US1072078A - Mechanism for aerial navigation. - Google Patents

Mechanism for aerial navigation. Download PDF

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Publication number
US1072078A
US1072078A US76909413A US1913769094A US1072078A US 1072078 A US1072078 A US 1072078A US 76909413 A US76909413 A US 76909413A US 1913769094 A US1913769094 A US 1913769094A US 1072078 A US1072078 A US 1072078A
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Prior art keywords
shafts
lifting
propellers
aerial navigation
propeller
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US76909413A
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Joseph H Beckwith
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage

Definitions

  • linrinonlal planes iyl'ierehy the entire rnerhanism may he raisei'l to and sustained at any desired altitude in the air, in combination with.
  • a nmnher oi devices Whose function generally is that of a parachute, which eoiiplarate with the sup porting and lifting mechanism to balance the machine. and Wherehy sudden falling or collapse of the machine will he prevented, anrl by which the machine only, in any instance, be lowered gently and safely" to the earth.
  • Figure l illustrates one emhodiment'of the invention.
  • Fig. 2 is a vertieal seelional View of the apper end of one of the vertical shafts which carry the lifting aml balancing devices.
  • Fig. 3 is a similar sectional view of the lower end of one of said shaltsi.
  • Fig. l is a plan "View of a. part of one of the lifting devices.
  • the open frame work 1 is oi any sniliahle construction adapted for these. purposes.
  • Said frame work supports, prefe'nhly near the middle part thereof.
  • a power or driving mechanism 2 which is arranged to rotate the shafts 8 extending toward the ends of the machine.
  • One ol sairl shafts earries a propeller wherehy the n'larhine will he driven through the air.
  • ll are eoimposml ol" senlions if snilnlile lalnie having lheir outer or lower inlgw; swnreil to rin s ll. llraees or reinl'oneinenh: [Ell may he nliliaeil to sti'l'aiglhen anrl hohl the rings ll.
  • said iii-ares having their inner eiirle serum-(l lo llllllji'l'lfl collars l ⁇ ; on the aha. .1: 7.
  • the shalls are linhular and have. holes 16 above the hlarlea 9 to HtlllllSlOIL 0E air untier the parts 10.
  • lhe devices 10 are a r angml above the hin'ivier famo Work and. therefore. not as halanees to n'event Mei-turning of the niaehimn and also are safeguards gainer 'apnl falling or collapse the combination with a frame Work, verlieal hollow shafts supported by said frame work.
  • a machine of the character described comprising a framework, a number of-v'ertical hollow rotating shafts, a permanently operable lifting propeller on each shaft, an'l'imber of permanently open -parachutes above said. propellers and above said frame work, said shafts having openings above and below said propellers effectively to conduct air from above said propellers to the under side thereof, a driving propeller, and power mechanism for operating said lifting propellers, said parachutes, and said driving /prop'eller, substantially as (specified.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Description

J. H. BECKWITH. MECHANISM FOR AERIAL NAVIGATION. APPLICATION FILED our. 12. mos. umnzwnn M AS. 1,072,078.
Patented Sept. 2, 1913.
ration.
i n tti i339 -ll. iii
finalisation is a spe gallon, o'l which the lollowinggij This ll'l'l'WlllHll has reference to aerial mivigalzon, llllll more partirnlarly' to that type of lllllllillllSlll for aerial navigation whii-h is heavier lhan llnair supporling; it. v anal whnch is raise-ll anal snpportl ll anal then. propelled in the operation againsl llnl nor of the (lriven mechanism,
The oliijeetml lhiinvenlis'in in to proilnee. in conneelion, with a snilahle 'l'ranie nnil propelling naval lllllF-Llil mounted l.ll.l'rl ll,llj i-- porting and lifting nieehanism emnprining a number of Cleric-es of the SOFCW"lJlUfHllliFl' type arranged to operate in. linrinonlal planes iyl'ierehy the entire rnerhanism may he raisei'l to and sustained at any desired altitude in the air, in combination with. a nmnher oi devices, Whose function generally is that of a parachute, which eoiiplarate with the sup porting and lifting mechanism to balance the machine. and Wherehy sudden falling or collapse of the machine will he prevented, anrl by which the machine only, in any instance, be lowered gently and safely" to the earth.
In the ai-eoinpanying drawings which form part of this specification, Figure l illustrates one emhodiment'of the invention. Fig. 2 is a vertieal seelional View of the apper end of one of the vertical shafts which carry the lifting aml balancing devices. Fig. 3, is a similar sectional view of the lower end of one of said shaltsi. Fig. l is a plan "View of a. part of one of the lifting devices.
The open frame work 1 .is oi any sniliahle construction adapted for these. purposes. Said frame work supports, prefe'nhly near the middle part thereof. a power or driving mechanism 2 which is arranged to rotate the shafts 8 extending toward the ends of the machine. One ol sairl shafts earries a propeller wherehy the n'larhine will he driven through the air. To each of :he shafts 3 a ;rear wheel is attar-hoil, saii'l gears being enmesheil with gm: 's 6 on the lower ends of the hollow oi lnhnlar rrrliieal shafts 7, lherehy rousing saii'l shafts to he rotate l when the power meehanisi'n in Specification of Letters; Patent.
ll ll lli lllllili ntenlrill iept. .23. 1191732 a1, will. Earl-a1 No. 769,094.
i in a il rrn'o lo, eraiiprnniiig in shape generally to that of :1 parachute, :unl subservinp; a like low-lion in hovering the machine to the earth. 'l'he ilerires ll are eoimposml ol" senlions if snilnlile lalnie having lheir outer or lower inlgw; swnreil to rin s ll. llraees or reinl'oneinenh: [Ell may he nliliaeil to sti'l'aiglhen anrl hohl the rings ll. in proper position, said iii-ares having their inner eiirle serum-(l lo llllllji'l'lfl collars l}; on the aha. .1: 7. Tie roils or r-ahles l-l eonneolinp revolving raps iii on the upper ends of the shafts 7 tonell'ier and with other parls of tho 1nachine iii-arr anil strengthen the structure. The shalls are linhular and have. holes 16 above the hlarlea 9 to HtlllllSlOIL 0E air untier the parts 10.
ll. will he observed that lhe devices 10 are a r angml above the hin'ivier famo Work and. therefore. not as halanees to n'event Mei-turning of the niaehimn and also are safeguards gainer 'apnl falling or collapse the combination with a frame Work, verlieal hollow shafts supported by said frame work. a lifting propeller on each of said verl'iral shalls, a pa 'aehnto on aeh of said shay s ahore said lifting propellers. said slnrlts lmi'in openings above and below naiil priniellers ell'eeliively to conduct air 'li'oin ahore saiil propellers to the miller sirle l'lil'fil'UlWf. and braces holding sairl vertical shal'ls from becoming; rhplarerl, of power rneehanisin, of a plurality of shafts lilinrs 9' on eaeh shaft Iii driven by said power mechanism, a driving propeller on one of said shafts, and gears entraining said last-named shafts with said vertical shafts whereby said lifting propellers and said paraeluitks will be driven when said driving propeller is operated, substantially zs specified.
2. Mechanism of the character described eomprisinga frame work, power mechanism on said frame work, a number of vertical hollow shafts rotated by said power meehanism, an open parachute on each of said shafts, and, a lifting propeller on each shaft below the parachute thereon said shafts avir openings above and below said pr0- pellers effectively to conduct air from above said propellers to the under sides thereof, substantially as specified.
3. A machine of the character described comprising a framework, a number of-v'ertical hollow rotating shafts, a permanently operable lifting propeller on each shaft, an'l'imber of permanently open -parachutes above said. propellers and above said frame work, said shafts having openings above and below said propellers effectively to conduct air from above said propellers to the under side thereof, a driving propeller, and power mechanism for operating said lifting propellers, said parachutes, and said driving /prop'eller, substantially as (specified.
ln testimony whereof I hereunto affix my signature this 9th day of September, 1908, in the presence of two witnesses.
J ()SEPH H. BEGKWITH. [1 s.]- VVitnesses I FRANKLIN MILLER,
\V. B. HAYS,
US76909413A 1913-05-21 1913-05-21 Mechanism for aerial navigation. Expired - Lifetime US1072078A (en)

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US76909413A US1072078A (en) 1913-05-21 1913-05-21 Mechanism for aerial navigation.

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US76909413A US1072078A (en) 1913-05-21 1913-05-21 Mechanism for aerial navigation.

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2555162A1 (en) * 2014-06-24 2015-12-29 Fº JAVIER PORRAS VILA Airplane with double counter-clockwise propellers, and domes (Machine-translation by Google Translate, not legally binding)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2555162A1 (en) * 2014-06-24 2015-12-29 Fº JAVIER PORRAS VILA Airplane with double counter-clockwise propellers, and domes (Machine-translation by Google Translate, not legally binding)

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