CN109319089A - A kind of airstair - Google Patents

A kind of airstair Download PDF

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Publication number
CN109319089A
CN109319089A CN201710645294.7A CN201710645294A CN109319089A CN 109319089 A CN109319089 A CN 109319089A CN 201710645294 A CN201710645294 A CN 201710645294A CN 109319089 A CN109319089 A CN 109319089A
Authority
CN
China
Prior art keywords
plate
pedal
left plate
outer rim
side plate
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
CN201710645294.7A
Other languages
Chinese (zh)
Inventor
高海燕
冯冬翔
甘亚东
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 CN201710645294.7A priority Critical patent/CN109319089A/en
Publication of CN109319089A publication Critical patent/CN109319089A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1407Doors; surrounding frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/24Steps mounted on, and retractable within, fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wing Frames And Configurations (AREA)

Abstract

The present invention relates to the design of aircraft door structure, in particular to a kind of airstairs.Airstair includes: the left plate being made of composite material, and the outer rim of left plate side is arc-shaped, and the outer rim of the other side is in step-like;The shapes and sizes of the right side plate being made of composite material, right side plate are identical as left plate, and right side plate is parallel to each other and is symmetrical arranged with left plate;The pedal being made of composite material, in multistage bending, by mortise-tenon joint, the right side edge of pedal and the outer rim of right side plate pass through mortise-tenon joint for the left side edge of pedal and the outer rim of left plate, in addition, being connect at the mortise-tenon joint of left plate and right side plate by co-curing in pedal.Airstair of the invention, connection structure stability is stronger, also, under the premise of meeting use intensity requirement, greatly reduces the weight of cabin door structure, improve the economy that hatch door uses.

Description

A kind of airstair
Technical field
The present invention relates to the design of aircraft door structure, in particular to a kind of airstairs.
Background technique
Airstairs of airplane is the aircraft proximity device to go on or off the plane for boarding personnel.Current Airstairs of airplane is especially Door ladder unification landing gate airstair considerably increases the weight of boarding door mostly using metal structure;In addition, stepping on Connection between each part of machine ladder causes airstair to can not meet intensity requirement there is also unreasonable defect is connected.
Summary of the invention
The object of the present invention is to provide a kind of airstairs, to solve the problems, such as at least one existing for existing airstair.
The technical scheme is that
A kind of airstair, comprising:
Left plate is made of composite material, and the outer rim of the left plate side is arc-shaped, with pre- applicable aircraft door Shape matches, and the outer rim of the other side opposite with the arcing outer edges is in step-like on the left plate;
Right side plate is made of composite material, and the shapes and sizes of the right side plate are identical as the left plate, the right side Plate is parallel to each other and is symmetrical arranged with the left plate;
Pedal is made of composite material, the pedal be in multistage bending, left and right sides edge be shaped to it is described Left plate and the step-like outer rim shape of right side plate are compatible step-like, wherein the left side edge of the pedal and the left side The outer rim of plate passes through mortise-tenon joint by mortise-tenon joint, the right side edge of the pedal and the outer rim of the right side plate, in addition, The pedal is connect at the mortise-tenon joint of the left plate and right side plate by co-curing.
Preferably, the tenon and tenon uniformly to distribute alternately is offered in the step-like outer rim of the left plate and right side plate Slot offers the compatible tongue-and-groove and tenon uniformly to distribute alternately in the left and right sides edge of the pedal.
The present invention has the advantages that
Airstair of the invention, connection structure stability is stronger, also, under the premise of meeting use intensity requirement, pole The weight for reducing cabin door structure greatly, improves the economy that hatch door uses.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of airstair left side perspective of the present invention;
Fig. 2 is the structural schematic diagram of airstair right side perspective of the present invention;
Fig. 3 is the structural schematic diagram of left plate or right side plate in airstair of the present invention;
Fig. 4 is the structural schematic diagram of pedal in airstair of the present invention.
Specific embodiment
To keep the purposes, technical schemes and advantages of the invention implemented clearer, below in conjunction in the embodiment of the present invention Attached drawing, technical solution in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from beginning to end or class As label indicate same or similar element or element with the same or similar functions.Described embodiment is the present invention A part of the embodiment, instead of all the embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to use It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiments of the present invention, ordinary skill people Member's every other embodiment obtained without creative efforts, shall fall within the protection scope of the present invention.Under Face is described in detail the embodiment of the present invention in conjunction with attached drawing.
In the description of the present invention, it is to be understood that, term " center ", " longitudinal direction ", " transverse direction ", "front", "rear", The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is based on attached drawing institute The orientation or positional relationship shown, is merely for convenience of description of the present invention and simplification of the description, rather than the dress of indication or suggestion meaning It sets or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as protecting the present invention The limitation of range.
1 to Fig. 4 airstair of the invention is described in further details with reference to the accompanying drawing.
The present invention provides a kind of airstairs, including left plate 11, right side plate 12 and pedal 2.
Left plate 11 is made of composite material;The outer rim of 11 side of left plate (lower left side in Fig. 1) is arc-shaped, is applicable in pre- The shape of aircraft door match;The outer rim of the other side opposite with arcing outer edges (upper right side in Fig. 1) is on left plate 11 It is step-like.
Right side plate 12 is made of composite material;The shapes and sizes of right side plate 12 are identical as left plate 11, right side plate 12 with Left plate 11 is parallel to each other and is symmetrical arranged.
Pedal 2 is made of composite material;Pedal 2 is in multistage bending, and left and right sides edge is shaped to and left plate 11 is compatible step-like with the step-like outer rim shape of right side plate 12;Wherein, the outer rim of the left side edge of pedal 2 and left plate 11 By mortise-tenon joint, the right side edge of pedal 2 and the outer rim of right side plate 12 are by mortise-tenon joint, in addition, in pedal 2 and left plate 11 are connected at the mortise-tenon joint of right side plate 12 by co-curing, to form airstair structure.
It should be noted that left plate 11, right side plate 12 and pedal 2 can use known a variety of suitable composite woods Material is constituted, and there is honeycomb in inside;Also, passes through co-curing molding mode again at the position by mortise-tenon joint and company is fixed It connects, so that connection structure stability is stronger, thus the economy used in the weight and raising hatch door for greatly reducing cabin door structure Property under the premise of, moreover it is possible to meet use intensity requirement.
Further, at the mortise-tenon joint of pedal 2 and left plate 11 and right side plate 12, it can be and tenon is set on pedal 2 First 31, matched tongue-and-groove 32 is set on left plate 11 and right side plate 12;Of course, it can be reversed;In the present embodiment, exist On pedal 2 or left side plate, spacing is smaller between two tenons 31, so that indirect forming is a tongue-and-groove 32, so similar It is spaced apart form in what a tenon 31 connect a tongue-and-groove 32, the stability of connection structure can be further strengthened.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any In the technical scope disclosed by the present invention, any changes or substitutions that can be easily thought of by those familiar with the art, all answers It is included within the scope of the present invention.Therefore, protection scope of the present invention should be with the scope of protection of the claims It is quasi-.

Claims (2)

1. a kind of airstair characterized by comprising
Left plate (11), is made of composite material, and the outer rim of left plate (11) side is arc-shaped, with pre- applicable aircraft cabin The shape of door matches, and the outer rim of the other side opposite with the arcing outer edges is in step-like on the left plate (11);
Right side plate (12), is made of composite material, and the shapes and sizes of the right side plate (12) are identical as the left plate (11), The right side plate (12) is parallel to each other and is symmetrical arranged with the left plate (11);
Pedal (2), is made of composite material, and the pedal (2) is in multistage bending, and left and right sides edge is shaped to and institute It states left plate (11) and the step-like outer rim shape of right side plate (12) is compatible step-like, wherein the left side of the pedal (2) The outer rim of edge and the left plate (11) passes through mortise-tenon joint, right side edge and the right side plate (12) of the pedal (2) Outer rim is by mortise-tenon joint, in addition, leading at the mortise-tenon joint of the pedal (2) and the left plate (11) and right side plate (12) Cross co-curing connection.
2. airstair according to claim 1, which is characterized in that in the step of the left plate (11) and right side plate (12) The tenon (31) and tongue-and-groove (32) uniformly to distribute alternately is offered in shape outer rim, in the left and right sides edge of the pedal (2) Offer the compatible tongue-and-groove (32) and tenon (31) uniformly to distribute alternately.
CN201710645294.7A 2017-08-01 2017-08-01 A kind of airstair Pending CN109319089A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710645294.7A CN109319089A (en) 2017-08-01 2017-08-01 A kind of airstair

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710645294.7A CN109319089A (en) 2017-08-01 2017-08-01 A kind of airstair

Publications (1)

Publication Number Publication Date
CN109319089A true CN109319089A (en) 2019-02-12

Family

ID=65245233

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710645294.7A Pending CN109319089A (en) 2017-08-01 2017-08-01 A kind of airstair

Country Status (1)

Country Link
CN (1) CN109319089A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4008626A1 (en) * 2020-12-04 2022-06-08 Gulfstream Aerospace Corporation Apparatus for supporting a person adjacent to an aircraft engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4008626A1 (en) * 2020-12-04 2022-06-08 Gulfstream Aerospace Corporation Apparatus for supporting a person adjacent to an aircraft engine

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PB01 Publication
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20190212