[go: up one dir, main page]

US1409241A - Aeroplane - Google Patents

Aeroplane Download PDF

Info

Publication number
US1409241A
US1409241A US446252A US44625221A US1409241A US 1409241 A US1409241 A US 1409241A US 446252 A US446252 A US 446252A US 44625221 A US44625221 A US 44625221A US 1409241 A US1409241 A US 1409241A
Authority
US
United States
Prior art keywords
planes
aeroplane
lifting
aeroplanes
angle
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
US446252A
Inventor
Ira B Sanders
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US446252A priority Critical patent/US1409241A/en
Application granted granted Critical
Publication of US1409241A publication Critical patent/US1409241A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C31/00Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/02Gliders, e.g. sailplanes

Definitions

  • My invention relates to aeroplanes and more particularly to planes adapted for gliding for hours without the aid of the motor and which embodies a new principle of aeronautics together with the principles of the aeroplanes now in use, the new principle relating to planes set at difierent angles from the ordinary planes and set at zero angle relative to direction of travel; and the object is to provide aeroplanes which will fill the requirements of a practical, more dependable commercial machine, more economical, adapted for safe passenger, mail, and express service, and more especially to provide an aeroplane which is adapted for slow and safe landings and to utilize the same natural fo-rces,wind.
  • Fig. 1 is a side elevation of the improved aeroplane.
  • Fig. 2 is a front elevation of the same.
  • the aeroplane shown herein has a body 1 which is provided with. doors and windows or port holes 2. Lifting planes of the usual curved type are mounted on the body 1 in the ordinary way.
  • Theaeroplane is provided with propellers of ordinary type for driving the machine and is provided with an ordinary rudder and tail piece.
  • inclined planes 3 and 4 are attached to the body 1 near the lower part and attached at their upper and outer ends to another plane
  • the planes 3 and 4 are set at an angle of zero relative to the direction of travel.
  • the member 5 is also a horizontal member of zero angle attached to the top of the aeroplane for soaring or floating purposes.
  • the lifting planes and rudders operate as such devices operate in aeroplanes now in use.
  • the soaring planes are for use after the desired height has been reached.
  • the soaring planes are set at zero angle or no lift or no resistance or an absolute plane with the direction of travel when ascending.
  • the engines may be cut off or slowed down. All planes of no angle or zero anglewill come into effect against the pull of gravitation and will sustain the aeroplane in the air without the aid of the motor, in a manner similar to the soaring of large birds which can soar for hours without flopping their wings.
  • the rudder can then be used to make the entire machine turn all the planes slightly downward and under these conditions, the pull of gravity will carry the aeroplane long distances without the aid of the motor, the aeroplane being sustained by means of the additional zero angle planes which operate on the parachute principle and effect slow and safe landings.
  • the automatic stabilizing effect is obtained by the four inclined planes 3 and 4. the principal part of the weight being below the center of gravity of the machine.
  • Vhat I claim is,-
  • an aeroplane provided with curved lifting planes and body.- sustaining planes consisting of a horizontal plane above said lifting planes attached to said body and of planes set at an angle relative to said lifting planes attached to said body and to said horizontal plane, all of the last named planes except the lifting planes being set at an angle of zero relative to the direction of travel.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Catching Or Destruction (AREA)

Description

l. B.. SANDERS.
AEROPLANE.
APPLICATION FILED FEB.I9,'I921.
.- 41 Patented Mar-14,1922.
. awwwkvz PATENT OFFICE.
IRA B. SANDERS, OF FORT WORTH, TEXAS.
i AEROPLANE.
Application filed February 19, 1921.
To all whom it may concern Be it known that I, IRA B. SANDERS, a citizen of the United States of America, residing at Fort Worth, in the county of Tarrant and State of Texas, have invented certain new and useful Improvements in Aeroplanes, of which the following is a specification.
My invention relates to aeroplanes and more particularly to planes adapted for gliding for hours without the aid of the motor and which embodies a new principle of aeronautics together with the principles of the aeroplanes now in use, the new principle relating to planes set at difierent angles from the ordinary planes and set at zero angle relative to direction of travel; and the object is to provide aeroplanes which will fill the requirements of a practical, more dependable commercial machine, more economical, adapted for safe passenger, mail, and express service, and more especially to provide an aeroplane which is adapted for slow and safe landings and to utilize the same natural fo-rces,wind. gravity, momentum, and velocity, that are utilized by certain large birds, such as the American eagle and the common blizzard. These birds spread their wings, and without flopping the wings. they can soar and soar and rise higher and higher, and then travel for hours with only natural forces to sustain them. Other objects and advantages will be fully explained in the following description and the invention will be more particularly pointed out in the claim.
Reference is had to the accompanying drawings which form a part of this application.
Fig. 1 is a side elevation of the improved aeroplane. Fig. 2 is a front elevation of the same.
Similar characters of reference are used to indicate the same parts throughout the several views.
The aeroplane shown herein has a body 1 which is provided with. doors and windows or port holes 2. Lifting planes of the usual curved type are mounted on the body 1 in the ordinary way. Theaeroplane is provided with propellers of ordinary type for driving the machine and is provided with an ordinary rudder and tail piece.
Specification of Letters Patent.
Patented Mar. 14, 1922'.
Serial No. 446,252.
In addition to the curved lifting planes above described, inclined planes 3 and 4 are attached to the body 1 near the lower part and attached at their upper and outer ends to another plane The planes 3 and 4 are set at an angle of zero relative to the direction of travel. The member 5 is also a horizontal member of zero angle attached to the top of the aeroplane for soaring or floating purposes.
In operation, the lifting planes and rudders operate as such devices operate in aeroplanes now in use. The soaring planes are for use after the desired height has been reached. The soaring planes are set at zero angle or no lift or no resistance or an absolute plane with the direction of travel when ascending. After the required height has been reached, the engines may be cut off or slowed down. All planes of no angle or zero anglewill come into effect against the pull of gravitation and will sustain the aeroplane in the air without the aid of the motor, in a manner similar to the soaring of large birds which can soar for hours without flopping their wings. The rudder can then be used to make the entire machine turn all the planes slightly downward and under these conditions, the pull of gravity will carry the aeroplane long distances without the aid of the motor, the aeroplane being sustained by means of the additional zero angle planes which operate on the parachute principle and effect slow and safe landings. The automatic stabilizing effect is obtained by the four inclined planes 3 and 4. the principal part of the weight being below the center of gravity of the machine.
Vhat I claim, is,-
In an aeroplane provided with curved lifting planes and body.- sustaining planes consisting of a horizontal plane above said lifting planes attached to said body and of planes set at an angle relative to said lifting planes attached to said body and to said horizontal plane, all of the last named planes except the lifting planes being set at an angle of zero relative to the direction of travel.
In testimony whereof, I set my hand, this 15th day of February, 1921.
IRA B. SANDERS.
US446252A 1921-02-19 1921-02-19 Aeroplane Expired - Lifetime US1409241A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US446252A US1409241A (en) 1921-02-19 1921-02-19 Aeroplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US446252A US1409241A (en) 1921-02-19 1921-02-19 Aeroplane

Publications (1)

Publication Number Publication Date
US1409241A true US1409241A (en) 1922-03-14

Family

ID=23771899

Family Applications (1)

Application Number Title Priority Date Filing Date
US446252A Expired - Lifetime US1409241A (en) 1921-02-19 1921-02-19 Aeroplane

Country Status (1)

Country Link
US (1) US1409241A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102092474A (en) * 2011-01-28 2011-06-15 曾道强 Novel airplane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102092474A (en) * 2011-01-28 2011-06-15 曾道强 Novel airplane

Similar Documents

Publication Publication Date Title
US2649265A (en) Airplane with stabilizing fins
US2118052A (en) Propeller assembly for aircraft
US2461805A (en) Airplane wing arrangement
US3025027A (en) Vertical airfoil
US2380535A (en) Aircraft
US2478967A (en) Stall warning device for airplanes
US1875267A (en) Umberto savoja
US1409241A (en) Aeroplane
US1968497A (en) Aeroplane
US3203649A (en) Rotor flap high lift system
US1881034A (en) Safety device for aeroplanes
US1772586A (en) Aircraft
US2303713A (en) Aircraft
US2469619A (en) Aircraft whose lift is increased by power means
US3063659A (en) Safety aircraft
US1848037A (en) Airplane
US1840683A (en) Airplane stabilizer
US2068616A (en) Aircraft
US2517850A (en) Combination airplane and wing unit for same
US1878808A (en) Aeroplane
US1560860A (en) Airplane
US2072029A (en) Aeroplane construction
US2084502A (en) Airplane construction
US1435848A (en) Aeroplane
US2515587A (en) Airplane with circular airfoil