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aforesaid¡¡by¡¡the¡¡Aero¡¡Club¡¡of¡¡America

by¡¡granting¡¡licenses¡¡to¡¡promoters¡¡who¡¡make¡¡satisfactory

arrangements¡¡with¡¡the¡¡company¡¡for¡¡its¡¡compensation

for¡¡the¡¡use¡¡of¡¡its¡¡patents¡£¡¡At¡¡such¡¡licensed¡¡meet¡¡any

machine¡¡of¡¡any¡¡make¡¡may¡¡participate¡¡freely¡¡without

securing¡¡any¡¡further¡¡license¡¡or¡¡permit¡£¡¡The¡¡details¡¡and

terms¡¡of¡¡all¡¡meets¡¡will¡¡be¡¡arranged¡¡by¡¡the¡¡committee

having¡¡in¡¡charge¡¡the¡¡interests¡¡of¡¡both¡¡organizations¡£







CHAPTER¡¡XXIV¡£



HINTS¡¡ON¡¡PROPELLER¡¡CONSTRUCTION¡£



Every¡¡professional¡¡aviator¡¡has¡¡his¡¡own¡¡ideas¡¡as¡¡to¡¡the

design¡¡of¡¡the¡¡propeller£»¡¡one¡¡of¡¡the¡¡most¡¡important¡¡features

of¡¡flying¡­machine¡¡construction¡£¡¡While¡¡in¡¡many

instances¡¡the¡¡propeller£»¡¡at¡¡a¡¡casual¡¡glance£»¡¡may¡¡appear

to¡¡be¡¡identical£»¡¡close¡¡inspection¡¡will¡¡develop¡¡the¡¡fact¡¡that

in¡¡nearly¡¡every¡¡case¡¡some¡¡individual¡¡idea¡¡of¡¡the¡¡designer

has¡¡been¡¡incorporated¡£¡¡Thus£»¡¡two¡¡propellers¡¡of¡¡the¡¡two¡­

bladed¡¡variety£»¡¡while¡¡of¡¡the¡¡same¡¡general¡¡size¡¡as¡¡to

length¡¡and¡¡width¡¡of¡¡blade£»¡¡will¡¡vary¡¡greatly¡¡as¡¡to¡¡pitch

and¡¡¡¨twist¡¨¡¡or¡¡curvature¡£



What¡¡the¡¡Designers¡¡Seek¡£



Every¡¡designer¡¡is¡¡seeking¡¡for¡¡the¡¡same¡¡resultthe

securing¡¡of¡¡the¡¡greatest¡¡possible¡¡thrust£»¡¡or¡¡air¡¡displacement£»

with¡¡the¡¡least¡¡possible¡¡energy¡£



The¡¡angles¡¡of¡¡any¡¡screw¡¡propeller¡¡blade¡¡having¡¡a

uniform¡¡or¡¡true¡¡pitch¡¡change¡¡gradually¡¡for¡¡every¡¡increased

diameter¡£¡¡In¡¡order¡¡to¡¡give¡¡a¡¡reasonably¡¡clear

explanation£»¡¡it¡¡will¡¡be¡¡well¡¡to¡¡review¡¡in¡¡a¡¡primary¡¡way

some¡¡of¡¡the¡¡definitions¡¡or¡¡terms¡¡used¡¡in¡¡connection¡¡with

and¡¡applied¡¡to¡¡screw¡¡propellers¡£



Terms¡¡in¡¡General¡¡Use¡£



Pitch¡£The¡¡term¡¡¡¨pitch£»¡¨¡¡as¡¡applied¡¡to¡¡a¡¡screw¡¡propeller£»

is¡¡the¡¡theoretical¡¡distance¡¡through¡¡which¡¡it¡¡would

travel¡¡without¡¡slip¡¡in¡¡one¡¡revolution£»¡¡and¡¡as¡¡applied¡¡to

a¡¡propeller¡¡blade¡¡it¡¡is¡¡the¡¡angle¡¡at¡¡which¡¡the¡¡blades¡¡are

set¡¡so¡¡as¡¡to¡¡enable¡¡them¡¡to¡¡travel¡¡in¡¡a¡¡spiral¡¡path¡¡through

a¡¡fixed¡¡distance¡¡theoretically¡¡without¡¡slip¡¡in¡¡one¡¡revolution¡£



Pitch¡¡speed¡£The¡¡term¡¡¡¨pitch¡¡speed¡¨¡¡of¡¡a¡¡screw

propeller¡¡is¡¡the¡¡speed¡¡in¡¡feet¡¡multiplied¡¡by¡¡the¡¡number¡¡of

revolutions¡¡it¡¡is¡¡caused¡¡to¡¡make¡¡in¡¡one¡¡minute¡¡of¡¡time¡£

If¡¡a¡¡screw¡¡propeller¡¡is¡¡revolved¡¡600¡¡times¡¡per¡¡minute£»

and¡¡if¡¡its¡¡pitch¡¡is¡¡7¡¡ft¡££»¡¡then¡¡the¡¡pitch¡¡speed¡¡of¡¡such¡¡a

propeller¡¡would¡¡be¡¡7x600¡¡revolutions£»¡¡or¡¡4200¡¡ft¡£¡¡per

minute¡£



Uniform¡¡pitch¡£A¡¡true¡¡pitch¡¡screw¡¡propeller¡¡is¡¡one

having¡¡its¡¡blades¡¡formed¡¡in¡¡such¡¡a¡¡manner¡¡as¡¡to¡¡enable

all¡¡of¡¡its¡¡useful¡¡portions£»¡¡from¡¡the¡¡portion¡¡nearest¡¡the

hub¡¡to¡¡its¡¡outer¡¡portion£»¡¡to¡¡travel¡¡at¡¡a¡¡uniform¡¡pitch

speed¡£¡¡Or£»¡¡in¡¡other¡¡words£»¡¡the¡¡pitch¡¡is¡¡uniform¡¡when¡¡the

projected¡¡area¡¡of¡¡the¡¡blade¡¡is¡¡parallel¡¡along¡¡its¡¡full

length¡¡and¡¡at¡¡the¡¡same¡¡time¡¡representing¡¡a¡¡true¡¡sector

of¡¡a¡¡circle¡£



All¡¡screw¡¡propellers¡¡having¡¡a¡¡pitch¡¡equal¡¡to¡¡their

diameters¡¡have¡¡the¡¡same¡¡angle¡¡for¡¡their¡¡blades¡¡at¡¡their

largest¡¡diameter¡£



When¡¡Pitch¡¡Is¡¡Not¡¡Uniform¡£



A¡¡screw¡¡propeller¡¡not¡¡having¡¡a¡¡uniform¡¡pitch£»¡¡but

having¡¡the¡¡same¡¡angle¡¡for¡¡all¡¡portions¡¡of¡¡its¡¡blades£»¡¡or

some¡¡arbitrary¡¡angle¡¡not¡¡a¡¡true¡¡pitch£»¡¡is¡¡distinguished

from¡¡one¡¡having¡¡a¡¡true¡¡pitch¡¡in¡¡the¡¡variation¡¡of¡¡the¡¡pitch

speeds¡¡that¡¡the¡¡various¡¡portions¡¡of¡¡its¡¡blades¡¡are¡¡forced

to¡¡travel¡¡through¡¡while¡¡traveling¡¡at¡¡its¡¡maximum¡¡pitch

speed¡£



On¡¡this¡¡subject¡¡Mr¡£¡¡R¡£¡¡W¡£¡¡Jamieson¡¡says¡¡in¡¡Aeronautics£º



¡¨Take¡¡for¡¡example¡¡an¡¡8¡­foot¡¡screw¡¡propeller¡¡having¡¡an

8¡­foot¡¡pitch¡¡at¡¡its¡¡largest¡¡diameter¡£¡¡If¡¡the¡¡angle¡¡is¡¡the

same¡¡throughout¡¡its¡¡entire¡¡blade¡¡length£»¡¡then¡¡all¡¡the¡¡porions

of¡¡its¡¡blades¡¡approaching¡¡the¡¡hub¡¡from¡¡its¡¡outer¡¡portion¡¡would

have¡¡a¡¡gradually¡¡decreasing¡¡pitch¡£¡¡The¡¡2¡­foot

portion¡¡would¡¡have¡¡a¡¡2¡­foot¡¡pitch£»¡¡the¡¡3¡­foot¡¡portion¡¡a¡¡3¡­

foot¡¡pitch£»¡¡and¡¡so¡¡on¡¡to¡¡the¡¡8¡­foot¡¡portion¡¡which¡¡would

have¡¡an¡¡8¡­foot¡¡pitch¡£¡¡When¡¡this¡¡form¡¡of¡¡propeller¡¡is

caused¡¡to¡¡revolve£»¡¡say¡¡500¡¡r¡£p¡£m¡££»¡¡the¡¡8¡­foot¡¡portion¡¡would

have¡¡a¡¡calculated¡¡pitch¡¡speed¡¡of¡¡8¡¡feet¡¡by¡¡500¡¡revolutions£»

or¡¡4£»000¡¡feet¡¡per¡¡min¡££»¡¡while¡¡the¡¡2¡­foot¡¡portion¡¡would

have¡¡a¡¡calculated¡¡pitch¡¡speed¡¡of¡¡500¡¡revolutions¡¡by¡¡2¡¡feet£»

or¡¡1£»000¡¡feet¡¡per¡¡minute¡£



Effect¡¡of¡¡Non¡­Uniformity¡£



¡¨Now£»¡¡as¡¡all¡¡of¡¡the¡¡portions¡¡of¡¡this¡¡type¡¡of¡¡screw

propeller¡¡must¡¡travel¡¡at¡¡some¡¡pitch¡¡speed£»¡¡which¡¡must¡¡have

for¡¡its¡¡maximum¡¡a¡¡pitch¡¡speed¡¡in¡¡feet¡¡below¡¡the¡¡calculated

pitch¡¡speed¡¡of¡¡the¡¡largest¡¡diameter£»¡¡it¡¡follows¡¡that

some¡¡portions¡¡of¡¡its¡¡blades¡¡would¡¡perform¡¡useful¡¡work

while¡¡the¡¡action¡¡of¡¡the¡¡other¡¡portions¡¡would¡¡be¡¡negative

resisting¡¡the¡¡forward¡¡motion¡¡of¡¡the¡¡portions¡¡having¡¡a

greater¡¡pitch¡¡speed¡£¡¡The¡¡portions¡¡having¡¡a¡¡pitch¡¡speed

below¡¡that¡¡at¡¡which¡¡the¡¡screw¡¡is¡¡traveling¡¡cease¡¡to¡¡perform

useful¡¡work¡¡after¡¡their¡¡pitch¡¡speed¡¡has¡¡been¡¡exceeded

by¡¡the¡¡portions¡¡having¡¡a¡¡larger¡¡diameter¡¡and¡¡a

greater¡¡pitch¡¡speed¡£



¡¨We¡¡might¡¡compare¡¡the¡¡larger¡¡and¡¡smaller¡¡diameter

portions¡¡of¡¡this¡¡form¡¡of¡¡screw¡¡propeller£»¡¡to¡¡two¡¡power¡­

driven¡¡vessels¡¡connected¡¡with¡¡a¡¡line£»¡¡one¡¡capable¡¡of¡¡traveling

20¡¡miles¡¡per¡¡hour£»¡¡the¡¡other¡¡10¡¡miles¡¡per¡¡hour¡£¡¡It

can¡¡be¡¡readily¡¡understood¡¡that¡¡the¡¡boat¡¡capable¡¡of¡¡traveling

10¡¡miles¡¡per¡¡hour¡¡would¡¡have¡¡no¡¡useful¡¡effect¡¡to

help¡¡the¡¡one¡¡traveling¡¡20¡¡miles¡¡per¡¡hour£»¡¡as¡¡its¡¡action

would¡¡be¡¡such¡¡as¡¡to¡¡impose¡¡a¡¡dead¡¡load¡¡upon¡¡the¡¡latter's

progress¡£¡¨



The¡¡term¡¡¡¨slip£»¡¨¡¡as¡¡applied¡¡to¡¡a¡¡screw¡¡propeller£»¡¡is¡¡the

distance¡¡between¡¡its¡¡calculated¡¡pitch¡¡speed¡¡and¡¡the¡¡actual

distance¡¡it¡¡travels¡¡through¡¡under¡¡load£»¡¡depending¡¡upon

the¡¡efficiency¡¡and¡¡proportion¡¡of¡¡its¡¡blades¡¡and¡¡the¡¡amount

of¡¡load¡¡it¡¡has¡¡to¡¡carry¡£



The¡¡action¡¡of¡¡a¡¡screw¡¡propeller¡¡while¡¡performing¡¡useful

work¡¡might¡¡be¡¡compared¡¡to¡¡a¡¡nut¡¡traveling¡¡on¡¡a

threaded¡¡bolt£»¡¡little¡¡resistance¡¡is¡¡offered¡¡to¡¡its¡¡forward

motion¡¡while¡¡it¡¡spins¡¡freely¡¡without¡¡load£»¡¡but¡¡give¡¡it¡¡a

load¡¡to¡¡carry£»¡¡then¡¡it¡¡will¡¡take¡¡more¡¡power¡¡to¡¡keep¡¡up¡¡its

speed£»¡¡if¡¡too¡¡great¡¡a¡¡load¡¡is¡¡applied¡¡the¡¡thread¡¡will¡¡strip£»

and¡¡so¡¡it¡¡is¡¡with¡¡a¡¡screw¡¡propeller¡¡gliding¡¡spirally¡¡on¡¡the

air¡£¡¡A¡¡propeller¡¡traveling¡¡without¡¡load¡¡on¡¡to¡¡new¡¡air

might¡¡be¡¡compared¡¡to¡¡the¡¡nut¡¡traveling¡¡freely¡¡on¡¡the¡¡bolt¡£

It¡¡would¡¡consume¡¡but¡¡little¡¡power¡¡and¡¡it¡¡would¡¡travel¡¡at

nearly¡¡its¡¡calculated¡¡pitch¡¡speed£»¡¡but¡¡give¡¡it¡¡work¡¡to¡¡do

and¡¡then¡¡it¡¡will¡¡take¡¡power¡¡to¡¡drive¡¡it¡£



There¡¡is¡¡a¡¡reaction¡¡caused¡¡from¡¡the¡¡propeller¡¡projecting

air¡¡backward¡¡when¡¡it¡¡slips£»¡¡which£»¡¡together¡¡with¡¡the¡¡supporting

effect¡¡of¡¡the¡¡blades£»¡¡combine¡¡to¡¡produce¡¡useful

work¡¡or¡¡pull¡¡on¡¡the¡¡object¡¡to¡¡be¡¡carried¡£



A¡¡screw¡¡propeller¡¡working¡¡under¡¡load¡¡approaches¡¡more

closely¡¡to¡¡its¡¡maximum¡¡efficiency¡¡as¡¡it¡¡carries¡¡its¡¡load

with¡¡a¡¡minimum¡¡amount¡¡of¡¡slip£»¡¡or¡¡nearing¡¡its¡¡calculated

pitch¡¡speed¡£



Why¡¡Blades¡¡Are¡¡Curved¡£



It¡¡has¡¡been¡¡pointed¡¡out¡¡by¡¡experiment¡¡that¡¡certain

forms¡¡of¡¡curved¡¡surfaces¡¡as¡¡applied¡¡to¡¡aeroplanes¡¡will¡¡lift

more¡¡per¡¡horse¡¡power£»¡¡per¡¡unit¡¡of¡¡square¡¡foot£»¡¡while¡¡on

the¡¡other¡¡hand¡¡it¡¡has¡¡been¡¡shown¡¡that¡¡a¡¡flat¡¡surface¡¡will

lift¡¡more¡¡per¡¡horse¡¡power£»¡¡but¡¡requires¡¡more¡¡area¡¡of¡¡surface

to¡¡do¡¡it¡£



As¡¡a¡¡true¡¡pitch¡¡screw¡¡propeller¡¡is¡¡virtually¡¡a¡¡rotating

aeroplane£»¡¡a¡¡curved¡¡surface¡¡may¡¡be¡¡advantageously¡¡employed

when¡¡the¡¡limit¡¡of¡¡size¡¡prevents¡¡using¡¡large¡¡plane

surfaces¡¡for¡¡the¡¡blades¡£



Care¡¡should¡¡be¡¡exercised¡¡in¡¡keeping¡¡the¡¡chord¡¡of¡¡any

curve¡¡to¡¡be¡¡used¡¡for¡¡the¡¡blades¡¡at¡¡the¡¡proper¡¡pitch¡¡angle£»

and¡¡in¡¡all¡¡cases¡¡propeller¡¡blades¡¡should¡¡be¡¡made¡¡rigid¡¡so

as¡¡to¡¡preserve¡¡the¡¡true¡¡angle¡¡and¡¡not¡¡be¡¡distorted¡¡by

centrifugal¡¡force¡¡or¡¡from¡¡any¡¡other¡¡cause£»¡¡as¡¡flexibility

will¡¡seriously¡¡affect¡¡their¡¡pitch¡¡speed¡¡and¡¡otherwise¡¡affect

their¡¡efficiency¡£



How¡¡to¡¡Determine¡¡Angle¡£



To¡¡find¡¡the¡¡angle¡¡for¡¡the¡¡proper¡¡pitch¡¡at¡¡any¡¡point¡¡in

the¡¡diameter¡¡of¡¡a¡¡propeller£»¡¡determine¡¡the¡¡circumference

by¡¡multiplying¡¡the¡¡diameter¡¡by¡¡3¡£1416£»¡¡which¡¡represent

by¡¡drawing¡¡a¡¡line¡¡to¡¡scale¡¡in¡¡feet¡£¡¡At¡¡the¡¡end¡¡of¡¡this¡¡line

draw¡¡another¡¡line¡¡to¡¡represent¡¡the¡¡desired¡¡pitch¡¡in¡¡feet¡£

Then¡¡draw¡¡a¡¡line¡¡from¡¡the¡¡point¡¡representing¡¡the¡¡desired

pitch¡¡in¡¡feet¡¡to¡¡the¡¡beginning¡¡of¡¡the¡¡circumference¡¡line¡£

For¡¡example£º



If¡¡the¡¡propeller¡¡to¡¡be¡¡laid¡¡out¡¡is¡¡7¡¡feet¡¡in¡¡diameter£»¡¡and

is¡¡to¡¡have¡¡a¡¡7¡­foot¡¡pitch£»¡¡the¡¡circumference¡¡will¡¡be¡¡21¡£99

feet¡£¡¡Draw¡¡a¡¡diagram¡¡representing¡¡the¡¡circumference

line¡¡and¡¡pitch¡¡in¡¡feet¡£¡¡If¡¡this¡¡diagram¡¡is¡¡wrapped¡¡around

a¡¡cylinder¡¡the¡¡angle¡¡line¡¡will¡¡represent¡¡a¡¡true¡¡thread¡¡7

feet¡¡in¡¡diameter¡¡and¡¡7¡¡feet¡¡long£»¡¡and¡¡the¡¡angle¡¡of¡¡the

thread¡¡will¡¡be¡¡17¡¡3/4¡¡degrees¡£



Relation¡¡of¡¡Diameter¡¡to¡¡Circumference¡£



Since¡¡the¡¡areas¡¡of¡¡circles¡¡decrease¡¡as¡¡the¡¡diameter

lessens£»¡¡it¡¡follows¡¡that¡¡if¡¡a¡¡propeller¡¡is¡¡to¡¡travel¡¡at¡¡a¡¡uniform

pitch¡¡speed£»¡¡the¡¡volume¡¡of¡¡its¡¡blade¡¡displacement

should¡¡decrease¡¡as¡¡its¡¡diameter¡¡becomes¡¡less£»¡¡so¡¡as¡¡to

occupy¡¡a¡¡corresponding¡¡relation¡¡to¡¡the¡¡circumferences¡¡of

larger¡¡diameters£»¡¡and¡¡at¡¡the¡¡same¡¡time¡¡the¡¡projected

area¡¡of¡¡the¡¡blade¡¡must¡¡be¡¡parallel¡¡along¡¡its¡¡full¡¡length

and¡¡should¡¡represent¡¡a¡¡true¡¡sector¡¡of¡¡a¡¡circle¡£



Let¡¡us¡¡suppose¡¡a¡¡7¡­foot¡¡circle¡¡to¡¡be¡¡divided¡¡into¡¡20

sectors£»¡¡one¡¡of¡¡which¡¡represents¡¡a¡¡propeller¡¡blade¡£¡¡If¡¡the

pitch¡¡is¡¡to¡¡be¡¡7¡¡feet£»¡¡then¡¡the¡¡greatest¡¡depth¡¡of¡¡the¡¡angle

would¡¡be¡¡1/20¡¡part¡¡of¡¡the¡¡pitch£»¡¡or¡¡4¡¡2/10¡¡inch¡£¡¡If¡¡the

line¡¡representing¡¡the¡¡greatest¡¡depth¡¡of¡¡the¡¡angle¡¡is¡¡kept

the¡¡same¡¡width¡¡as¡¡it¡¡approaches¡¡the¡¡hub£»¡¡the¡¡pitch¡¡will

be¡¡uniform¡£¡¡If¡¡the¡¡blade¡¡is¡¡set¡¡at¡¡an¡¡angle¡¡so¡¡its¡¡projected

area¡¡is¡¡1/20¡¡part¡¡of¡¡the¡¡pitch£»¡¡and¡¡if¡¡it¡¡is¡¡moved

through¡¡20¡¡divisions¡¡for¡¡one¡¡revolution£»¡¡it¡¡would¡¡have¡¡a

travel¡¡of¡¡7¡¡feet¡£







CHAPTER¡¡XXV¡£



NEW¡¡MOTORS¡¡AND¡¡DEVICES¡£



Since¡¡the¡¡first¡¡edition¡¡of¡¡this¡¡book¡¡was¡¡printed£»¡¡early¡¡in¡¡1910£»

there¡¡has¡¡been¡¡a¡¡remarkable¡¡advance¡¡in¡¡the¡¡construction¡¡of

aeroplane¡¡motors£»¡¡which¡¡has¡¡resulted¡¡in¡¡a¡¡wonderful¡¡decrease

in¡¡the¡¡amount¡¡of¡¡surface¡¡area¡¡from¡¡that¡¡formerly¡¡required¡£

Marked¡¡gain¡¡in¡¡lightness¡¡and¡¡speed¡¡of¡¡the¡¡motor¡¡has¡¡enabled

aviators¡¡to¡¡get¡¡along£»¡¡in¡¡some¡¡instances£»¡¡with¡¡one¡­quarter¡¡of

the¡¡plane¡¡supporting¡¡area¡¡previously¡¡used¡£¡¡The¡¡first¡¡Wright

biplane£»¡¡propelled¡¡by¡¡a¡¡motor¡¡of¡¡25¡¡h¡£p¡££»¡¡productive¡¡of¡¡a¡¡fair

average¡¡speed¡¡of¡¡30¡¡miles¡¡an¡¡hour£»¡¡had¡¡a¡¡plane¡¡surface¡¡of¡¡538

square¡¡feet¡£¡¡Now£»¡¡by¡¡using¡¡a¡¡specially¡¡designed¡¡motor¡¡of¡¡65

h¡£¡¡p¡££»¡¡capable¡¡of¡¡developing¡¡a¡¡speed¡¡of¡¡from¡¡
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