PL424676A1 - Movable object with decreased air resistance - Google Patents

Movable object with decreased air resistance

Info

Publication number
PL424676A1
PL424676A1 PL424676A PL42467618A PL424676A1 PL 424676 A1 PL424676 A1 PL 424676A1 PL 424676 A PL424676 A PL 424676A PL 42467618 A PL42467618 A PL 42467618A PL 424676 A1 PL424676 A1 PL 424676A1
Authority
PL
Poland
Prior art keywords
air resistance
movable object
nozzle
decreased air
fuselage
Prior art date
Application number
PL424676A
Other languages
Polish (pl)
Other versions
PL236134B1 (en
Inventor
Cezary Śliwiński
Janusz Śliwiński
Original Assignee
Wojskowy Instytut Techniki Inżynieryjnej Im. Profesora Józefa Kosackiego
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 Wojskowy Instytut Techniki Inżynieryjnej Im. Profesora Józefa Kosackiego filed Critical Wojskowy Instytut Techniki Inżynieryjnej Im. Profesora Józefa Kosackiego
Priority to PL424676A priority Critical patent/PL236134B1/en
Publication of PL424676A1 publication Critical patent/PL424676A1/en
Publication of PL236134B1 publication Critical patent/PL236134B1/en

Links

Landscapes

  • Air Bags (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

Przedmiotem zgłoszenia jest ruchomy obiekt o zmniejszonym oporze powietrza, który przeznaczony jest do szybkiego przemieszczania się w przestrzeni powietrznej. Ruchomy obiekt o zmniejszonym oporze powietrza posiada kadłub (1), w którym umieszczona jest dysza (3) posiadająca dno (8) osadzone w otworze kadłuba (4). Na walcowej części dyszy (3), wylocie stożkowym dyszy (12) oraz wylocie stożkowym kadłuba (5) zamontowany jest pojemnik próżniowy (2). W statecznikach (6) zamontowane są dysze reakcyjne sterujące (7).The subject of the application is a mobile object with reduced air resistance, which is intended for rapid movement in the airspace. The mobile object with reduced air resistance has a fuselage (1) with a nozzle (3) with a bottom (8) embedded in the fuselage (4) opening. A vacuum container (2) is mounted on the cylindrical part of the nozzle (3), the conical outlet of the nozzle (12) and the conical outlet of the body (5). In the ballasts (6) steering reaction nozzles (7) are mounted.

PL424676A 2018-02-26 2018-02-26 Movable object with decreased air resistance PL236134B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL424676A PL236134B1 (en) 2018-02-26 2018-02-26 Movable object with decreased air resistance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL424676A PL236134B1 (en) 2018-02-26 2018-02-26 Movable object with decreased air resistance

Publications (2)

Publication Number Publication Date
PL424676A1 true PL424676A1 (en) 2019-09-09
PL236134B1 PL236134B1 (en) 2020-12-14

Family

ID=67844602

Family Applications (1)

Application Number Title Priority Date Filing Date
PL424676A PL236134B1 (en) 2018-02-26 2018-02-26 Movable object with decreased air resistance

Country Status (1)

Country Link
PL (1) PL236134B1 (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3350887A (en) * 1963-03-09 1967-11-07 Wasagchemie Ag Two-stage rocket propulsion system

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3350887A (en) * 1963-03-09 1967-11-07 Wasagchemie Ag Two-stage rocket propulsion system

Also Published As

Publication number Publication date
PL236134B1 (en) 2020-12-14

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