CN109421916A - A kind of baby plane boarding method - Google Patents
A kind of baby plane boarding method Download PDFInfo
- Publication number
- CN109421916A CN109421916A CN201710735233.XA CN201710735233A CN109421916A CN 109421916 A CN109421916 A CN 109421916A CN 201710735233 A CN201710735233 A CN 201710735233A CN 109421916 A CN109421916 A CN 109421916A
- Authority
- CN
- China
- Prior art keywords
- ladder
- trailing edge
- baby plane
- boarding
- wing
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/24—Steps mounted on, and retractable within, fuselages
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Ladders (AREA)
Abstract
A kind of baby plane boarding method, the following steps are included: setting ladder-shaped for baby plane wing wing root trailing edge potion and forming entirety with aircraft wing, ladder-shaped is connect with baby plane trailing edge by hinge axis, and in baby plane trailing edge setting lock for locking after receiving upper ladder；The lock of baby plane trailing edge is unlocked, then manually puts down the ladder of aircraft wing wing root trailing edge potion, ladder around hinge axis deflects down, and personnel pass through ladder boarding；Personnel are got off the plane by ladder, upward deflect in receipts by the way that ladder is received upper and aircraft wing rear pairing, ladder around hinge axis manually, then the lock of baby plane trailing edge is locked, so that ladder and aircraft wing form entirety.The baby plane boarding method alleviates baby plane boarding work difficulty, reduces the demand to ground boarding equipment, has saved boarding cost and time, the usability and maintainability of aircraft are improved in the case where guaranteeing Aerodynamic Configuration of Aireraft.
Description
Technical field
The invention belongs to airplane design technical fields, and in particular to a kind of baby plane boarding method.
Background technique
Baby plane, which is boarded a plane, generally uses the ladder of boarding, needs staff that ladder is placed in suitable position,
Meet boarding demand.Ladder is replaced again after the completion of boarding operation, this mode needs to make ladder and also needs to ladder
Daily management is carried out, workload is not only increased, also increases the investment of cost, but also aircraft utilization and maintainability are not able to satisfy
It is required that.
Summary of the invention
In order to solve the above technical problems, being not required to working stand the present invention provides one kind climbs up small baby plane, machine in reduction
Workload does not influence the baby plane boarding method of Aerodynamic Configuration of Aireraft again.
A kind of baby plane boarding method, comprising the following steps: (1) boarding device is arranged: by baby plane wing wing root
Trailing edge potion is set as ladder-shaped and forms entirety with aircraft wing, will be after ladder-shaped and baby plane wing by hinge axis
Edge connection, and in baby plane trailing edge setting lock for locking after receiving upper ladder；(2) aboard: by baby plane machine
The lock of wing rear is unlocked, and then manually puts down the ladder of aircraft wing wing root trailing edge potion, ladder around hinge axis downward bias
Turn, personnel pass through ladder boarding；(3) get off the plane: personnel are got off the plane by ladder, by the way that ladder is received upper and aircraft wing manually
Rear pairing, ladder around hinge axis upward deflects in receipts, then the lock of baby plane trailing edge is locked, so that ladder
Entirety is formed with aircraft wing.
Further, the manual ladder by aircraft wing wing root trailing edge potion of the step of baby plane boarding method (2) is put
Under replace with hydraulic actuation or motor actuation, ladder is received upper and aircraft wing rear pairing and replaces with liquid by the manual of step (3)
Press actuation or motor actuation.
It being had the beneficial effect that by what the technological means present invention obtained, the baby plane boarding method is simple, convenient for operating,
Baby plane boarding work difficulty is alleviated, the demand to ground boarding equipment is reduced, has saved boarding cost and time, protected
The usability and maintainability of aircraft are improved in the case where card Aerodynamic Configuration of Aireraft.
Specific embodiment
Principles and features of the present invention are described below in conjunction with example, example is served only for explaining invention, not
For limiting the scope of the invention.
A kind of baby plane boarding method, comprising the following steps:
(1) boarding device be arranged: by baby plane wing wing root trailing edge potion be set as ladder-shaped and with aircraft wing shape
It is integral, ladder-shaped is connect with baby plane trailing edge by hinge axis, and be arranged in baby plane trailing edge and lock
For locking after receiving upper ladder；
(2) aboard: the lock of baby plane trailing edge is unlocked, then manually by aircraft wing wing root rear
The ladder in portion is put down, and ladder around hinge axis deflects down, and personnel pass through ladder boarding；
(3) get off the plane: personnel are got off the plane by ladder, by the way that ladder is received upper and aircraft wing rear pairing, ladder manually
Sub- around hinge axis upward deflects in receipts, and then the lock of baby plane trailing edge is locked, so that ladder and aircraft wing
It is formed whole.
To make ladder receive upper and putting down with various ways, its adaptability is improved.The step of baby plane boarding method
(2) the manual ladder by aircraft wing wing root trailing edge potion, which is put down, replaces with hydraulic actuation or motor actuation, step (3) it is manual
Ladder is received into upper and aircraft wing rear pairing and replaces with hydraulic actuation or motor actuation.
Above-mentioned technical proposal only embodies the optimal technical scheme of technical solution of the present invention, those skilled in the art
The principle of the present invention is embodied to some variations that some of them part may be made, belongs to the scope of protection of the present invention it
It is interior.
Claims (2)
1. a kind of baby plane boarding method, it is characterised in that: the described method comprises the following steps:
(1) boarding device is arranged: setting ladder-shaped for baby plane wing wing root trailing edge potion and is formed with aircraft wing whole
Ladder-shaped is connect by body by hinge axis with baby plane trailing edge, and is used in baby plane trailing edge setting lock
It locks after ladder in receipts；
(2) aboard: the lock of baby plane trailing edge is unlocked, then manually by aircraft wing wing root trailing edge potion
Ladder is put down, and ladder around hinge axis deflects down, and personnel pass through ladder boarding；
(3) get off the plane: personnel are got off the plane by ladder, by the way that ladder is received upper and aircraft wing rear pairing manually, ladder around
Hinge axis upward deflects in receipts, and then the lock of baby plane trailing edge is locked, so that ladder is formed with aircraft wing
It is whole.
2. baby plane boarding method according to claim 1, it is characterised in that: the step (2) it is manual by aircraft
The ladder of wing wing root trailing edge potion, which is put down, replaces with hydraulic actuation or motor actuation, and the manual of step (3) receives ladder
Hydraulic actuation or motor actuation are replaced with aircraft wing rear pairing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710735233.XA CN109421916A (en) | 2017-08-24 | 2017-08-24 | A kind of baby plane boarding method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710735233.XA CN109421916A (en) | 2017-08-24 | 2017-08-24 | A kind of baby plane boarding method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109421916A true CN109421916A (en) | 2019-03-05 |
Family
ID=65501084
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710735233.XA Pending CN109421916A (en) | 2017-08-24 | 2017-08-24 | A kind of baby plane boarding method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109421916A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE722976C (en) * | 1940-01-31 | 1942-07-25 | Henschel Flugzeug Werke A G | Access ladder formed by an edge of the aircraft wing |
| CN2129265Y (en) * | 1992-05-22 | 1993-04-07 | 北京石油化工专科学校 | Plane door integrated with stepladder |
| CN203428045U (en) * | 2013-05-30 | 2014-02-12 | 江西洪都航空工业集团有限责任公司 | Combined hook ladder for airplane |
| CN104816816A (en) * | 2013-11-08 | 2015-08-05 | 埃姆普里萨有限公司 | Force-balancing mechanisms especially useful for assisted lifting/lowering of aircraft stairs |
| CN105667759A (en) * | 2015-12-28 | 2016-06-15 | 武汉蓝天翔航空科技有限公司 | Movable wing large airplane with flexible take-off or landing function |
| BR102015031730A2 (en) * | 2015-12-17 | 2017-06-20 | Embraer Sa | ACCESS DOOR FOR AIRCRAFT AND AIRCRAFT |
| CN206288227U (en) * | 2016-11-30 | 2017-06-30 | 江西洪都航空工业集团有限责任公司 | A kind of random airstair of folded turnover formula |
-
2017
- 2017-08-24 CN CN201710735233.XA patent/CN109421916A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE722976C (en) * | 1940-01-31 | 1942-07-25 | Henschel Flugzeug Werke A G | Access ladder formed by an edge of the aircraft wing |
| CN2129265Y (en) * | 1992-05-22 | 1993-04-07 | 北京石油化工专科学校 | Plane door integrated with stepladder |
| CN203428045U (en) * | 2013-05-30 | 2014-02-12 | 江西洪都航空工业集团有限责任公司 | Combined hook ladder for airplane |
| CN104816816A (en) * | 2013-11-08 | 2015-08-05 | 埃姆普里萨有限公司 | Force-balancing mechanisms especially useful for assisted lifting/lowering of aircraft stairs |
| BR102015031730A2 (en) * | 2015-12-17 | 2017-06-20 | Embraer Sa | ACCESS DOOR FOR AIRCRAFT AND AIRCRAFT |
| US20170174309A1 (en) * | 2015-12-17 | 2017-06-22 | Embraer S.A. | Aircraft access door and aircraft |
| CN105667759A (en) * | 2015-12-28 | 2016-06-15 | 武汉蓝天翔航空科技有限公司 | Movable wing large airplane with flexible take-off or landing function |
| CN206288227U (en) * | 2016-11-30 | 2017-06-30 | 江西洪都航空工业集团有限责任公司 | A kind of random airstair of folded turnover formula |
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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 |
Application publication date: 20190305 |
|
| WD01 | Invention patent application deemed withdrawn after publication |