CN106592357B - A kind of airfield pavement bend transition face elevation design method - Google Patents

A kind of airfield pavement bend transition face elevation design method Download PDF

Info

Publication number
CN106592357B
CN106592357B CN201611153972.XA CN201611153972A CN106592357B CN 106592357 B CN106592357 B CN 106592357B CN 201611153972 A CN201611153972 A CN 201611153972A CN 106592357 B CN106592357 B CN 106592357B
Authority
CN
China
Prior art keywords
face
point
elevation
transition
pavement slab
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.)
Active
Application number
CN201611153972.XA
Other languages
Chinese (zh)
Other versions
CN106592357A (en
Inventor
李光元
许巍
邵斌
史保华
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.)
Air Force Engineering University of PLA
Original Assignee
Air Force Engineering University of PLA
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 Air Force Engineering University of PLA filed Critical Air Force Engineering University of PLA
Priority to CN201611153972.XA priority Critical patent/CN106592357B/en
Publication of CN106592357A publication Critical patent/CN106592357A/en
Application granted granted Critical
Publication of CN106592357B publication Critical patent/CN106592357B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E01CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01CCONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
    • E01C1/00Design or layout of roads, e.g. for noise abatement, for gas absorption
    • E01C1/002Design or lay-out of roads, e.g. street systems, cross-sections ; Design for noise abatement, e.g. sunken road
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06TIMAGE DATA PROCESSING OR GENERATION, IN GENERAL
    • G06T11/002D [Two Dimensional] image generation
    • G06T11/20Drawing from basic elements, e.g. lines or circles
    • G06T11/203Drawing of straight lines or curves

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Road Paving Structures (AREA)

Abstract

The invention discloses a kind of Dao Mian bends area elevation design methods, first to needing the region that transition face is arranged to be designed into trade face dividing, the design altitude value on sideline that determining rule face connects with transition face, height value mark is in the known point that on road face dividing angle point, these points are designed as bend area;Obtain the coordinate (x of N number of regular face marginal pointi,yi) and height value (zi);Assuming that new pavement slab angular coordinate is (x0,y0);New pavement slab angle point is calculated to the horizontal distance of each known point, calculates pavement slab angle point elevation z0, by pavement slab angle point elevation z0It is labeled in face dividing point (x0,y0) position, road face dividing elevation map is formed, transition face region is drawn and designs contour, whether the draining of test design face is smooth.The beneficial effects of the invention are as follows making the face transition of transition region road gentler, aircraft utilization more smoothes out, and the draining of road face is more smooth.

Description

A kind of airfield pavement bend transition face elevation design method
Technical field
The invention belongs to airfield runway technical field of buildings, are related to a kind of airfield pavement bend transition face elevation design side Method.
Background technology
When airfield pavement designs, the road face vertical and horizontal gradient requirement of airfield pavement different parts is different, due to skill Art index is different, and the value of slope of design is often also different.In the curved areas that people having a common goal face is not connected mutually due to adjacent road face region The gradient it is different, can be in junction generation road face faulting of slab ends.In order to meet the use of aircraft, it is necessary to which the gentle transition for solving faulting of slab ends is asked Topic, the method used at present are a new inclined-plane to be arranged as transition face in faulting of slab ends position, with the road face of filling-in faulting of slab ends both sides, But new transition face is an irregular face, and pavement slab is rectangle rule plate, therefore there are transition faces and road for existing method Panel is uncoordinated, road face may ponding, aircraft operation be not much smoother problem.
Invention content
The purpose of the present invention is to provide a kind of Dao Mian bends area elevation design methods, solve and are set at present in airfield pavement Timing transition region road faceplate panels are uncoordinated to cause aircraft to run the problem of having some setbacks.
The technical solution adopted in the present invention is to follow the steps below:
Step 1:First to needing the region that transition face is arranged to be designed into trade face dividing, determine that rule face connects with transition face Sideline on design altitude value, to curved areas pavement slab according to regulation size piecemeal, calculate on the sideline of curved areas Design altitude value, and mark in the known point that on road face dividing angle point, these points are designed as bend area;
Step 2:Obtain the coordinate (x of N number of regular face marginal pointi,yi) and height value (zi);
Step 3:Assuming that new pavement slab angular coordinate is (x0,y0);
Step 4:Calculate new pavement slab angle point to each known point horizontal distance di0, share N number of value
Step 5:Calculate pavement slab angle point elevation z0
Step 6:By pavement slab angle point elevation z0It is labeled in face dividing point (x0,y0) position, form road face dividing elevation Figure draws transition face region and designs contour, and whether the draining of test design face is smooth.
Further, it in the step 6, if contour does not have closed annular region, is evenly distributed, then drains smooth.
The beneficial effects of the invention are as follows using the method based on anti-distance power interpolation, a kind of novel bend transition region is established Elevation design method overcomes and needs to design defect of the plane as transition face so that the face transition of transition region road is more over Add gently, aircraft utilization more smoothes out, and the draining of road face is more smooth.
Description of the drawings
Fig. 1 is curved areas rule face edge elevation schematic diagram;
Fig. 2 is designed contour map.
Specific implementation mode
The present invention is described in detail With reference to embodiment.
1, first to needing the region that transition face is arranged to be designed into trade face dividing, according to runway, taxiway or connecting taxiway Design grade, the design altitude value on sideline that determining rule face connects with transition face.Such as Fig. 1, first to curved areas pavement slab According to regulation size piecemeal, according to five angle point elevations 12.665,12.755,12.555,12.455,12.515, linear interpolation The design altitude value on the sideline of curved areas is calculated, and is marked on road face dividing angle point, these points are designed as bend area Known point.
2, the coordinate (x of known N number of regular face marginal pointi,yi) and height value (zi)。
3, assume to need to calculate new pavement slab angular coordinate (x0,y0)。
4, horizontal distance d of the new pavement slab angle point of calculating to each known pointi0, share N number of value
5, pavement slab angle point elevation z is calculated with formula once0
6, height value z will be calculated0It is labeled in face dividing point (x0,y0) position, form road face dividing elevation map.Using general Logical linear interpolation method draws transition face region and designs contour, and whether the draining of test design face is smooth, if contour does not close Annular region is closed, is evenly distributed, then drains smooth.
As a result such as Fig. 2, rectangle black lines are road face dividing sideline, and number is road face dividing height value, and curved lines are According to the design road face contour that road face dividing height value is drawn, contour interval 2cm, every 5 contour overstrikings, one contour.
The above is only the better embodiment to the present invention, not makees limit in any form to the present invention System, every any simple modification that embodiment of above is made according to the technical essence of the invention, equivalent variations and modification, Belong in the range of technical solution of the present invention.

Claims (2)

1. a kind of airfield pavement bend transition face elevation design method, it is characterised in that follow the steps below:
Step 1:First to needing the region that transition face is arranged to be designed into trade face dividing, the side that rule face connects with transition face is determined Design altitude value on line calculates the design on the sideline of curved areas to curved areas pavement slab according to regulation size piecemeal Height value, and mark in the known point that on road face dividing angle point, these points are designed as bend area;
Step 2:Obtain the coordinate (x of N number of regular face marginal pointi,yi) and height value (zi);
Step 3:Assuming that new pavement slab angular coordinate is (x0,y0);
Step 4:Calculate new pavement slab angle point to each known point horizontal distance di0, share N number of value
Step 5:Calculate pavement slab angle point elevation z0
Step 6:By pavement slab angle point elevation z0It is labeled in face dividing point (x0,y0) position, road face dividing elevation map is formed, is painted Contour is designed in transition face region processed, and whether the draining of test design face is smooth.
2. according to a kind of airfield pavement bend transition face elevation design method described in claim 1, it is characterised in that:The step It in 6, if contour does not have closed annular region, is evenly distributed, then drains smooth.
CN201611153972.XA 2016-12-14 2016-12-14 A kind of airfield pavement bend transition face elevation design method Active CN106592357B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611153972.XA CN106592357B (en) 2016-12-14 2016-12-14 A kind of airfield pavement bend transition face elevation design method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611153972.XA CN106592357B (en) 2016-12-14 2016-12-14 A kind of airfield pavement bend transition face elevation design method

Publications (2)

Publication Number Publication Date
CN106592357A CN106592357A (en) 2017-04-26
CN106592357B true CN106592357B (en) 2018-10-23

Family

ID=58801288

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611153972.XA Active CN106592357B (en) 2016-12-14 2016-12-14 A kind of airfield pavement bend transition face elevation design method

Country Status (1)

Country Link
CN (1) CN106592357B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107391915B (en) * 2017-07-10 2020-06-09 中国人民解放军空军工程大学 Road and airplane runway clearance assessment method
CN110794260B (en) * 2019-11-04 2021-08-31 国网福建省电力有限公司 Overhead transmission line positioning method based on double RTK unmanned aerial vehicles

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001222569A (en) * 2000-02-10 2001-08-17 Ricoh Co Ltd Method and device for generating interference line in three-dimensional form processing system and recording medium
KR100644332B1 (en) * 2005-08-18 2006-11-14 이기영 Fold-up ramp
CN103049608A (en) * 2012-12-18 2013-04-17 南京航空航天大学 System and method of load identification based on restrained edge strain extreme value coordinates
CN104331928A (en) * 2014-10-28 2015-02-04 中国航空工业集团公司洛阳电光设备研究所 Automatic contour elevation value assignment method based on triangulation network
CN104408771A (en) * 2014-11-12 2015-03-11 东北大学 Underground mine ramp constructing method based on three-dimensional model
CN106097450A (en) * 2016-06-21 2016-11-09 武汉瑞得信息工程有限责任公司 A kind of contour lines creation method and device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001222569A (en) * 2000-02-10 2001-08-17 Ricoh Co Ltd Method and device for generating interference line in three-dimensional form processing system and recording medium
KR100644332B1 (en) * 2005-08-18 2006-11-14 이기영 Fold-up ramp
CN103049608A (en) * 2012-12-18 2013-04-17 南京航空航天大学 System and method of load identification based on restrained edge strain extreme value coordinates
CN104331928A (en) * 2014-10-28 2015-02-04 中国航空工业集团公司洛阳电光设备研究所 Automatic contour elevation value assignment method based on triangulation network
CN104408771A (en) * 2014-11-12 2015-03-11 东北大学 Underground mine ramp constructing method based on three-dimensional model
CN106097450A (en) * 2016-06-21 2016-11-09 武汉瑞得信息工程有限责任公司 A kind of contour lines creation method and device

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
浅谈机场旧刚性道面上水泥砼盖被设计;邢耀忠;《公路工程》;20110228;第36卷(第1期);第70-71、96页 *
高程差异的双跑道机场内水平确定方法研究;王维等;《中国民航大学学报》;20130228;第31卷(第1期);第59-62页 *

Also Published As

Publication number Publication date
CN106592357A (en) 2017-04-26

Similar Documents

Publication Publication Date Title
US20220309201A1 (en) Artificial-intelligence-assisted method for providing urban design form and layout with improved wind environment
CN102779231B (en) Based on contiguous coordinate transformation parameter computing method
CN105023014B (en) A kind of shaft tower target extraction method in unmanned plane inspection transmission line of electricity image
CN103020342B (en) Method for extracting contour and corner of building from ground LiDAR data
CN103366631B (en) A kind of method making indoor map and the device making indoor map
CN109887082A (en) A kind of interior architecture three-dimensional modeling method and device based on point cloud data
CN102609941A (en) Three-dimensional registering method based on ToF (Time-of-Flight) depth camera
CN110532602A (en) A kind of indoor autodraft and modeling method based on plan view image
CN107808386A (en) A kind of sea horizon detection method based on image, semantic segmentation
CN106592357B (en) A kind of airfield pavement bend transition face elevation design method
CN104463970B (en) Method for determining three-dimensional gravity center of city based on remote-sensing image and application thereof
CN104318605B (en) Parallel lamination rendering method of vector solid line and three-dimensional terrain
Kim et al. Semiautomatic reconstruction of building height and footprints from single satellite images
CN105006006A (en) City high-temperature region ventilation tunnel calculation method and system
CN104750938A (en) GIS (Geographic Information System)-based urban ventilating gallery identifying method and system
CN107391915A (en) A kind of pavement airstrip headroom assessment method
CN105469057A (en) Hough line detection and projection-based automobile window detection method
CN104134389A (en) Interactive sand table demonstration system and method
CN102938064A (en) Park structure extraction method based on LiDAR data and ortho-images
CN105184854B (en) For the fast modeling method of underground space scanning element cloud performance data
CN104457691A (en) Method for obtaining elevation information of main building body
CN110298778A (en) One kind being based on raster data and the modified traffic zone demographics method of area ratio
CN106339985A (en) Method for aviation image mosaic by selecting mosaic lines from vector building data
CN103489197B (en) A kind of urban aerial image corner feature matching process
CN103810450B (en) Method and system for accurate area positioning of radio frequency identification

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
GR01 Patent grant
GR01 Patent grant