US1293688A - Aircraft. - Google Patents

Aircraft. Download PDF

Info

Publication number
US1293688A
US1293688A US17865217A US17865217A US1293688A US 1293688 A US1293688 A US 1293688A US 17865217 A US17865217 A US 17865217A US 17865217 A US17865217 A US 17865217A US 1293688 A US1293688 A US 1293688A
Authority
US
United States
Prior art keywords
transparent
covering
aircraft
openings
fuselage
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
US17865217A
Inventor
Mittie Taylor Brush
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 US17865217A priority Critical patent/US1293688A/en
Application granted granted Critical
Publication of US1293688A publication Critical patent/US1293688A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C7/00Structures or fairings not otherwise provided for

Definitions

  • My invention relates more particularly to air-craft of the aeroplane type, and has for its object the reduction of the visibility of such machines when in the .air to a minimum.
  • FIG. 1 is a perspective view, from below, of a common monoplane showing by way of illustration merely one embodiment of my invention
  • Fig. 2 a broken detail, enlarged, showing one means of lighting the engine and fuel tank mounted within the fuselage
  • Fig. 3 an enlarged detail of my improved surface covering material
  • Fig. 4 a section of such material a shown in Fig. 3.
  • the covering with which the upper and lower surfaces of the wings, the forward end of the fuselage, and both surfaces of the elevating planes and the vertical rudder of the machine are covered consists of a thin body-piece or sheet 1, provided with openings 2 to the edges of which are sewed or otherwise suitably secured thin pieces 3 of transparent material, and a sheet of woven wire or light wire or linen mesh 4 which is applied to and reinforces the back of the body-piece and the windows.
  • the prepared linen cloth now commonly used as a surfacing material for aeroplanes and for the windows a non-inflammable or slow burning material which is known in the market as celestrome, and the front of the covering is, or may be.
  • the outer surfaces of the engine .5, fuel tank 6, and other similar non-transparent bodies mounted within the fuselage, or between the wings of a biplane, are lighted by electric lamps 7, which may be conveniently supported either upon' the parts themselves or on the adjacent framework of the fuselage and are supplied with electricity from any suitable source (not shown); or, in stead of electric lights, acetylene lamps or other suitable means for illuminating these surfaces may be employed. It may also be found desirable, wherever practicable, tolight the edges of the wings and control planes and the outlines of the fuselage.
  • An aircraft having for its outer surfaces a covering provided at intervals throughout its area with relatively small openings filled with a transparent material.
  • An aircraft ha-vin for its outer surfaces a covering provi ed with a plurality of relatively small openings filled with a transparent material and means for illuminating the surfaces of non-transparent bodies carried therein.
  • An aeroplane having wings which are covered above and below with a surfacing material provided with a plurality of relatively small windows closed to air but permitting the passage of rays of light.
  • An aeroplane having its wings and portions of its fuselage covered with a nontransparent surfacing material provided at more or less regular intervals throughout its area with closed windows through which rays of lightmay pass.
  • An aeroplane having its wings and fuselage covered with a non-transparent surfaceing material provided at intervals throughout-its area with relatively small windows which permit the passage of rays of with a plurality of relatively small and more.
  • ering for aircraft which consists of a body of prepared linen cloth having a plurality of relatively small and more or less'reg'ularly distributed openings and thin pieces of a transparent slow burning material secured to the edges of and covering the openings.
  • a covering for aircraft which consists of a prepared linen cloth provided with a plurality "of small openings covered with pieces of transparent slow burning material and a reinforcement of woven wire secured to the back'of the cloth.

Description

M. T. BRUSH.
AIRCRAFT.
APPLICATION FILED JULY 5,1917
Patented'lieb. 11, 1919.
mm; )1, 4t, mu
INVENTOR. BY M 6 ATTO RNEY
MITTIE TAYLOR BRUSH, 0F DUBLIN, NEW HAMPSHIRE.
AIRCRAFT.
Specification of Letters Patent.
Patented Feb. 111, 1919,
Application filed July 5, 1917. Serial No. 178,652.
To all whom, it may concern:
Be it known that I, MITTIE TAYLOR BRUSH, a citizen of the United States, residing at Dublin, in the county of Cheshire and State of New Hampshire, have invented certain new and useful Improvements in Aircraft, of which the following is a specification.
My invention relates more particularly to air-craft of the aeroplane type, and has for its object the reduction of the visibility of such machines when in the .air to a minimum.
The visibility of an object is dependent upon the contrasts of light and shade on its different surfaces, due to the diflerent amounts of light reflected therefrom, and between the object as a whole and the background against which it is silhouetted. Consequently, a transparent object will be invisible (at least if its surfaces do not reflect light or all reflect. the same amount) because an observer, looking toward it, will see only the background.
It has accordingly been proposed to use a transparent material for the surface cov ering of the wings and body of aeroplanes in order to reduce their visibility when in use, but nosuitable material has as yet been found for the purpose. I
I have discovered, however, that, viewed from an appreciable distance, the effect of transparency is obtained when a non trans parent material or body is provided with a plurality of relatively small and more or less regularly distributed openings, since the rays of light which pass through such openings become diffused and practicall obliterate all contrasts of light and sha e on adjacent surfaces. Thus, by forming in the linen cloth or other non-transparent mate'- rial ordinarily used for the purpose a number of small openings and filling or covering them with a suitable transparent medium, I have obtained what is in effect a new transparent covering material; and I have found that by artificially lighting the non-transparent bodies, such as the motor, fuel tank, etc., usually mounted upon or within the fuselage of an aeroplane thus cov- I ered, I am able to produce amachine which is practically invisible when in the air.
My invention, which embraces the two features mentioned, will be understood by reference to the accompanying drawing, in which Figure 1 is a perspective view, from below, of a common monoplane showing by way of illustration merely one embodiment of my invention; Fig. 2, a broken detail, enlarged, showing one means of lighting the engine and fuel tank mounted within the fuselage; Fig. 3, an enlarged detail of my improved surface covering material; and Fig. 4, a section of such material a shown in Fig. 3.
As here illustrated, the covering with which the upper and lower surfaces of the wings, the forward end of the fuselage, and both surfaces of the elevating planes and the vertical rudder of the machine are covered consists of a thin body-piece or sheet 1, provided with openings 2 to the edges of which are sewed or otherwise suitably secured thin pieces 3 of transparent material, and a sheet of woven wire or light wire or linen mesh 4 which is applied to and reinforces the back of the body-piece and the windows. For the body of the covering I prefer to use the prepared linen cloth now commonly used as a surfacing material for aeroplanes and for the windows a non-inflammable or slow burning material which is known in the market as celestrome, and the front of the covering is, or may be. varnished to better secure the edges of the openings in the cloth and to give a smooth outer surface. I thus obtain a strong smooth covering which is non-combustible, or, rather, slow burning, and which, when the machine is in the air, is practically transparent. It is to be understood, however, that I do not limit myself to the specified materials for the body and the windows, as any suitable materials may be used; and, whenever it may be found to be desirable to cover the fuselage, either in whole or in part, with a sheathing of wood or with metal plates, windows of suitable material may be set in openings therein and secured in any suitable manner. The wire backing may, of course, be omitted. if not required to secure the needed strength.
The outer surfaces of the engine .5, fuel tank 6, and other similar non-transparent bodies mounted within the fuselage, or between the wings of a biplane, are lighted by electric lamps 7, which may be conveniently supported either upon' the parts themselves or on the adjacent framework of the fuselage and are supplied with electricity from any suitable source (not shown); or, in stead of electric lights, acetylene lamps or other suitable means for illuminating these surfaces may be employed. It may also be found desirable, wherever practicable, tolight the edges of the wings and control planes and the outlines of the fuselage.
Having explained the principle of my invention and illustrated and described one practical embodiment of its several features, what I claim as new, and desire to secure by Letters Patent, is-
. 1. An aircraft having for its outer surfaces a covering provided at intervals throughout its area with relatively small openings filled with a transparent material.
2. An aircraft ha-vin for its outer surfaces a covering provi ed with a plurality of relatively small openings filled with a transparent material and means for illuminating the surfaces of non-transparent bodies carried therein.
3. An aeroplane having wings which are covered above and below with a surfacing material provided with a plurality of relatively small windows closed to air but permitting the passage of rays of light.
4. An aeroplane having its wings and portions of its fuselage covered with a nontransparent surfacing material provided at more or less regular intervals throughout its area with closed windows through which rays of lightmay pass.
5. An aeroplane having its wings and fuselage covered with a non-transparent surfaceing material provided at intervals throughout-its area with relatively small windows which permit the passage of rays of with a plurality of relatively small and more.
or less regularly distributed openings filled with a transparent medium, and a backing of woven wire.
ering for aircraft which consists of a body of prepared linen cloth having a plurality of relatively small and more or less'reg'ularly distributed openings and thin pieces of a transparent slow burning material secured to the edges of and covering the openings.
9. As a new article of manufacture, a covering for aircraft which consists of a prepared linen cloth provided with a plurality "of small openings covered with pieces of transparent slow burning material and a reinforcement of woven wire secured to the back'of the cloth.
MITTIE TAYLOR BRUSH.
8. As a new article of manufacture, a cov-
US17865217A 1917-07-05 1917-07-05 Aircraft. Expired - Lifetime US1293688A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US17865217A US1293688A (en) 1917-07-05 1917-07-05 Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US17865217A US1293688A (en) 1917-07-05 1917-07-05 Aircraft.

Publications (1)

Publication Number Publication Date
US1293688A true US1293688A (en) 1919-02-11

Family

ID=3361243

Family Applications (1)

Application Number Title Priority Date Filing Date
US17865217A Expired - Lifetime US1293688A (en) 1917-07-05 1917-07-05 Aircraft.

Country Status (1)

Country Link
US (1) US1293688A (en)

Similar Documents

Publication Publication Date Title
US2053173A (en) Shadow producing screen for luminous projections and other applications and process for its manufacture
DE2245861A1 (en) ARRANGEMENT OF IMITATED FIREPLACE FIRE
CN104235718A (en) Vehicle headlamp assmebly
DE19859195A1 (en) Sight integrated component part of compound material with at least one carrier layer and at least partly light permeable decorative layer also light reflecting surface for background illumination of decorative layer
DE102015219081A1 (en) Light emission device and vehicle light
US1293688A (en) Aircraft.
US9764855B2 (en) Exterior structure component for an aircraft, aircraft with an exterior structure component, and method for manufacturing an exterior structure component for an aircraft
US2386268A (en) Approach light
GB1209918A (en) Improvements in or relating to vehicle fuel cells
US2704321A (en) Aircraft illuminating system for identification
CN204937457U (en) A kind of Material Stiffened Panel and there is its aerofoil and aircraft
US2571158A (en) Illuminated aircraft wing tip
DE102016104113B4 (en) FLAT LIGHTING DEVICE FOR PARTITION WALLS IN AIRPLANE INTERIORS
US1946379A (en) Vehicle light
US2994150A (en) Ornamental articles
DE102021125960A1 (en) Lighting for an airplane window
US3402981A (en) Glare reduced light ray screen
US2132850A (en) Lamp shade
DE102006005692A1 (en) Sun shield visor for motor vehicle has flat light source between translucent decor material and body
GB990254A (en) Improvements in or relating to lamp shades, diffusers and the like
DE453532C (en) Headlight mirror
US1803439A (en) Advertising sign
US2350166A (en) Windshield glare diffuser
DE202022102291U1 (en) Concealable lamp mirror
GB260576A (en) Improvements in lamps or searchlights for aircraft