US1000252A - Aeroplane. - Google Patents

Aeroplane. Download PDF

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Publication number
US1000252A
US1000252A US58795210A US1910587952A US1000252A US 1000252 A US1000252 A US 1000252A US 58795210 A US58795210 A US 58795210A US 1910587952 A US1910587952 A US 1910587952A US 1000252 A US1000252 A US 1000252A
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US
United States
Prior art keywords
frame
aeroplane
gardner
plane
shaft
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.)
Expired - Lifetime
Application number
US58795210A
Inventor
Robert F Gardner
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Individual
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Individual
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Publication date
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Priority to US58795210A priority Critical patent/US1000252A/en
Application granted granted Critical
Publication of US1000252A publication Critical patent/US1000252A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile

Definitions

  • a propeller 37 Connected toV the shaft of the motor 35 is a propeller 37, through the instrumentality of which the aeroplane is driven.
  • the various parts of the frame A are strengthened by means of. steel stay wires connected to' the frame at t-he most advantageous points and constructed with a view to lightness'andstrength.
  • An aeroplane comprising a frame, ⁇ a. supporting plane carried by said frame, lifting planes pivotally mounted in said frame and disposedl at each end of the supporting plane, a tubular member having an intermediate portion thereof pivotally connected to the frame and provided with a transverse opening above its pivot point interrupted by other end connected respectively to the lift,-

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Harvesting Machines For Specific Crops (AREA)

Description

R. I'. GARDNER.
AEROPLANE.
APPLICATION FILED 00119, 1910 42l,OOC ),252.I Patented Aug. 8, 1911 4 SHBETMEHEET 1.
TIE?. l
lI mw l RP.GARDNER{ AEROPLANB.
APPLICATION FILED OCT. 19. 1910.
1 ,000,252. lPatented Aug. 8, 1,911.
4 BHEETi-BHEET 2. l
n. 1". GARDNER. i AEBPLANE. l APPLIOATION ILED OUT. 19:1910
Patented Aug. 8, 1911.
4 sums-sum a.
fader/LI mnef,
R- I'. GARDNER.'
im@ @am able pulleys in the frame A and are Secured to the tubular member 26 at a point above its pivotal connection with the frame A. The steering plane is provided with a cross arm 32 transverse to its axisof rotation and this cross arm has its terminals connected to the shaft 28 by means of cables 33 which extend through the opening 27 so that the rotation of said shaft by the operation of the hand Wheel 29 will in turn rotate the steering plane 25 in order to chan e the direction of the aeroplane during ight. 'By this construction, it will. be apparent that boththe lifting planes and the steering' plane are under the control of the operator when his hands are upon the hand Wheel 29 as he can then effect b'oth the "the motor 354 and the operators seat 36.
Connected toV the shaft of the motor 35 is a propeller 37, through the instrumentality of which the aeroplane is driven.
The various parts of the frame A are strengthened by means of. steel stay wires connected to' the frame at t-he most advantageous points and constructed with a view to lightness'andstrength.
What is claimed is An aeroplane comprising a frame,^ a. supporting plane carried by said frame, lifting planes pivotally mounted in said frame and disposedl at each end of the supporting plane, a tubular member having an intermediate portion thereof pivotally connected to the frame and provided with a transverse opening above its pivot point interrupted by other end connected respectively to the lift,-
ing planes whereby the rocking 0f the tubular member'on its pivot will move said 1ift ing planes so as to present different angles of incidence to the atmosphere, a vertical steering plane pivoted in the frame, and connections ,between'the' steering lanes and the shaft whereby the rotation o the latter Will move said steering plane-on its pivot,
said connections leading to the shaft through the transverse opening 1n the tubular inember.
In testimony whereof, I affix my signature', in presence oftwo witnesses.
y ROBERT GARDNER. Witnesses: F. P. OHARA,
N. E. RFDDAN.y
the latter, a pair
US58795210A 1910-10-19 1910-10-19 Aeroplane. Expired - Lifetime US1000252A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US58795210A US1000252A (en) 1910-10-19 1910-10-19 Aeroplane.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US58795210A US1000252A (en) 1910-10-19 1910-10-19 Aeroplane.

Publications (1)

Publication Number Publication Date
US1000252A true US1000252A (en) 1911-08-08

Family

ID=3068578

Family Applications (1)

Application Number Title Priority Date Filing Date
US58795210A Expired - Lifetime US1000252A (en) 1910-10-19 1910-10-19 Aeroplane.

Country Status (1)

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US (1) US1000252A (en)

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