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GB2109755B - Propulsion system with thrust vectoring for a v/stol airplane - Google Patents

Propulsion system with thrust vectoring for a v/stol airplane

Info

Publication number
GB2109755B
GB2109755B GB08135263A GB8135263A GB2109755B GB 2109755 B GB2109755 B GB 2109755B GB 08135263 A GB08135263 A GB 08135263A GB 8135263 A GB8135263 A GB 8135263A GB 2109755 B GB2109755 B GB 2109755B
Authority
GB
United Kingdom
Prior art keywords
propulsion system
thrust vectoring
stol
airplane
stol airplane
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
Application number
GB08135263A
Other versions
GB2109755A (en
Inventor
Ganey W Bradfield
Glynn P Gragin
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.)
General Dynamics Corp
Original Assignee
General Dynamics Corp
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 General Dynamics Corp filed Critical General Dynamics Corp
Priority to GB08135263A priority Critical patent/GB2109755B/en
Publication of GB2109755A publication Critical patent/GB2109755A/en
Application granted granted Critical
Publication of GB2109755B publication Critical patent/GB2109755B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB08135263A 1981-11-23 1981-11-23 Propulsion system with thrust vectoring for a v/stol airplane Expired GB2109755B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08135263A GB2109755B (en) 1981-11-23 1981-11-23 Propulsion system with thrust vectoring for a v/stol airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08135263A GB2109755B (en) 1981-11-23 1981-11-23 Propulsion system with thrust vectoring for a v/stol airplane

Publications (2)

Publication Number Publication Date
GB2109755A GB2109755A (en) 1983-06-08
GB2109755B true GB2109755B (en) 1985-06-12

Family

ID=10526080

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08135263A Expired GB2109755B (en) 1981-11-23 1981-11-23 Propulsion system with thrust vectoring for a v/stol airplane

Country Status (1)

Country Link
GB (1) GB2109755B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7726609B2 (en) * 2007-03-16 2010-06-01 The Boeing Company High-performance low-noise aircraft exhaust systems and methods
DE102017108543B4 (en) 2016-04-23 2022-04-28 Oleg Tchebunin Vertical take-off aircraft, the propulsion of which has rotary piston engines with a continuous combustion process and thrust direction pivoting systems
CN107521665A (en) * 2017-09-08 2017-12-29 中国民航大学 Aerial turbo fan engine bilayer " D " shape nozzle
CN120007463B (en) * 2025-03-10 2025-10-17 南京航空航天大学 Large-range variable area ratio vector exhaust device and exhaust method thereof

Also Published As

Publication number Publication date
GB2109755A (en) 1983-06-08

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19951123