US1025941A - Aeroplane. - Google Patents

Aeroplane. Download PDF

Info

Publication number
US1025941A
US1025941A US635146A US1911635146A US1025941A US 1025941 A US1025941 A US 1025941A US 635146 A US635146 A US 635146A US 1911635146 A US1911635146 A US 1911635146A US 1025941 A US1025941 A US 1025941A
Authority
US
United States
Prior art keywords
landing
frame
aeroplane
wheels
shoes
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
US635146A
Inventor
Rene Arnoux
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
Priority claimed from US52915309A external-priority patent/US1095952A/en
Application filed by Individual filed Critical Individual
Priority to US635146A priority Critical patent/US1025941A/en
Application granted granted Critical
Publication of US1025941A publication Critical patent/US1025941A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42Arrangement or adaptation of brakes

Definitions

  • the present invention relates to improvements in aeroplanes, and it has for its object primarily to provide an improved mounting for structures of this character which embodies a frame, preferably the main frame of the apparatus, such frame having relatively long skids or shoes, and Wheels which are sustained by springs whereby during the landing of the aeroplane or while the same is traveling over the ground, the
  • FIG. 1 represents aside elevation of an aeroplane equipped with a mounting or landing mechanism constructed in accordance with the present invention
  • Fig. 2 is a top plan view of one of the landing wheels showing its spring mounting and a portion of the frame to which these springs are connected.
  • nism as applied to one form of aeroplane as an example, it having a main or base frame 1, an'uipper frame 2 which serves as a mounting for the lanes 3 and for a propeller 4, the prope ler being mounted on a driving shaft 5 and the driving shaft is aperatively connected by sprocket and chain gearin 6 or equivalent mechanism to a motor 7, t e latter being preferably placed at a relatively low point on the structure and in.
  • the main or base frame is formed with longitudinally extending skids or shoes 8, these skids or shoes preferably extending substantially throughout the length of the base or main frame andthe rear portion of the main frame is supported. by a trailing wheel 9 while the forward portion of the main or base frame is provided with landing wheels 10.
  • Each of these wheels has a yielding connection with themain or base frame whereby when the weight of the machine is imposed upon these landing wheels, the spring connections will yield and allow the skids or shoes on the bottom of the main or base frame to engage and slide over the surface of the ground, the friction thus produced serving to retardthe motion of the apparatus.
  • the axis 1 of each landing wheel is secured to a pair of springs 12 which are preferably arranged at opposite sides ofthe landing wheel.
  • the springs are pivotally wherebythe wheels 10 may assume different positions about these pivots which are in advance of the respective wheels and thereby enable the wheels to steer themselves antomatically.
  • These springs are secured to a cross member or other appropriate part of the main or base frame.
  • skids or shoes normally slope up wardly toward the front of the main or base frame so that when the spring-mounted landing wheels receive the thrust due to the weight of the apparatus in landing, these skids or shoes will descend and assume a position substantially parallel to the ground. Owing to the relatively long surfaces offered by the skids or shoes to the ground, stability afforded the apparatus that will prevent its pitching forward or overturning, and, moreover, the maximum braking or retarding effectwill be obtained.
  • skids or shoes according to the present invention are rigidly attached to or form rigid parts of the main or base frame of the machine and, hence, they may be made very strong and will be amply able to withstand the shocks incident to the landing of the apparatus without liability of breakage.
  • a frame provided with a relatively fixed shoe, landing wheels, and means for yieldably mounting said wheels with respect to said frame to permit -said shoe to contact with and produce a vbraking action upon the ground during landing of the aeroplane and causing said wheels to nern'ially project below said shoe and to support the aeroplane.
  • a frame provided with a long and straight skid or shoe, a landing wheel arranged toward the front of said skid 'or shoe, and a spring connection between said frame and landing wheel to permit said skid or shoe to descend relatively to the landing wheel and engage substantially uniformly throughout its length with the ground.
  • a main supporting frame having a substantially straight longitudinally extending skid or shoe rigidly connected in fixed relation thereto, a landing wheel arranged toward the front of the skid or shoe, and a spring connection bet-ween said landing wheel and frame and adapted to support the forward end of the skid or shoe in an upwardly and forwardly inclined position with respect to the ground, said spring connection being yieldable to permit the skid or shoe to descend relatively to the landing wheel and engage the ground to produce a braking action thereon during landing of the aeroplane.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)

Description

R.- ARNOUX.
AEROPLANE. 7 APPLICATION FILED JUNE 24, 1911.
1,025,941; Patented May 7,1912.
RENE annoox, arrears, FRANCE.
' annormn'n.
esson.
Specification of Letters I'atent.
, Patented Mayi', 1912.
Original application filed November 20, 1909, Serial No. 529,153. Divided. and this application filed June 24, 1911. Serial No. 635,146.
The present invention relates to improvements in aeroplanes, and it has for its object primarily to provide an improved mounting for structures of this character which embodies a frame, preferably the main frame of the apparatus, such frame having relatively long skids or shoes, and Wheels which are sustained by springs whereby during the landing of the aeroplane or while the same is traveling over the ground, the
weight of the apparatus will cause such springs to yield and thereby permit the relatively long skids or shoes of the frame to engage or contactwith the ground and thereby produce a braking or retarding effect which will bring the apparatus to a state of rest. Furthermore, while the aeroplane is traveling over the ground, these relatively long skids or shoes will bridge or span ruts, holes or transverse ditches in which the wheels may enter, the movement of the machine being unimpeded owing to the support afforded by these skids or shoes, and the wheels will be able to leave the rats, holes or ditches without liability of injury or breakage.
To these and other ends, the invention consists in certain improvements and combinations and arrangements of parts, all as will be hereinafter morefully described, the novel features being pointed out particularly in the claims at the end of the specification.
In the accompanying drawing:-l igure 1 represents aside elevation of an aeroplane equipped with a mounting or landing mechanism constructed in accordance with the present invention; and Fig. 2 is a top plan view of one of the landing wheels showing its spring mounting and a portion of the frame to which these springs are connected.
Similar parts are designated by the same reference characters in the several views.
nism as applied to one form of aeroplane as an example, it having a main or base frame 1, an'uipper frame 2 which serves as a mounting for the lanes 3 and for a propeller 4, the prope ler being mounted on a driving shaft 5 and the driving shaft is aperatively connected by sprocket and chain gearin 6 or equivalent mechanism to a motor 7, t e latter being preferably placed at a relatively low point on the structure and in.
the present instance it is mounted on the main or base frame 1. v The particular type of aeroplane shown generally in the present instance is described fully in my prior application, Serial No.
529,158 of which the presentapplication is a division. 9
The main or base frame is formed with longitudinally extending skids or shoes 8, these skids or shoes preferably extending substantially throughout the length of the base or main frame andthe rear portion of the main frame is supported. by a trailing wheel 9 while the forward portion of the main or base frame is provided with landing wheels 10. Each of these wheels has a yielding connection with themain or base frame whereby when the weight of the machine is imposed upon these landing wheels, the spring connections will yield and allow the skids or shoes on the bottom of the main or base frame to engage and slide over the surface of the ground, the friction thus produced serving to retardthe motion of the apparatus. In the present instance the axis 1 of each landing wheel is secured to a pair of springs 12 which are preferably arranged at opposite sides ofthe landing wheel. In the preferred construction, the
forward ends'of the springs are pivotally wherebythe wheels 10 may assume different positions about these pivots which are in advance of the respective wheels and thereby enable the wheels to steer themselves antomatically. These springs are secured to a cross member or other appropriate part of the main or base frame.
To insure substantially. uniform contact of practically the entire length of the skids or shoes with the ground during landing, these skids or shoes normally slope up wardly toward the front of the main or base frame so that when the spring-mounted landing wheels receive the thrust due to the weight of the apparatus in landing, these skids or shoes will descend and assume a position substantially parallel to the ground. Owing to the relatively long surfaces offered by the skids or shoes to the ground, stability afforded the apparatus that will prevent its pitching forward or overturning, and, moreover, the maximum braking or retarding effectwill be obtained. These skids or shoes according to the present invention are rigidly attached to or form rigid parts of the main or base frame of the machine and, hence, they may be made very strong and will be amply able to withstand the shocks incident to the landing of the apparatus without liability of breakage.
I claim as my invention 1. In an aeroplane, a frame provided with a relatively fixed shoe, landing wheels, and means for yieldably mounting said wheels with respect to said frame to permit -said shoe to contact with and produce a vbraking action upon the ground during landing of the aeroplane and causing said wheels to nern'ially project below said shoe and to support the aeroplane.
2, In an ae1.'(. plane, a frame provided with a long and straight skid or shoe, a landing wheel arranged toward the front of said skid 'or shoe, and a spring connection between said frame and landing wheel to permit said skid or shoe to descend relatively to the landing wheel and engage substantially uniformly throughout its length with the ground.
3. In an aeroplane, the combination of a main supporting frame having a substantially straight longitudinally extending skid or shoe rigidly connected in fixed relation thereto, a landing wheel arranged toward the front of the skid or shoe, and a spring connection bet-ween said landing wheel and frame and adapted to support the forward end of the skid or shoe in an upwardly and forwardly inclined position with respect to the ground, said spring connection being yieldable to permit the skid or shoe to descend relatively to the landing wheel and engage the ground to produce a braking action thereon during landing of the aeroplane.
In testimony whereof I have hereunto setlny hand in presence of two subscribing witnesses.
RENE ARNOUX.
\Vitnesses II. (J. Coxn, lan. 'BLUAI.
US635146A 1909-11-20 1911-06-24 Aeroplane. Expired - Lifetime US1025941A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US635146A US1025941A (en) 1909-11-20 1911-06-24 Aeroplane.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US52915309A US1095952A (en) 1909-11-20 1909-11-20 Aeroplane.
US635146A US1025941A (en) 1909-11-20 1911-06-24 Aeroplane.

Publications (1)

Publication Number Publication Date
US1025941A true US1025941A (en) 1912-05-07

Family

ID=3094236

Family Applications (1)

Application Number Title Priority Date Filing Date
US635146A Expired - Lifetime US1025941A (en) 1909-11-20 1911-06-24 Aeroplane.

Country Status (1)

Country Link
US (1) US1025941A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5217183A (en) * 1991-07-24 1993-06-08 James Liautaud Cantilevered helicopter skid

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5217183A (en) * 1991-07-24 1993-06-08 James Liautaud Cantilevered helicopter skid

Similar Documents

Publication Publication Date Title
EP2712804A1 (en) Landing gear provided with a stiffening element to increase its roll stiffness, and aircraft
US1844295A (en) Landing gear for aircraft
US1302508A (en) Aeroplane.
US2181656A (en) Braking method and device for airplane launching systems
US1581415A (en) Landing apparatus of aircraft
US1362511A (en) Landing device for aircraft
US1355256A (en) Aeroplane
US1156215A (en) Heavier-than-air flying-machine.
US1003605A (en) Aeroplane.
US1068165A (en) Aerial navigation.
US989520A (en) Flying-machine.
US1127362A (en) Traction means for vehicle-wheels.
US1340483A (en) Aeroplane-undercarriage
US1112731A (en) Aeroplane.
US1104045A (en) Flying-machine.
US1528970A (en) Aeroplane
US1288781A (en) Flying-machine.
US1856778A (en) Tail wheel for aircraft
US1470087A (en) Motor sleigh
US1056063A (en) Runner attachment for automobiles.
GB274167A (en) Improvements in under-carriages or landing gear for aircraft
US1165580A (en) Flying-machine.
US1893381A (en) Coaster sled
US1119632A (en) Flying-machine.
US1358596A (en) Hydroaeroplane