[go: up one dir, main page]

CN109056561A - A kind of automatic telescopic ladder helideck - Google Patents

A kind of automatic telescopic ladder helideck Download PDF

Info

Publication number
CN109056561A
CN109056561A CN201810636035.2A CN201810636035A CN109056561A CN 109056561 A CN109056561 A CN 109056561A CN 201810636035 A CN201810636035 A CN 201810636035A CN 109056561 A CN109056561 A CN 109056561A
Authority
CN
China
Prior art keywords
helideck
ladder
hydraulic stem
control device
folding ladder
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
Application number
CN201810636035.2A
Other languages
Chinese (zh)
Inventor
宋照飞
孔德群
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.)
Send Fly Industrial Group Co Ltd
Original Assignee
Send Fly Industrial Group Co Ltd
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 Send Fly Industrial Group Co Ltd filed Critical Send Fly Industrial Group Co Ltd
Priority to CN201810636035.2A priority Critical patent/CN109056561A/en
Publication of CN109056561A publication Critical patent/CN109056561A/en
Pending legal-status Critical Current

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E01CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01FADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
    • E01F3/00Landing stages for helicopters, e.g. located above buildings

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Ladders (AREA)

Abstract

The present invention relates to a kind of automatic telescopic ladder helidecks, including folding ladder, hydraulic stem, bracket, modular pressure, control device and helideck, the hydraulic stem is scalable hydraulic stem, the hydraulic stem both ends are fixedly connected with the folding ladder both ends, one end of the bracket is connected with folding ladder by bolt, the other end of the bracket is by buckle and is bolted to helideck edge, and the control device is set on the helideck, and the control device and hydraulic stem communicate to connect.Originally practical that aircraft weight is sensed by modular pressure, just ladder is made to stretch automatically, personnel can get on, and in no aircraft, ladder be will withdraw, and prevent irrelevant personnel up.

Description

A kind of automatic telescopic ladder helideck
Technical field
The art is related to helideck field, especially a kind of automatic telescopic ladder helideck.
Background technique
Helideck is to provide a platform of helicopter landing, common some airplane parking areas all in the top layer of building, It is unexpected in order to prevent to hit because cannot all there is barrier obstruction around when helicopter landing, so having selected building Top, but also therefore some can run forward and play, while these personnel are also possible to the equipment to helideck above Certain destruction is caused, some unnecessary losses are caused, staff is also different surely timely to be found, helicopter is made to rise and fall When increase difficulty.
Summary of the invention
In order to solve the above-mentioned technical problems, the present invention provides the following technical solutions: the present invention is a kind of automatic telescopic Terraced helideck, including folding ladder, bracket, hydraulic stem, modular pressure, control device, helideck.The folding ladder with it is hydraulic Bar is connected, and one end of the bracket is connected with folding ladder by bolt, and the other end of the bracket by buckle and is bolted To helideck edge, the control centre is embedded at helideck surface, and the control device and hydraulic stem communicate to connect.This It is practical that aircraft weight is sensed by modular pressure, just ladder is made to stretch automatically, personnel can get on, in no aircraft, Ladder will withdraw.
As a preferred solution of the present invention, the modular pressure is embedded in the elasticity landing plate of helideck, when When helicopter is parked in above, modular pressure is sent instructions to the aerial heart of control by gravity.
As a preferred solution of the present invention, the hydraulic stem is connected with folding ladder, hydraulic when control device is to signal Bar can be stretched out or be withdrawn, so that folding ladder expansion or withdrawal.
As a preferred solution of the present invention, the folding ladder makes folding ladder using aluminum alloy materials, aluminium alloy Folding ladder lighter weight, while can prevent from getting rusty.
The beneficial effects of the present invention are: preventing above irrelevant personnel man the helo level ground, especially helicopter is some ignorant Situations such as personnel cause helicopter that can not land above.
Detailed description of the invention
Fig. 1 is a kind of collapsed state schematic diagram of automatic telescopic ladder helideck of the present invention;
Fig. 2 is a kind of unfolded state schematic diagram of automatic telescopic ladder helideck of the present invention.
Specific embodiment
As shown in Figs. 1-2, a kind of automatic telescopic ladder helideck that one embodiment of the invention provides, including folding ladder 1, liquid Compression bar 2, modular pressure 3, control device 4, helideck 5, bracket 6.The folding ladder 1 is connected with hydraulic stem 2, the hydraulic stem 2 are connected with helideck 5, and one end of the bracket 6 is connected with folding ladder 1 by bolt, and the other end of the bracket 6 passes through card Detain and be bolted to 5 edge of helideck, the control centre 4 is connected with helideck 5, the control device 4 with it is hydraulic Bar 5 is connected, and the modular pressure 3 is connected with control module circuit 4.
The hydraulic stem 2 is connected with folding ladder 1 by bolt, and after hydraulic stem 2 is shunk completely, folding ladder 1 is in rugosity State;When 2 full extension of hydraulic stem, folding ladder 1 is in the state being fully deployed.
Further, the modular pressure 3 is installed in 5 intermediate region of helideck, with airplane parking area 5 be combined into one it is whole Body.
Further, the control device 4 is mounted on 1 side of folding ladder, is embedded in 4 the inside of helideck.
Further, the folding ladder 1 makes folding ladder 1 using aluminum alloy materials, 1 mass of folding ladder of aluminium alloy compared with Gently, it while can prevent from getting rusty.
Each technical characteristic of embodiment described above can be combined arbitrarily, for simplicity of description, not to above-mentioned reality It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited In contradiction, all should be considered as described in this specification.
The embodiments described above only express several embodiments of the present invention, and the description thereof is more specific and detailed, but simultaneously It cannot therefore be construed as limiting the scope of the patent.It should be pointed out that coming for those of ordinary skill in the art It says, without departing from the inventive concept of the premise, various modifications and improvements can be made, these belong to protection of the invention Range.Therefore, the scope of protection of the patent of the invention shall be subject to the appended claims.

Claims (4)

1. a kind of automatic telescopic ladder helideck, it is characterised in that: including folding ladder, hydraulic stem, bracket, modular pressure, control Device and helideck, the hydraulic stem are scalable hydraulic stem, the fixed company in the hydraulic stem both ends and the folding ladder both ends It connects, one end of the bracket is connected with folding ladder by bolt, and the other end of the bracket by buckle and is bolted to straight Machine level ground edge is risen, the control device is set on the helideck, and the control device and hydraulic stem communicate to connect.
2. a kind of automatic telescopic ladder helideck according to claim 1, it is characterised in that: the modular pressure is covered on directly It rises in the middle part of machine level ground, the modular pressure and the control device communicate to connect.
3. a kind of automatic telescopic ladder helideck according to claim 2, it is characterised in that: the modular pressure is perception pressure The element of power is varistor.
4. a kind of automatic telescopic ladder helideck according to claim 1, it is characterised in that: the material of the folding ladder is aluminium Alloy folding ladder.
CN201810636035.2A 2018-06-20 2018-06-20 A kind of automatic telescopic ladder helideck Pending CN109056561A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810636035.2A CN109056561A (en) 2018-06-20 2018-06-20 A kind of automatic telescopic ladder helideck

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810636035.2A CN109056561A (en) 2018-06-20 2018-06-20 A kind of automatic telescopic ladder helideck

Publications (1)

Publication Number Publication Date
CN109056561A true CN109056561A (en) 2018-12-21

Family

ID=64821045

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810636035.2A Pending CN109056561A (en) 2018-06-20 2018-06-20 A kind of automatic telescopic ladder helideck

Country Status (1)

Country Link
CN (1) CN109056561A (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0427001A (en) * 1990-05-22 1992-01-30 Kajima Corp heliport
CN201291807Y (en) * 2008-11-24 2009-08-19 中国电子科技集团公司第二十八研究所 Automatic companion-way
CN202264691U (en) * 2011-09-01 2012-06-06 国网通用航空有限公司 Helicopter landing system for power operation
CN203938977U (en) * 2014-07-02 2014-11-12 太平洋海洋工程(舟山)有限公司 The helicopter start and stop platform of ocean platform
KR20150033981A (en) * 2013-09-25 2015-04-02 삼성중공업 주식회사 Hand rail of heli-deck stairs
CN205617256U (en) * 2016-02-25 2016-10-05 广州送飞助航机电设备实业有限公司 Novel foldable deck of helideck
CN205637778U (en) * 2016-03-17 2016-10-12 广州送飞助航机电设备实业有限公司 Novel steel construction helideck
CN205891275U (en) * 2016-07-25 2017-01-18 南充驭云创新科技有限公司 A automatic airport system and automatic airport device for unmanned aerial vehicle

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0427001A (en) * 1990-05-22 1992-01-30 Kajima Corp heliport
CN201291807Y (en) * 2008-11-24 2009-08-19 中国电子科技集团公司第二十八研究所 Automatic companion-way
CN202264691U (en) * 2011-09-01 2012-06-06 国网通用航空有限公司 Helicopter landing system for power operation
KR20150033981A (en) * 2013-09-25 2015-04-02 삼성중공업 주식회사 Hand rail of heli-deck stairs
CN203938977U (en) * 2014-07-02 2014-11-12 太平洋海洋工程(舟山)有限公司 The helicopter start and stop platform of ocean platform
CN205617256U (en) * 2016-02-25 2016-10-05 广州送飞助航机电设备实业有限公司 Novel foldable deck of helideck
CN205637778U (en) * 2016-03-17 2016-10-12 广州送飞助航机电设备实业有限公司 Novel steel construction helideck
CN205891275U (en) * 2016-07-25 2017-01-18 南充驭云创新科技有限公司 A automatic airport system and automatic airport device for unmanned aerial vehicle

Similar Documents

Publication Publication Date Title
US20210402235A1 (en) Quint configuration fire apparatus
US1306860A (en) sheet
US9315263B2 (en) Method of automatically triggering an emergency buoyancy system for a hybrid helicopter
US4087062A (en) Aircraft undercarriage including a safety device having a predetermined breaking load
US20160145941A1 (en) Outrigger assembly for a fire apparatus
US20140252166A1 (en) Crash Load Attenuator for Water Ditching and Floatation
CN109625305A (en) A kind of unmanned plane recyclable device
CN207148654U (en) A kind of fixed wing aircraft cargo dropping and reception system
CN104843194A (en) Airport mobile control tower command and control center
DE19934210A1 (en) Transport system with carrier has cargo volume in form of cargo module for replaceable mounting in bay or aperture in fuselage of carrier arrangement, e.g. passenger or transport aircraft
WO2024017419A1 (en) A bionic folding fixed wing household small manned aircraft
CN109056561A (en) A kind of automatic telescopic ladder helideck
CN110406454A (en) Quick carrying equipment for emergency rescue of airplane
CN104443413A (en) Unmanned aerial vehicle withdrawing equipment
US7871037B2 (en) Emergency landing apparatus
CN107190608A (en) A kind of forced landing buffering rescue runway
CN204750595U (en) Control tower commander control center is moved on airport
CN203237402U (en) Wheelless forced landing refugee board of aircraft on runway or without runway
CN117602058A (en) Oval wing foldable light household small-sized manned aircraft
DE19610052A1 (en) Parachute device with sliding landing board
US4000871A (en) Airplane fuselage structure
CN104386239B (en) A kind of anti-rollover airframe steel framework structure
CN2146430Y (en) Aircraft-carrier flight deck
US20220134152A1 (en) Precision Aerial Firefighting and Deluge System for Helicopters and Unmanned Aerial Systems
CN221438369U (en) Airport visual shielding object capable of reducing electromagnetic environment influence

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
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20181221