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第12章

flying machines-第12章

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without adding materially to the gross weight of

the framework and equipment minus passengers。



How to Distribute the Weight。



Let us take 1;030 pounds as the net weight of the machine

as against the same average in the Wright and

Curtiss machines。 Now comes the question of distributing

this weight between the framework; motor; and

other equipment。 As a general proposition the framework

should weigh about twice as much as the complete

power plant (this is for amateur work)。



The word 〃framework〃 indicates not only the wooden

frames of the main planes; auxiliary planes; rudders;

etc。; but the cloth coverings as welleverything in fact

except the engine and propeller。



On the basis named the framework would weigh 686

pounds; and the power plant 344。 These figures are

liberal; and the results desired may be obtained well

within them as the novice will learn as he makes progress

in the work。



Figuring on Surface Area。



It was Prof。 Langley who first brought into prominence

in connection with flying machine construction the

mathematical principle that the larger the object the

smaller may be the relative area of support。 As explained

in Chapter XIII; there are mechanical limits as

to size which it is not practical to exceed; but the main

principle remains in effect。



Take two aeroplanes of marked difference in area of

surface。 The larger will; as a rule; sustain a greater

weight in relative proportion to its area than the smaller

one; and do the work with less relative horsepower。 As

a general thing well…constructed machines will average

a supporting capacity of one pound for every one…half

square foot of surface area。 Accepting this as a working

rule we find that to sustain a weight of 1;200 pounds

machine and two passengerswe should have 600

square feet of surface。



Distributing the Surface Area。



The largest surfaces now in use are those of the

Wright; Voisin and Antoinette machines538 square

feet in each。 The actual sustaining power of these machines;

so far as known; has never been tested to the

limit; it is probable that the maximum is considerably

in excess of what they have been called upon to show。

In actual practice the average is a little over one pound

for each one…half square foot of surface area。



Allowing that 600 square feet of surface will be used;

the next question is how to distribute it to the best

advantage。 This is another important matter in which

individual preference must rule。 We have seen how

the professionals disagree on this point; some using

auxiliary planes of large size; and others depending upon

smaller auxiliaries with an increase in number so as to

secure on a different plan virtually the same amount of

surface。



In deciding upon this feature the best thing to do is

to follow the plans of some successful aviator; increasing

the area of the auxiliaries in proportion to the increase

in the area of the main planes。 Thus; if you use 600

square feet of surface where the man whose plans you

are following uses 500; it is simply a matter of making

your planes one…fifth larger all around。



The Cost of Production。



Cost of production will be of interest to the amateur

who essays to construct a flying machine。 Assuming

that the size decided upon is double that of the glider

the material for the framework; timber; cloth; wire; etc。;

will cost a little more than double。 This is because it

must be heavier in proportion to the increased size of

the framework; and heavy material brings a larger price

than the lighter goods。 If we allow 20 as the cost of

the glider material it will be safe to put down the cost

of that required for a real flying machine framework

at 60; provided the owner builds it himself。



As regards the cost of motor and similar equipment

it can only be said that this depends upon the selection

made。 There are some reliable aviation motors which

may be had as low as 500; and there are others which

cost as much as 2;000。



Services of Expert Necessary。



No matter what kind of a motor may be selected the

services of an expert will be necessary in its proper

installation unless the amateur has considerable genius

in this line himself。 As a general thing 25 should be

a liberal allowance for this work。 No matter how carefully

the engine may be placed and connected it will be

largely a matter of luck if it is installed in exactly the

proper manner at the first attempt。 The chances are

that several alterations; prompted by the results of trials;

will have to be made。 If this is the case the expert's bill may

readily run up to 50。 If the amateur is competent to do this

part of the work the entire item of 50 may; of course; be cut

out。



As a general proposition a fairly satisfactory flying machine;

one that will actually fly and carry the operator with it; may be

constructed for 750; but it will lack the better qualities which

mark the higher priced machines。 This computation is made on

the basis of 60 for material; 50 for services of expert; 600

for motor; etc。; and an allowance of 40 for extras。



No man who has the flying machine germ in his system will be long

satisfied with his first moderate price machine; no matter how

well it may work。 It's the old story of the automobile 〃bug〃

over again。 The man who starts in with a modest 1;000 automobile

invariably progresses by easy stages to the 4;000 or 5;000

class。 The natural tendency is to want the biggest and best

attainable within the financial reach of the owner。



It's exactly the same way with the flying machine

convert。 The more proficient he becomes in the manipulation

of his car; the stronger becomes the desire to fly

further and stay in the air longer than the rest of his

brethren。 This necessitates larger; more powerful; and

more expensive machines as the work of the germ progresses。



Speed Affects Weight Capacity。



Don't overlook the fact that the greater speed you

can attain the smaller will be the surface area you can

get along with。 If a machine with 500 square feet of

sustaining surface; traveling at a speed of 40 miles an

hour; will carry a weight of 1;200 pounds; we can cut

the sustaining surface in half and get along with 250

square feet; provided a speed of 60 miles an hour can

be obtained。 At 100 miles an hour only 80 square feet

of surface area would be required。 In both instances the

weight sustaining capacity will remain the same as with

the 500 square feet of surface area1;200 pounds。



One of these days some mathematical genius will

figure out this problem with exactitude and we will have

a dependable table giving the maximum carrying capacity

of various surface areas at various stated speeds;

based on the dimensions of the advancing edges。 At

present it is largely a matter of guesswork so far as

making accurate computation goes。 Much depends upon

the shape of the machine; and the amount of surface

offering resistance to the wind; etc。







CHAPTER IX。



SELECTION OF THE MOTOR。



Motors for flying machines must be light in weight;

of great strength; productive of extreme speed; and

positively dependable in action。 It matters little

as to the particular form; or whether air or

water cooled; so long as the four features named are

secured。 There are at least a dozen such motors or

engines now in use。 All are of the gasolene type; and

all possess in greater or lesser degree the desired qualities。

Some of these motors are:



Renault8…cylinder; air…cooled; 50 horse power;

weight 374 pounds。



Fiat8…cylinder; air…cooled; 50 horse power; weight

150 pounds。



Farcot8…cylinder; air…cooled; from 30 to 100 horse

power; according to bore of cylinders; weight of smallest;

84 pounds。



R。 E。 P。10…cylinder; air…cooled; 150 horse power;

weight 215 pounds。



Gnome7 and 14 cylinders; revolving type; air…cool

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