CN108008762A - A kind of passenger takes the determination methods of aircraft seat comfort level during flight - Google Patents
A kind of passenger takes the determination methods of aircraft seat comfort level during flight Download PDFInfo
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- CN108008762A CN108008762A CN201711255317.XA CN201711255317A CN108008762A CN 108008762 A CN108008762 A CN 108008762A CN 201711255317 A CN201711255317 A CN 201711255317A CN 108008762 A CN108008762 A CN 108008762A
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- 238000000034 method Methods 0.000 title claims abstract description 13
- 238000000205 computational method Methods 0.000 claims description 5
- 230000002159 abnormal effect Effects 0.000 claims description 3
- 230000000630 rising effect Effects 0.000 claims description 3
- 102000003712 Complement factor B Human genes 0.000 claims description 2
- 108090000056 Complement factor B Proteins 0.000 claims description 2
- 230000037396 body weight Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06C—DIGITAL COMPUTERS IN WHICH ALL THE COMPUTATION IS EFFECTED MECHANICALLY
- G06C3/00—Arrangements for table look-up, e.g. menstruation table
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- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61B—DIAGNOSIS; SURGERY; IDENTIFICATION
- A61B5/00—Measuring for diagnostic purposes; Identification of persons
- A61B5/103—Detecting, measuring or recording devices for testing the shape, pattern, colour, size or movement of the body or parts thereof, for diagnostic purposes
- A61B5/107—Measuring physical dimensions, e.g. size of the entire body or parts thereof
- A61B5/1072—Measuring physical dimensions, e.g. size of the entire body or parts thereof measuring distances on the body, e.g. measuring length, height or thickness
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01G—WEIGHING
- G01G19/00—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups
- G01G19/44—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing persons
- G01G19/50—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing persons having additional measuring devices, e.g. for height
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- Oral & Maxillofacial Surgery (AREA)
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- Heart & Thoracic Surgery (AREA)
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- Seats For Vehicles (AREA)
Abstract
The invention discloses the determination methods that a kind of passenger takes aircraft seat comfort level during flight, comprise the following steps：According to the height and weight data of individual, standard stature index is calculated to judge whether individual belongs to partially fat stature；The stature index correction factor of individual is calculated according to standard stature index；The standard sitting posture hip breadth of human body is calculated according to standard stature index；According to the height and weight data of individual, hip breadth correction factor is calculated；According to the standard sitting posture hip breadth and hip breadth correction factor of human body, individual human body sitting posture hip breadth is calculated；Aircraft seat width data table is searched, and according to standard stature index range, when calculating seat width comfort level, that is, people sits down on the seat, the distance under seat is empty；Judge whether seat width is suitable.The present invention can calculate aircraft seat comfort level according to the height and weight data of passenger, provide a kind of scientific basis for selecting flight and cabin etc. for passenger, that improves passenger seizes the opportunity experience.
Description
Technical field
The present invention relates to the determination methods that a kind of passenger takes aircraft seat comfort level during flight, belong to civil aviaton's information
Technical field.
Background technology
With booming, the convenient and efficient and safe aviation of more and more passengers' selections of civil aviaton's cause and economy
Trip, so for passenger, flight comfort level is to select the important references condition of flight.The general aircraft of Civil Aviation Industry now
Seat comfort degree measurement standard, for the passenger of standard stature, it is necessary to which a kind of aircraft seat comfort level is provided
Determination methods, targetedly calculate aircraft seat comfort level according to the height and weight data of different passengers, being capable of the trip of allowing
Visitor judges the seat comfort degree of aircraft according to the actual conditions of oneself, so that flight and cabin for selecting to be adapted to oneself etc., with
Further improve the flight experience of passenger.
The content of the invention
The present invention is exactly to relax in view of the deficienciess of the prior art, providing aircraft seat during a kind of passenger takes flight
The determination methods of appropriateness, can calculate aircraft seat comfort level according to the height and weight data of passenger, one is provided for passenger
Kind selects the scientific basis in flight and cabin etc., and that improves passenger seizes the opportunity experience.
To solve the above problems, the technical solution used in the present invention is as follows：
A kind of passenger takes the determination methods of aircraft seat comfort level during flight, comprises the following steps：
S1：According to the height and weight data of individual, standard stature index is calculated, whether individual is judged according to standard stature index
Belong to partially fat stature；
S2：The stature index correction factor of individual is calculated according to standard stature index；
S3：According to standard stature index, using the human body standard sitting posture hip breadth computational methods of ergonomics, the mark of human body is calculated
Quasi- sitting posture hip breadth；
S4：According to the height and weight data of individual, hip breadth correction factor is calculated；
S5：According to the standard sitting posture hip breadth and hip breadth correction factor of human body, individual human body sitting posture hip breadth is calculated；
S6：Aircraft seat width data table is searched, and according to standard stature index range, calculates seat width comfort level, and seat
When chair width comfort level refers to that people sits down on the seat, the distance under seat is empty；
S7：Judge whether seat width is suitable according to seat width comfort level criterion.
As the specific preferred of above-mentioned technical proposal, comprise the following steps：
S1：According to the height H of individual and weight W data, standard stature Index A is calculated：
A=W/H,
Stipulated that normal stature Index A 1：0<A≤0.35, abnormal stature Index A 2：A>0.35；
S2：Calculate the stature index correction factor B of individual：
B=A*10；
S3：According to the human body standard sitting posture hip breadth computational methods of ergonomics, the standard sitting posture hip breadth L of human body is calculated：
L=0.199*H；
S4：According to the height and weight data of individual, hip breadth correction factor C is calculated：
C=1.105*W-4.937*10H；
S5：Calculate the human body sitting posture hip breadth P of individual：
P=L+C；
S6：Aircraft seat width data table is searched, and according to standard stature index range, calculates seat width comfort level M, aircraft
Seat width is Q, then：
When 0<A≤0.35, M=Q-P,
Work as A>0.35, M=Q- (P+B)；
S7：Search seat width comfort level and describe the table of comparisons：
When M≤5, seat width is squeezed very much, may be had not enough seats for, uncomfortable, it is proposed that cabin is risen,
When 5<M<10, seat width is proper, if the travelling of long-distance flight is suggested rising cabin, improves seat comfort degree；
When M >=10, seat width is most suitable.
Compared with prior art, implementation result of the invention is as follows by the present invention：
A kind of passenger of the present invention takes the determination methods of aircraft seat comfort level during flight, can be according to different trips
The height and weight data of visitor, calculates the aircraft seat comfort level for multiplying flight, a kind of freight space intuitively quantified is provided for passenger
Feeling for taking, the important references condition of flight and cabin etc. is selected as passenger, improves the flight ride experience of passenger.
Embodiment
Illustrate present disclosure below in conjunction with specific embodiments.
The determination methods of aircraft seat comfort level during a kind of passenger seating flight that the present embodiment is provided, including with
Lower step：
Step 1. calculates standard stature index according to the height and weight data of individual：
If：Stature index is A, and individual height is H（Unit：cm）, whose body weight W（Unit：kg）,
Draw：A=W/H,
And provide normal stature Index A 1：0<A≤0.35, abnormal stature Index A 2：A>0.35.
Step 2. calculates the stature index correction factor of individual：
If：Stature index correction factor is B=A*10.
Step 3. calculates the standard sitting posture stern of human body according to the human body standard sitting posture hip breadth computational methods of ergonomics
It is wide：
If：The standard sitting posture hip breadth of human body is L（Unit：cm）,
Draw：L=0.199*H.
Step 4. calculates hip breadth correction factor according to the height and weight data of individual：
If：Hip breadth correction factor is C,
Draw：C=1.105*W-4.937*10H.
Step 5. calculates the human body sitting posture hip breadth of individual：
If：Human body sitting posture hip breadth is P（Unit：cm）,
Draw：P=L+C.
Step 6. searches aircraft seat width data table, and according to standard stature index range, it is comfortable to calculate seat width
Degree, i.e., when people sits down on the seat, the distance under seat is empty：
If：Seat width comfort level is M（Unit：cm）, aircraft seat width is Q（Unit：cm）,
Draw：
When 0<A≤0.35, M=Q-P,
Work as A>0.35, M=Q- (P+B).
Step 7. searches seat width comfort level and describes the table of comparisons：
When M≤5, seat width is squeezed very much, may be had not enough seats for, uncomfortable, it is proposed that cabin is risen,
When 5<M<10, seat width is proper, if the travelling of long-distance flight is suggested rising cabin, improves seat comfort degree；
When M >=10, seat width is most suitable.
A kind of passenger that the present embodiment is provided takes the determination methods of aircraft seat comfort level during flight, Neng Gougen
According to the height and weight data of different passengers, the aircraft seat comfort level for multiplying flight is calculated, is the freight space feeling for taking of passenger
A kind of important references condition directly perceived for quantifying determination methods, flight and cabin etc. being selected as passenger is provided, so that favorably
In the flight ride experience for improving passenger.
Above content is detailed description made for the present invention in conjunction with specific embodiments, it is impossible to assert that the present invention is specific real
Apply and be only limitted to these explanations.For those skilled in the art, before present inventive concept is not departed from
Put, some simple deduction or replace can also be made, should all be considered as belonging to the scope of protection of the invention.
Claims (2)
1. a kind of passenger takes the determination methods of aircraft seat comfort level during flight, it is characterized in that, comprise the following steps：
S1：According to the height and weight data of individual, standard stature index is calculated, whether individual is judged according to standard stature index
Belong to partially fat stature；
S2：The stature index correction factor of individual is calculated according to standard stature index；
S3：According to standard stature index, using the human body standard sitting posture hip breadth computational methods of ergonomics, the mark of human body is calculated
Quasi- sitting posture hip breadth；
S4：According to the height and weight data of individual, hip breadth correction factor is calculated；
S5：According to the standard sitting posture hip breadth and hip breadth correction factor of human body, individual human body sitting posture hip breadth is calculated；
S6：Aircraft seat width data table is searched, and according to standard stature index range, calculates seat width comfort level, and seat
When chair width comfort level refers to that people sits down on the seat, the distance under seat is empty；
S7：Judge whether seat width is suitable according to seat width comfort level criterion.
2. a kind of passenger as claimed in claim 1 takes the determination methods of aircraft seat comfort level during flight, its feature
It is to comprise the following steps：
S1：According to the height H of individual and weight W data, standard stature Index A is calculated：
A=W/H,
Stipulated that normal stature Index A 1：0<A≤0.35, abnormal stature Index A 2：A>0.35；
S2：Calculate the stature index correction factor B of individual：
B=A*10；
S3：According to the human body standard sitting posture hip breadth computational methods of ergonomics, the standard sitting posture hip breadth L of human body is calculated：
L=0.199*H；
S4：According to the height and weight data of individual, hip breadth correction factor C is calculated：
C=1.105*W-4.937*10H；
S5：Calculate the human body sitting posture hip breadth P of individual：
P=L+C；
S6：Aircraft seat width data table is searched, and according to standard stature index range, calculates seat width comfort level M, aircraft
Seat width is Q, then：
When 0<A≤0.35, M=Q-P,
Work as A>0.35, M=Q- (P+B)；
S7：Search seat width comfort level and describe the table of comparisons：
When M≤5, seat width is squeezed very much, may be had not enough seats for, uncomfortable, it is proposed that cabin is risen,
When 5<M<10, seat width is proper, if the travelling of long-distance flight is suggested rising cabin, improves seat comfort degree；
When M >=10, seat width is most suitable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711255317.XA CN108008762A (en) | 2017-12-03 | 2017-12-03 | A kind of passenger takes the determination methods of aircraft seat comfort level during flight |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711255317.XA CN108008762A (en) | 2017-12-03 | 2017-12-03 | A kind of passenger takes the determination methods of aircraft seat comfort level during flight |
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| CN108008762A true CN108008762A (en) | 2018-05-08 |
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| CN201711255317.XA Pending CN108008762A (en) | 2017-12-03 | 2017-12-03 | A kind of passenger takes the determination methods of aircraft seat comfort level during flight |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103010465A (en) * | 2011-09-27 | 2013-04-03 | 波音公司 | Aircraft seating systems |
| US20130328366A1 (en) * | 2012-06-07 | 2013-12-12 | B/E Aerospace, Inc. | Aircraft seating arrangement accommodating high-percentile hip widths |
| WO2014098620A1 (en) * | 2012-12-18 | 2014-06-26 | Serko Limited | Travel comfort index |
| CN104715380A (en) * | 2015-03-13 | 2015-06-17 | 深圳汇洁集团股份有限公司 | Clothing size calculating method |
-
2017
- 2017-12-03 CN CN201711255317.XA patent/CN108008762A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103010465A (en) * | 2011-09-27 | 2013-04-03 | 波音公司 | Aircraft seating systems |
| US20130328366A1 (en) * | 2012-06-07 | 2013-12-12 | B/E Aerospace, Inc. | Aircraft seating arrangement accommodating high-percentile hip widths |
| WO2014098620A1 (en) * | 2012-12-18 | 2014-06-26 | Serko Limited | Travel comfort index |
| CN104715380A (en) * | 2015-03-13 | 2015-06-17 | 深圳汇洁集团股份有限公司 | Clothing size calculating method |
Non-Patent Citations (1)
| Title |
|---|
| 杨光，黄毓瑜: "计算机辅助人机工程设计系统的研究", 《工程图学学报》 * |
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Application publication date: 20180508 |