CN204125013U - A kind of erecting by overhang - Google Patents

A kind of erecting by overhang Download PDF

Info

Publication number
CN204125013U
CN204125013U CN201420564567.7U CN201420564567U CN204125013U CN 204125013 U CN204125013 U CN 204125013U CN 201420564567 U CN201420564567 U CN 201420564567U CN 204125013 U CN204125013 U CN 204125013U
Authority
CN
China
Prior art keywords
hanging
suspension ring
crossbeam
connecting panel
poly
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.)
Expired - Lifetime
Application number
CN201420564567.7U
Other languages
Chinese (zh)
Inventor
路丽丽
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xian Aircraft Design and Research Institute of AVIC
Original Assignee
Xian Aircraft Design and Research Institute of AVIC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Xian Aircraft Design and Research Institute of AVIC filed Critical Xian Aircraft Design and Research Institute of AVIC
Priority to CN201420564567.7U priority Critical patent/CN204125013U/en
Application granted granted Critical
Publication of CN204125013U publication Critical patent/CN204125013U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Connection Of Plates (AREA)

Abstract

The utility model belongs to transporation by plane technical field, relates to a kind of erecting by overhang for transporation by plane docking.A kind of erecting by overhang, comprise a hanging crossbeam, suspension ring and poly-ester fibres band, it is characterized in that, two grooved parts (1), hanging board (2) and two pieces of connecting panels (3) are coupled together by bolt and form hanging crossbeam, two grooved part (1) dos-à-doss are placed, centre is added with hanging board (2) and connecting panel (3), hanging board (2) there is hanging hole (7), connecting panel (3) is positioned at hanging crossbeam two ends, respectively there are two suspension ring stringed together (4) at hanging crossbeam two ends, suspension ring (4) one end hangs on connecting panel (3), the other end hangs with set square (5), the two ends of poly-ester fibres band (6) are fixed on the groove on set square (5).The utility model is simple and easy to combination, can regulate length by demand, and docking installed by the aircraft components being applicable to different size, also can be used for short range transport.

Description

A kind of erecting by overhang
Technical field
The utility model belongs to transporation by plane technical field, relates to a kind of erecting by overhang for transporation by plane docking.
Background technology
When transporation by plane, because each segment body of fuselage is long-pending large, mobile difficulty, not easily dock, cause transporation by plane to be wasted time and energy, also easily collide with airplane component.
Summary of the invention
The purpose of this utility model is to provide a kind of erecting by overhang of transporation by plane, to ensure the simple and safe of transporation by plane.Can not be worn and torn aircraft configuration and enamelled coating, need not design the sling point being specifically designed to assembling aboard.
The utility model comprises hanging crossbeam, suspension ring and a poly-ester fibres band, two grooved parts 1, hanging board 2 and two pieces of connecting panels 3 are coupled together by bolt and form hanging crossbeam, two grooved part 1 dos-à-doss are placed, centre is added with hanging board 2 and connecting panel 3, hanging board 2 has hanging hole 7, connecting panel 3 is positioned at hanging crossbeam two ends.Respectively there are two suspension ring stringed together 4 at hanging crossbeam two ends, and suspension ring 4 one end hangs on connecting panel 3, and the other end hangs with set square 5, and the two ends of poly-ester fibres band 6 are fixed on the groove on set square 5.
The utility model hanging adopts poly-ester fibres band, can not cause damage, can not cause scratch of colliding with to the aircraft skin sprayed paint during lifting aircraft to aircraft skin profile; Two hanging with the use of, for large aircraft components assembling docking safe and reliable, save time, save manpower, reduce costs; Hanging is simple and easy to combination, can regulate length by demand, and docking installed by the aircraft components being applicable to different size, also can be used for short range transport.
Accompanying drawing explanation
Accompanying drawing 1 is schematic diagram of the present invention;
Accompanying drawing 2 is suspension ring 4 of the present invention and connecting panel 3 connection diagram.
Detailed description of the invention
The utility model is made up of hanging crossbeam, 4 suspension ring and a poly-ester fibres band.Two grooved parts 1, hanging board 2 and two pieces of connecting panels 3 are coupled together by bolt and form hanging crossbeam, two grooved part 1 dos-à-doss are placed, and centre is added with hanging board 2 and connecting panel 3, and hanging board 2 is positioned in the middle of hanging crossbeam, hanging board 2 has hanging hole 7, connecting panel 3 is positioned at hanging crossbeam two ends.Respectively there are two suspension ring stringed together 4 at hanging crossbeam two ends, and suspension ring 4 one end hangs on connecting panel 3, and the other end hangs with set square 5, and poly-ester fibres band 6 is through the groove on set square 5, and poly-ester fibres band 6 is coupled together with hanging crossbeam by set square 5 and suspension ring 4.Connect suspension ring 4 bolt 8 safety locking of set square 5, unthread bolts 8, can take off poly-ester fibres band 6, during use, can choose the poly-ester fibres band 6 of different size by demand.
Hanging can regulate length by demand, unthread bolts 8, just can pull down poly-ester fibres band, the poly-ester fibres band of a configurable multiple size of hanging crossbeam, and docking installed by the aircraft components being applicable to different size.If two hangings are with the use of, the large long body parts safety and reliability of lifting diameter.

Claims (1)

1. an erecting by overhang, comprise a hanging crossbeam, suspension ring and poly-ester fibres band, it is characterized in that, two grooved parts (1), hanging board (2) and two pieces of connecting panels (3) are coupled together by bolt and form hanging crossbeam, two grooved part (1) dos-à-doss are placed, centre is added with hanging board (2) and connecting panel (3), hanging board (2) there is hanging hole (7), connecting panel (3) is positioned at hanging crossbeam two ends, respectively there are two suspension ring stringed together (4) at hanging crossbeam two ends, suspension ring (4) one end hangs on connecting panel (3), the other end hangs with set square (5), the two ends of poly-ester fibres band (6) are fixed on the groove on set square (5).
CN201420564567.7U 2014-09-28 2014-09-28 A kind of erecting by overhang Expired - Lifetime CN204125013U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420564567.7U CN204125013U (en) 2014-09-28 2014-09-28 A kind of erecting by overhang

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420564567.7U CN204125013U (en) 2014-09-28 2014-09-28 A kind of erecting by overhang

Publications (1)

Publication Number Publication Date
CN204125013U true CN204125013U (en) 2015-01-28

Family

ID=52381388

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420564567.7U Expired - Lifetime CN204125013U (en) 2014-09-28 2014-09-28 A kind of erecting by overhang

Country Status (1)

Country Link
CN (1) CN204125013U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106429797A (en) * 2016-12-15 2017-02-22 南通华夏飞机工程技术股份有限公司 Vertical-fin hanger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106429797A (en) * 2016-12-15 2017-02-22 南通华夏飞机工程技术股份有限公司 Vertical-fin hanger

Similar Documents

Publication Publication Date Title
CN204355957U (en) A kind of novel pipeline anchor ear lifting connection structure
CN204057233U (en) Vacuum drop formula transport pipeline
CN204125013U (en) A kind of erecting by overhang
CN202431695U (en) Safe lifting-ring bolt
CN104340843A (en) Reactor core hoisting tool
CN104527966A (en) Split empennage for fixed wing airplane model
CN103332624A (en) Pulley for high-altitude line or pipe diameter, and mounting method thereof
CN203372995U (en) Automatic-locking lifting claw for lifting braking devices of airplane
CN204210518U (en) A kind of combined transport vehicle
CN205401376U (en) Aircraft cockpit lid hanger bolt
CN203382368U (en) Simple segment end face lifting auxiliary device
CN207705603U (en) Convenient for the power distribution cabinet of hanging
CN105109665B (en) A kind of multi-functional wing jack nest
CN204198248U (en) A kind of box hanging beam
CN204161363U (en) A kind of overhead man-riding zero-speed device of boarding
CN103644181A (en) Tension expansion locking device
CN204433081U (en) A kind of double-layer folding formula plane draw bar draw gear
CN204198226U (en) A kind of reactor core lifting device
CN204846898U (en) Mainboard container
CN204021685U (en) The Simple transportation tool of band conveyer corridor prefabricated board
CN202214138U (en) Safety lifting hook for hanging aircraft seat
CN202791282U (en) Equipment capsizing preventing device
CN203865014U (en) Aircraft supporting frame
CN204237148U (en) Novel spiral propelling machine
CN203922569U (en) A kind of Simple power pole loading and unloading bracket

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term
CX01 Expiry of patent term

Granted publication date: 20150128