分开的独立设备,拖杆一端与飞机连接,一端与牵引车连接,实现飞机的拖拉或顶推作业。抱夹式是飞机牵引车与抱夹装置集成在一起,为一个独立设备,称为无杆牵引车。无杆牵引车在取消了拖杆的前提下,运用抱夹装置将飞机的前轮托起并夹住,进行拖曳,实现飞机的拖拉或顶推作业。In the field of airport special equipment technology, when various aircraft move on the ground, they often need to be dragged or pushed by tractors. For this purpose, a traction device needs to be configured between the tractor and the aircraft. Existing towing devices are divided into tow bar type and clamp type. The tow bar type separates the aircraft tractor from the tow bar. The tow bar and the towing vehicle are two separate independent devices. One end of the tow bar is connected to the aircraft, and the other end is connected to the aircraft. The tractor is connected to realize the towing or pushing operation of the aircraft. The clamp-on tractor is an aircraft tractor integrated with the clamp-on device and is an independent device, called a rodless tractor. On the premise that the tow bar is eliminated, the rodless tractor uses a clamping device to lift and clamp the front wheel of the aircraft for towing, thereby completing the towing or pushing operation of the aircraft.
然而,现有技术在实际使用时发现,现有民航常见飞机的牵引装置与很多机型(如私人公务机、直升飞机、战机等)不能通用,不能满足战时民用机场对战机的应急保障,只能配备专用的牵引车,但是专用设备用作应急设备储备时,存在采购成本高昂,后期维护费用高,设备管理不便等问题,且使用频率低,造成资源浪费。However, when the existing technology is actually used, it is found that the towing devices of existing common aircraft in civil aviation cannot be used universally with many types of aircraft (such as private business jets, helicopters, fighter planes, etc.), and cannot meet the emergency support of civilian airports for fighter aircraft in wartime. , can only be equipped with special tractors, but when special equipment is used as emergency equipment reserve, there are problems such as high procurement costs, high subsequent maintenance costs, inconvenient equipment management, etc., and the frequency of use is low, resulting in a waste of resources.
发明内容Contents of the invention
本发明就是要解决上述技术问题,提供一种通用性强的飞机应急牵引装置。The present invention is to solve the above technical problems and provide an aircraft emergency traction device with strong versatility.
本发明提供的飞机应急牵引装置,包括机架、上臂升降架、下臂升降架、上臂、下臂、液压千斤顶、棘轮扳手和挡臂;The aircraft emergency traction device provided by the invention includes a frame, an upper arm lifting frame, a lower arm lifting frame, an upper arm, a lower arm, a hydraulic jack, a ratchet wrench and a blocking arm;
机架整体为U型结构,其底部连接有四个万向轮,中部左右两侧设有牵引挂钩,后部两侧设有两个并排布置的立柱,后部中间为开缺结构,立柱的侧面设有T型槽;机架的后侧设有扶手;The overall frame is a U-shaped structure, with four universal wheels connected to the bottom, traction hooks on the left and right sides of the middle, two columns arranged side by side on both sides of the rear, and an open structure in the middle of the rear. There are T-shaped slots on the side; there are handrails on the back of the rack;
挡臂与机架的前侧连接,挡臂可以打开和关闭;The blocking arm is connected to the front side of the frame, and the blocking arm can be opened and closed;
下臂升降架整体为倒T型结构,其底部的前侧面设有横向T型槽,后部中间设有立板盒,下臂升降架的后侧面两侧设有两个对称的T型连接块,立板盒的前侧设有耳板,耳板设有丝杆支撑孔,下臂升降架底部的上平面的中部设有丝杆支撑盲孔,丝杆支撑盲孔的两侧均设有若干个等间距锁销孔;下臂升降架的两个T型连接块分别插接于机架后部两个立柱的T型槽中;The lower arm lifting frame has an inverted T-shaped structure as a whole, with a transverse T-shaped slot on the front side of the bottom, a vertical plate box in the middle of the rear, and two symmetrical T-shaped connections on both sides of the rear side of the lower arm lifting frame. block, the front side of the vertical plate box is provided with an ear plate, the ear plate is provided with a screw rod support hole, the middle part of the upper plane at the bottom of the lower arm lifting frame is provided with a screw rod support blind hole, and both sides of the screw rod support blind hole are provided with There are several equally spaced locking pin holes; the two T-shaped connecting blocks of the lower arm lifting frame are respectively inserted into the T-shaped slots of the two columns at the rear of the frame;
下臂为L型方管结构,其前部的横截面为梯形,后部设有T型连接块,下臂的T型连接块顶面的中部开有锁销盲孔,下臂的T型连接块侧面的中部设有螺纹孔;两个下臂的T型连接块分别插接于下臂升降架的横向T型槽内,两个下臂左右对称布置;两个下臂上的螺纹孔的旋向相反,两个螺纹孔之间通过双头丝杆相连;棘轮扳手与双头丝杆的端部相连;可以用锁销穿过下臂升降架的锁销孔后插入下臂的锁销盲孔中,实现下臂的固定;The lower arm is an L-shaped square tube structure, with a trapezoidal cross-section at the front and a T-shaped connecting block at the rear. There is a locking blind hole in the middle of the top surface of the T-shaped connecting block of the lower arm. The T-shaped lower arm There is a threaded hole in the middle of the side of the connecting block; the T-shaped connecting blocks of the two lower arms are respectively inserted into the transverse T-shaped slots of the lower arm lifting frame, and the two lower arms are symmetrically arranged left and right; the threaded holes on the two lower arms The direction of rotation is opposite, and the two threaded holes are connected through a double-headed screw; the ratchet wrench is connected to the end of the double-headed screw; a locking pin can be passed through the locking pin hole of the lower arm lifting frame and then inserted into the lock of the lower arm. Pin in the blind hole to fix the lower arm;
上臂升降架的前侧面设有T型槽,后侧面设于两个对称布置的T型连接块,顶面设有若干个等间距锁止孔,上臂升降架顶面的中部设有梯形螺纹套,若干个锁止孔位于梯形螺纹套的两侧;上臂升降架的两个T型连接块分别插接于机架后部两个立柱的T型槽中;The front side of the upper arm lifting frame is provided with a T-shaped slot, the rear side is provided with two symmetrically arranged T-shaped connecting blocks, the top surface is provided with a number of equally spaced locking holes, and the middle part of the top surface of the upper arm lifting frame is provided with a trapezoidal thread sleeve , several locking holes are located on both sides of the trapezoidal thread sleeve; the two T-shaped connecting blocks of the upper arm lifting frame are respectively inserted into the T-shaped slots of the two columns at the rear of the frame;
上臂为方管结构,其前部的横截面为梯形,后部设有T型连接块,上臂的T型连接块顶面的中部开有锁销孔;两个上臂的T型连接块分别插接于上臂升降架的T型槽内;可以用锁销穿过上臂升降架的锁止孔后插入上臂的锁销孔中,实现上臂的固定;The upper arm has a square tube structure, with a trapezoidal cross-section at the front and a T-shaped connecting block at the rear. There is a lock pin hole in the middle of the top surface of the T-shaped connecting block of the upper arm; the T-shaped connecting blocks of the two upper arms are inserted into each other respectively. Connected to the T-shaped slot of the upper arm lifting frame; the locking pin can be passed through the locking hole of the upper arm lifting frame and then inserted into the locking pin hole of the upper arm to secure the upper arm;
上臂升降架和下臂升降架通过丝杆连接在一起,丝杆的上部设有梯形螺纹,梯形螺纹与上臂支架的梯形螺纹套相连,丝杆的下部插接于下臂支架的耳板的丝杆支撑孔内;丝杆的顶部连接有手柄;丝杆上部的梯形螺纹连接有锁紧螺母,锁紧螺母的四周设有环形操作把手;The upper arm lifting frame and the lower arm lifting frame are connected together through a screw rod. The upper part of the screw rod is provided with a trapezoidal thread. The trapezoidal thread is connected to the trapezoidal thread sleeve of the upper arm bracket. The lower part of the screw rod is plugged into the wire of the ear plate of the lower arm bracket. In the rod support hole; the top of the screw rod is connected with a handle; the trapezoidal thread on the upper part of the screw rod is connected with a locking nut, and an annular operating handle is provided around the locking nut;
液压千斤顶固定连接在机架后部中间开缺处,液压千斤顶的输出端与下臂升降架的立板盒连接。The hydraulic jack is fixedly connected to the middle opening at the rear of the frame, and the output end of the hydraulic jack is connected to the vertical plate box of the lower arm lifting frame.
优选地,丝杆设有挡圈槽,丝杆的挡圈槽了有挡圈,挡圈靠近耳板的丝杆支撑孔。Preferably, the screw rod is provided with a retaining ring groove, the retaining ring of the screw rod is provided with a retaining ring, and the retaining ring is close to the screw rod support hole of the lug plate.
优选地,机架的前侧设有挡臂铰接耳座和挡臂锁止耳座;挡臂的右端设有铰接孔,左端设有长条孔,挡臂的左端还设有操作把手,挡臂右端的铰接孔与机架前部的挡臂铰接耳座铰接;挡臂左端的长条孔可与机架前部的挡臂锁止耳座配合,用销钉穿过挡臂锁止耳座并插入挡臂左端的长条孔中,实现挡臂的关闭。Preferably, the front side of the frame is provided with a hinged ear seat and a locking ear seat of the arm; the right end of the arm is provided with a hinge hole, the left end is provided with a long hole, and the left end of the arm is also provided with an operating handle. The hinge hole at the right end of the arm is hinged with the arm hinge ear seat at the front of the frame; the long hole at the left end of the arm can be matched with the arm locking ear seat at the front of the rack, and a pin is passed through the arm locking ear seat. And insert it into the long hole on the left end of the blocking arm to close the blocking arm.
本发明的有益效果是:结构简易、成本低、维护、管理方便,使用方便,使用过程可靠性高、稳定性好,利用民航常见设备即可完成对飞机的牵引作业,实现应急情况下的飞机保障。本发明可以适用于不同尺寸大小的飞机鼻轮,即适应不同种类、型号的飞机,具有很好的通用性。The invention has the following beneficial effects: simple structure, low cost, convenient maintenance and management, convenient use, high reliability and good stability in the use process. The towing operation of the aircraft can be completed by using common civil aviation equipment, and the aircraft can be towed in emergency situations. Assure. The invention can be applied to aircraft nose wheels of different sizes, that is, it is suitable for different types and models of aircraft, and has good versatility.
本发明进一步的特征和方面,将在以下参考附图的具体实施方式的描述中,得以清楚地记载。Further features and aspects of the invention will become apparent from the following description of specific embodiments with reference to the accompanying drawings.
附图说明Description of drawings
图1是本发明的结构立体图;Figure 1 is a structural perspective view of the present invention;
图2是本发明的爆炸结构立体图;Figure 2 is a perspective view of the explosive structure of the present invention;
图3是本发明的上臂升降架立体图;Figure 3 is a perspective view of the upper arm lifting frame of the present invention;
图4是本发明的下臂升降架立体图;Figure 4 is a perspective view of the lower arm lifting frame of the present invention;
图5是本发明的上臂立体图;Figure 5 is a perspective view of the upper arm of the present invention;
图6是本发明的下臂立体图;Figure 6 is a perspective view of the lower arm of the present invention;
图7是本发明的锁紧螺母立体图;Figure 7 is a perspective view of the lock nut of the present invention;
图8是本发明的机架立体图。Figure 8 is a perspective view of the frame of the present invention.
图中符号说明:Explanation of symbols in the figure:
1.机架,1-1.扶手,1-2.立柱,1-2-1.T型槽,1-3.挡臂铰接耳座,1-4.挡臂锁止耳座;2、上臂,2-1.T型连接块,2-1-1.锁销孔;3、下臂,3-1.T型连接块,3-1-1.锁销盲孔,3-1-2.螺纹孔;4、上臂升降架,4-1.T型槽,4-2.T型连接块,4-3.锁止孔,4-4.梯形螺纹套;5、丝杆;6、锁紧螺母;7、下臂升降架,7-1.横向T型槽,7-2.T型连接块,7-3.立板盒,7-3-1.耳板,7-4.丝杆支撑盲孔;8、万向轮;9、牵引挂钩;10、棘轮扳手;11、锁销;12、双头丝杆;13、液压千斤顶;14、手柄;15、挡圈;16、挡臂,16-1.操作把手。1. Frame, 1-1. Handrail, 1-2. Column, 1-2-1. T-shaped slot, 1-3. Arm hinge ear seat, 1-4. Arm locking ear seat; 2. Upper arm, 2-1. T-shaped connecting block, 2-1-1. Lock pin hole; 3. Lower arm, 3-1. T-shaped connecting block, 3-1-1. Lock pin blind hole, 3-1- 2. Threaded hole; 4. Upper arm lifting frame, 4-1. T-shaped slot, 4-2. T-shaped connecting block, 4-3. Locking hole, 4-4. Trapezoidal thread sleeve; 5. Screw rod; 6 , locking nut; 7. Lower arm lifting frame, 7-1. Transverse T-shaped slot, 7-2. T-shaped connecting block, 7-3. Vertical plate box, 7-3-1. Ear plate, 7-4 .Screw support blind hole; 8. Universal wheel; 9. Traction hook; 10. Ratchet wrench; 11. Lock pin; 12. Double-headed screw; 13. Hydraulic jack; 14. Handle; 15. Back-up ring; 16 , blocking arm, 16-1. Operating handle.
具体实施方式Detailed ways
以下参照附图,以具体实施例对本发明作进一步详细说明。The present invention will be further described in detail with specific embodiments below with reference to the accompanying drawings.
如图1、图2所示,一种飞机应急牵引装置,包括机架1、上臂2、上臂升降架4、下臂3、下臂升降架7、液压千斤顶13、挡臂16,机架1是飞机应急牵引装置的基体框架,机架1的底部连接有四个万向轮8,机架1中部左右两侧设有牵引挂钩9,机架1后部中间固定有液压千斤顶13,机架1前部设有挡臂16。下臂升降架7与液压千斤顶13连接,下臂升降架7和上臂升降架4插接于机架1的同一槽内,可在槽内上下移动,下臂升降架7与上臂升降架4通过丝杆5相连,可上下调节高度;下臂3和上臂2各有两件,分别插接于上臂升降架4和下臂升降架7的槽内,可以分别在槽内左右移动;挡臂16与机架耳座铰接,可绕铰接轴旋转。As shown in Figures 1 and 2, an aircraft emergency traction device includes a frame 1, an upper arm 2, an upper arm lifting frame 4, a lower arm 3, a lower arm lifting frame 7, a hydraulic jack 13, and a blocking arm 16. The frame 1 It is the base frame of the aircraft emergency traction device. Four universal wheels 8 are connected to the bottom of the frame 1. Towing hooks 9 are provided on the left and right sides of the middle part of the frame 1. A hydraulic jack 13 is fixed in the middle of the rear part of the frame 1. The frame 1. The front part is provided with a blocking arm 16. The lower arm lifting frame 7 is connected to the hydraulic jack 13. The lower arm lifting frame 7 and the upper arm lifting frame 4 are plugged into the same slot of the frame 1 and can move up and down in the slot. The lower arm lifting frame 7 and the upper arm lifting frame 4 pass through The screw rod 5 is connected and can adjust the height up and down; the lower arm 3 and the upper arm 2 each have two pieces, which are plugged into the slots of the upper arm lifting frame 4 and the lower arm lifting frame 7 respectively, and can move left and right in the slot respectively; the blocking arm 16 It is hinged with the frame ear seat and can rotate around the hinge axis.
如图8所示,机架1整体为U型结构,其后部两侧设有两个并排布置的立柱1-2,其后部中间为开缺结构,立柱1-2的侧面开有T型槽1-2-1,机架1的左右两侧设有牵引挂钩9,机架1的后侧设有扶手1-1,机架1的前侧设有挡臂铰接耳座1-3和挡臂锁止耳座1-4。As shown in Figure 8, the rack 1 has a U-shaped structure as a whole. There are two columns 1-2 arranged side by side on both sides of the rear. The middle of the rear is an open structure, and there are T's on the sides of the columns 1-2. groove 1-2-1, the left and right sides of the frame 1 are provided with traction hooks 9, the rear side of the frame 1 is provided with handrails 1-1, and the front side of the frame 1 is provided with arm hinge ear seats 1-3 and arm locking lugs 1-4.
如图4所示,下臂升降架7整体为倒T型结构,其底部的前侧面设有横向T型槽7-1,后侧面两侧设有两个对称的T型连接块7-2,后部中间设有用于与液压千斤顶13连接的立板盒7-3,立板盒7-3的前侧设有耳板7-3-1,耳板7-3-1设有丝杆支撑孔,下臂升降架7底部的上平面的中部设有丝杆支撑盲孔7-4,丝杆支撑盲孔7-4的两侧均设有若干个等间距锁销孔7-5。下臂升降架7的两个T型连接块7-2分别插接于机架1后部两个立柱1-2的T型槽1-2-1中。As shown in Figure 4, the lower arm lifting frame 7 is an inverted T-shaped structure as a whole, with a transverse T-shaped slot 7-1 on the front side of the bottom, and two symmetrical T-shaped connecting blocks 7-2 on both sides of the rear side. , there is a vertical plate box 7-3 for connecting with the hydraulic jack 13 in the middle of the rear part. The front side of the vertical plate box 7-3 is provided with an ear plate 7-3-1, and the ear plate 7-3-1 is provided with a screw rod. Support hole, the middle part of the upper plane of the bottom of the lower arm lift frame 7 is provided with a screw support blind hole 7-4, and both sides of the screw support blind hole 7-4 are provided with a number of equally spaced lock pin holes 7-5. The two T-shaped connecting blocks 7-2 of the lower arm lifting frame 7 are respectively inserted into the T-shaped slots 1-2-1 of the two uprights 1-2 at the rear of the frame 1.
如图6所示,下臂3为L型方管结构,其前部的横截面为梯形,后部设有T型连接块3-1,T型连接块3-1的顶面的中部开有锁销盲孔3-1-1,T型连接块3-1的侧面的中部设有螺纹孔3-1-2。如图1、图2所示,下臂3的数量是两个,两个下臂3的T型连接块3-1分别插接于下臂升降架7的横向T型槽7-1内,实现两个下臂3与下臂升降架7滑动连接,两个下臂3左右对称布置。两个下臂3上的螺纹孔的旋向相反,其中一个下臂3中T型连接块3-1侧面中部的螺纹孔3-1-2是左旋,另一个下臂3中T型连接块侧面中部的螺纹孔是右旋。两个螺纹孔3-1-2之间通过双头丝杆12相连,双头丝杆12的一端螺纹是左旋,另一端螺纹是右旋,双头丝杆12的一端与其中一个下臂3上的螺纹孔连接配合,双头丝杆12的另一端与第二个下臂3上的螺纹孔连接配合。As shown in Figure 6, the lower arm 3 is an L-shaped square tube structure with a trapezoidal cross-section at the front and a T-shaped connecting block 3-1 at the rear. The top surface of the T-shaped connecting block 3-1 is open in the middle. There is a locking pin blind hole 3-1-1, and a threaded hole 3-1-2 is provided in the middle of the side of the T-shaped connecting block 3-1. As shown in Figures 1 and 2, the number of lower arms 3 is two. The T-shaped connecting blocks 3-1 of the two lower arms 3 are respectively inserted into the transverse T-shaped slots 7-1 of the lower arm lifting frame 7. The two lower arms 3 are slidingly connected to the lower arm lifting frame 7, and the two lower arms 3 are arranged symmetrically left and right. The threaded holes on the two lower arms 3 have opposite directions of rotation. The threaded hole 3-1-2 in the middle of the side of the T-shaped connecting block 3-1 in one of the lower arms 3 is left-handed, and the T-shaped connecting block in the other lower arm 3 has a left-hand direction. The threaded hole in the middle of the side is right-hand. The two threaded holes 3-1-2 are connected through a double-headed screw 12. One end of the double-headed screw 12 has a left-hand thread and the other end has a right-hand thread. One end of the double-headed screw 12 is connected to one of the lower arms 3 The threaded hole on the second lower arm 3 is connected and matched, and the other end of the double-head screw rod 12 is connected and matched with the threaded hole on the second lower arm 3.
如图1和2所示,双头丝杆12一端的端部设有六方形轴头,棘轮扳手10与六方形轴头相连,通过外力操作棘轮扳手10进而带动双头丝杆12转动,从而使两个下臂3移动,实现两个下臂3之间距离的调节。当下臂3的位置调节好后,用锁销穿过锁销孔7-5后插入锁销盲孔3-1-1中,实现下臂3的固定、定位,防止下臂3左右移动As shown in Figures 1 and 2, one end of the double-head screw rod 12 is provided with a hexagonal shaft head. The ratchet wrench 10 is connected to the hexagonal shaft head. The ratchet wrench 10 is operated by external force to drive the double-head screw rod 12 to rotate. The two lower arms 3 are moved to adjust the distance between the two lower arms 3 . After adjusting the position of the lower arm 3, use the lock pin to pass through the lock pin hole 7-5 and then insert it into the lock pin blind hole 3-1-1 to achieve the fixation and positioning of the lower arm 3 and prevent the lower arm 3 from moving left and right.
如图3所示,上臂升降架4的前侧面设有T型槽4-1,后侧面设于两个对称布置的T型连接块4-2,上臂升降架4的顶面开有等间距锁止孔4-3,上臂升降架4顶面的中部设有梯形螺纹套4-4。若干个锁止孔4-3位于梯形螺纹套4-4的两侧。如图1和2所示,上臂升降架4的两个T型连接块4-2分别插接于机架1后部两个立柱1-2的T型槽1-2-1中。As shown in Figure 3, the front side of the upper arm lifting frame 4 is provided with a T-shaped slot 4-1, and the rear side is provided with two symmetrically arranged T-shaped connecting blocks 4-2. The top surface of the upper arm lifting frame 4 is provided with equal intervals. The locking hole 4-3 is provided with a trapezoidal thread sleeve 4-4 in the middle of the top surface of the upper arm lifting frame 4. Several locking holes 4-3 are located on both sides of the trapezoidal thread sleeve 4-4. As shown in Figures 1 and 2, the two T-shaped connecting blocks 4-2 of the upper arm lifting frame 4 are respectively inserted into the T-shaped slots 1-2-1 of the two uprights 1-2 at the rear of the frame 1.
如图5所示,上臂2为方管结构,其前部的横截面为梯形,后部设有T型连接块2-1,T型连接块2-1的顶面的中部开有锁销孔2-1-1。如图1、图2所示,上臂2的数量是两个,为左右对称结构,两个上臂2的T型连接块2-1分别插接于上臂升降架4的T型槽4-1内,实现两个上臂2与上臂升降架4滑动连接。两个上臂2之间距离可调。当两个上臂2的左右距离调整好后,用锁销11穿过锁止孔4-3后插入锁销孔2-1-1中,实现上臂2的固定、定位,防止上臂2左右移动。As shown in Figure 5, the upper arm 2 is a square tube structure with a trapezoidal cross-section at the front and a T-shaped connecting block 2-1 at the rear. There is a locking pin in the middle of the top surface of the T-shaped connecting block 2-1. Hole 2-1-1. As shown in Figure 1 and Figure 2, the number of upper arms 2 is two, which is a left-right symmetrical structure. The T-shaped connecting blocks 2-1 of the two upper arms 2 are respectively inserted into the T-shaped slots 4-1 of the upper arm lifting frame 4. , realizing a sliding connection between the two upper arms 2 and the upper arm lifting frame 4. The distance between the two upper arms 2 is adjustable. After the left and right distance of the two upper arms 2 is adjusted, use the lock pin 11 to pass through the lock hole 4-3 and then insert into the lock pin hole 2-1-1 to achieve the fixation and positioning of the upper arm 2 and prevent the upper arm 2 from moving left and right.
如图1、图2所示,上臂升降架4和下臂升降架7通过丝杆5连接在一起,丝杆5的上部设有梯形螺纹,该梯形螺纹与上臂支架4的梯形螺纹套4-4相连,丝杆5的下部插接于下臂支架7的耳板7-3-1的丝杆支撑孔内。丝杆5设有挡圈槽,挡圈15卡在丝杆5的挡圈槽上,挡圈15靠近耳板7-3-1的丝杆支撑孔,挡圈15可以防止丝杆5脱离丝杆支撑孔。由于上臂2位于下臂3的上方,通过转动丝杆5可以调节上臂2和下臂3之间的在垂直方向上的间距和夹紧力。手柄14与丝杆5的顶部连接(具体可以在丝杆5的顶部设置用于和手柄14连接的方形柱体结构),工作人员操作手柄14就可以使丝杆5转动。As shown in Figures 1 and 2, the upper arm lifting frame 4 and the lower arm lifting frame 7 are connected together through the screw rod 5. The upper part of the screw rod 5 is provided with a trapezoidal thread, and the trapezoidal thread is connected with the trapezoidal thread sleeve 4- of the upper arm bracket 4. 4 are connected, and the lower part of the screw rod 5 is inserted into the screw rod support hole of the ear plate 7-3-1 of the lower arm bracket 7. The screw rod 5 is provided with a retaining ring groove. The retaining ring 15 is stuck on the retaining ring groove of the screw rod 5. The retaining ring 15 is close to the screw support hole of the lug plate 7-3-1. The retaining ring 15 can prevent the screw rod 5 from being separated from the thread. Rod support hole. Since the upper arm 2 is located above the lower arm 3, the vertical distance and clamping force between the upper arm 2 and the lower arm 3 can be adjusted by rotating the screw rod 5. The handle 14 is connected to the top of the screw rod 5 (specifically, a square cylindrical structure for connecting with the handle 14 can be provided on the top of the screw rod 5), and the staff can rotate the screw rod 5 by operating the handle 14.
如图1、图2、图7所示,锁紧螺母6与丝杆5上部的梯形螺纹连接配合,锁紧螺母6四周通过焊接的方式连接有环形操作把手。当通过外力拧紧锁紧螺母6后,能够防止轮胎压紧后丝杆松动脱落。As shown in Figures 1, 2, and 7, the locking nut 6 is connected and matched with the trapezoidal thread on the upper part of the screw rod 5, and an annular operating handle is connected around the locking nut 6 by welding. When the locking nut 6 is tightened by external force, it can prevent the screw rod from loosening and falling off after the tire is tightened.
如图1、图2所示,挡臂16为长条杆结构,其右端设有铰接孔,左端设有长条孔,左端还设有操作把手16-1。挡臂16右端的铰接孔与机架前部的挡臂铰接耳座1-3铰接。挡臂16左端的长条孔可与机架前部的挡臂锁止耳座1-4配合,用销钉穿过挡臂锁止耳座1-4并插入挡臂16左端的长条孔中,实现挡臂的关闭。当需要打开挡臂16时,拔出销钉,用手拉操作把手16-1即可。通过快插销的方式实现快速锁止。As shown in Figures 1 and 2, the blocking arm 16 is a long rod structure with a hinge hole at its right end, a long hole at its left end, and an operating handle 16-1 at its left end. The hinge hole at the right end of the blocking arm 16 is hinged with the hinged ear seat 1-3 of the blocking arm at the front of the frame. The long hole on the left end of the blocking arm 16 can be matched with the blocking arm locking ear seat 1-4 on the front of the frame. Use a pin to pass through the blocking arm locking ear seat 1-4 and insert it into the long hole on the left end of the blocking arm 16. , to achieve the closing of the blocking arm. When it is necessary to open the blocking arm 16, pull out the pin and pull the operating handle 16-1. Quick locking is achieved by means of quick latch.
如图1和2所示,液压千斤顶13固定安装在机架1后部中间开缺处,液压千斤顶13的输出端与下臂升降架7的立板盒7-3连接。As shown in Figures 1 and 2, the hydraulic jack 13 is fixedly installed at the middle opening at the rear of the frame 1, and the output end of the hydraulic jack 13 is connected to the vertical plate box 7-3 of the lower arm lifting frame 7.
本发明使用时,参考图1,将下臂3降到最低位置,将上臂、下臂距离调节到合适的位置,打开挡臂16,从飞机鼻轮侧面推入,关闭挡臂16,摇动手柄14使上臂、下臂夹紧轮胎,拧紧锁紧螺母6固定丝杆5,操作液压千斤顶13升降带动上臂、下臂升降,从而实现飞机鼻轮的升降,然后通过飞机牵引车带动拖杆与机架一侧的牵引挂钩9相连实现飞机的牵引移动。可见,本发明结构简易、成本低、维护、管理方便,使用方便,使用过程可靠性高、稳定性好,利用民航常见设备即可完成对飞机的牵引作业,实现应急情况下的飞机保障。When using the present invention, refer to Figure 1, lower the lower arm 3 to the lowest position, adjust the distance between the upper arm and the lower arm to a suitable position, open the blocking arm 16, push in from the side of the nose wheel of the aircraft, close the blocking arm 16, and shake the handle 14. Make the upper arm and lower arm clamp the tire, tighten the locking nut 6 to fix the screw rod 5, operate the hydraulic jack 13 to lift and lower the upper arm and lower arm, thereby realizing the lifting and lowering of the aircraft nose wheel, and then drive the tow bar and the aircraft tractor through the aircraft tractor. The traction hook 9 on one side of the frame is connected to realize the traction movement of the aircraft. It can be seen that the present invention has a simple structure, low cost, convenient maintenance and management, is easy to use, has high reliability and good stability in the use process. It can complete the towing operation of the aircraft by using common civil aviation equipment, and realize the aircraft support in emergency situations.
通过调整两个下臂左右方向上的间距,调整两个上臂左右方向上的间距,可以适用于不同尺寸大小的飞机鼻轮,即适应不同种类、型号的飞机,具有很好的通用性。By adjusting the distance between the two lower arms in the left and right directions, and adjusting the distance between the two upper arms in the left and right directions, it can be applied to aircraft nose wheels of different sizes, that is, it can be adapted to different types and models of aircraft, and has good versatility.
以上所述仅对本发明的优选实施例而已,并不用于限制本发明,对于本领域的技术人员来说,本发明可以有各种更改和变化。凡是在本发明的权利要求限定范围内,所做的任何修改、等同替换、改进等,均应在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention and are not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and changes. Any modifications, equivalent substitutions, improvements, etc. made within the scope of the claims of the present invention shall be within the protection scope of the present invention.
Claims (3)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311078726.2A CN117104521A (en) | 2023-08-25 | 2023-08-25 | Emergency traction device for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311078726.2A CN117104521A (en) | 2023-08-25 | 2023-08-25 | Emergency traction device for airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN117104521A true CN117104521A (en) | 2023-11-24 |
Family
ID=88799649
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202311078726.2A Pending CN117104521A (en) | 2023-08-25 | 2023-08-25 | Emergency traction device for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN117104521A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5054714A (en) * | 1989-04-28 | 1991-10-08 | Man Gutehoffnungshutte Aktiengesellschaft | Aircraft tractor without tow-bar with adjustable tow arms |
| US20030165375A1 (en) * | 2000-06-26 | 2003-09-04 | Magnus Johansson | Traction vehicle for aircraft and engagement and hoisting device therefor |
| CN102211539A (en) * | 2010-06-25 | 2011-10-12 | 叶伟兵 | Mini road dragging wrecker |
| CN202935585U (en) * | 2012-12-02 | 2013-05-15 | 威海广泰空港设备股份有限公司 | Clamping device of airplane nosewheel |
| CN111703585A (en) * | 2020-06-23 | 2020-09-25 | 南京航空航天大学 | Self-adjusting wheel clamping device for stickless aircraft tractor |
| CN112829962A (en) * | 2021-01-12 | 2021-05-25 | 宝鸡赫威特机械科技有限公司 | Wheel holding mechanism for aircraft tractor |
| CN113247293A (en) * | 2021-06-28 | 2021-08-13 | 中国船舶重工集团公司第七一三研究所 | Rodless aircraft tractor of side direction centre gripping |
-
2023
- 2023-08-25 CN CN202311078726.2A patent/CN117104521A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5054714A (en) * | 1989-04-28 | 1991-10-08 | Man Gutehoffnungshutte Aktiengesellschaft | Aircraft tractor without tow-bar with adjustable tow arms |
| US20030165375A1 (en) * | 2000-06-26 | 2003-09-04 | Magnus Johansson | Traction vehicle for aircraft and engagement and hoisting device therefor |
| CN102211539A (en) * | 2010-06-25 | 2011-10-12 | 叶伟兵 | Mini road dragging wrecker |
| CN202935585U (en) * | 2012-12-02 | 2013-05-15 | 威海广泰空港设备股份有限公司 | Clamping device of airplane nosewheel |
| CN111703585A (en) * | 2020-06-23 | 2020-09-25 | 南京航空航天大学 | Self-adjusting wheel clamping device for stickless aircraft tractor |
| CN112829962A (en) * | 2021-01-12 | 2021-05-25 | 宝鸡赫威特机械科技有限公司 | Wheel holding mechanism for aircraft tractor |
| CN113247293A (en) * | 2021-06-28 | 2021-08-13 | 中国船舶重工集团公司第七一三研究所 | Rodless aircraft tractor of side direction centre gripping |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9441382B2 (en) | Adjustable aircraft maintenance platform for improving efficiency and safety of aircraft maintenance operations | |
| CN209193464U (en) | A kind of aircraft main landing gear disassembly-assembly bracket device | |
| WO2020177160A1 (en) | Retractable train platform stepping board apparatus | |
| CN117104521A (en) | Emergency traction device for airplane | |
| AU2013101706A4 (en) | Tow hitch | |
| CN110104188B (en) | Emergency rescue device and method for aircraft wheel burst | |
| CN201729276U (en) | Ejection system of small-sized unmanned aircraft | |
| CN210102019U (en) | Ground trailer of helicopter and trailer assembly of helicopter | |
| CN114084367B (en) | Emergency rescue equipment for tire burst of airplane wheel, use method and application | |
| CN111890290B (en) | Door mechanism installation auxiliary device of EMUs stopper sliding door | |
| CN113566159A (en) | LED street lamp convenient to overhaul and having lifting function | |
| CN210284656U (en) | Traction device | |
| CN209351375U (en) | A kind of vehicle drawing unit | |
| CN211380578U (en) | A universal parking rack for multi-directional display of ejection seats | |
| CN111634438A (en) | General aircraft is with pulling external member | |
| CN216810322U (en) | Simple and easy erection joint reinforced structure of building steel construction | |
| CN103991462A (en) | Scissor type car arrester | |
| CN207955177U (en) | Auxiliary self-rescue device for wheeled vehicles | |
| CN210337656U (en) | Unlocking mechanism | |
| CN208650606U (en) | A kind of Double-layer parking space of ground bicycle position | |
| CN110859459A (en) | A universal parking rack for multi-directional display of an ejection seat and a method of using the same | |
| CN205997938U (en) | airport trolley handlebar | |
| CN215886291U (en) | High-altitude lifting platform tilting device | |
| CN219279444U (en) | Lifting device for municipal road well lid | |
| CN220764245U (en) | Consultation patrol car for property management |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |